Advanced Materials by Design
June 1988
NTIS order #PB88-243548 Recommended Citation: U.S. Congress, Office of Technology Assessment, Advanced Materials by Design, OTA- E-351 (Washington, DC: U.S. Government Printing Office, June 1988).
Library of Congress Catalog Card Number 87-619860
For sale by the Superintendent of Documents U.S. Government Printing Office, Washington, DC 20402-9325 (order form can be found in the back of this report) Foreword
This assessment responds to a joint request from the House Committee on Sci- ence, Space, and Technology and the Senate Committee on Commerce, Science, and Transportation to analyze the military and commercial opportunities presented by new structural materials technologies, and to outline the Federal policy objectives that are consistent with those opportunities. New structural materials–ceramics, polymers, metals, or hybrid materials derived from these, called composites–open a promising avenue to renewed international com- petitiveness of U.S. manufacturing industries. There will be many opportunities for use of the materials in aerospace, automotive, industrial, medical, and construction appli- cations in the next 25 years. This assessment addresses the impact of advanced struc- tural materials on the competitiveness of the U.S. manufacturing sector, and offers policy options for accelerating the commercial utilization of the materials. in recent years, several excellent studies have been published on both ceramics and polymer matrix composites. This assessment draws on this body of work and presents a broad picture of where these technologies stand today and where they are likely to go in the future. OTA appreciates the assistance provided by the contractors, advisory panel, and workshop participants, as well as the many reviewers whose com- ments helped to ensure the accuracy of the report. Advanced Materials by Design Advisory Panel
Rodney W. Nichols, Chairman Executive Vice President, The Rockefeller University
J. Michael Bowman Joseph Panzarino Director, Composites Venture Director E. I. du Pent de Nemours & Co. R&D of High Performance Ceramics Norton Co. Robert Buffenbarger Chairman, Bargaining Committee Dennis W. Readey International Association of Machinists Chairman Ceramics Engineering Department Joel Clark Ohio State University Associate Professor of Materials Systems Massachusetts Institute of Technology B. Waker Rosen President Laimonis Embrekts Materials Sciences Corp. Consultant Dix Hills, NY Amy L. Walton Member, Technical Staff Samuel Goldberg Jet Propulsion Laboratory President, INCO-US, Inc. New York, NY Alvin S. Weinstein Consultant Sheldon Lambert Concord, NH Consultant Piano, TX Dick J. Wilkins Director James W. Mar Center for Composite Materials Professor University of Delaware Department of Aeronautics and Astronautics Massachusetts Institute of Technology Arthur F. McLean Manager, Ceramics Research Ford Motor Co.
NOTE: OTA appreciates the valuable assistance and thoughtful critiques provided by the advisory panel members. The panel does not, however, necessarily approve, disapprove, or endorse this assessment. OTA assumes full responsibility for the assessment and the accuracy of its contents. iv OTA Project Staff for Advanced Materials by Design
LioneI S. Johns, Assistant Director, OTA Energy, Materials, and International Security Division
Peter D, Blair, Energy and Materials Program Manager
Gregory Eyring, Project Director, November 1985 - June 1988
Laurie Evans Gavrin, Analyst, June 1986 - June 1988
Thomas E. Bull, Project Director, June 1985 - November 1985
Joan Adams, Analyst, June 1985 - January 1986
Administrative Staff Lillian Chapman Linda Long Tina Brumfield Contents
Page Overview ...... 1 Chapter l. Executive Summary ...... 7 Chapter 2. Advanced Ceramics ...... 37 Chapter 3. Polymer Matrix Composites ...... 73 Chapter 4. Metal Matrix Composites...... 99 Chapter 5. Factors Affecting the Use of Advanced Structural Materials...... 121 Chapter 6. Impacts on the Basic Metals Industries ...... 137 Chapter 7. Case Study: Polymer Matrix Composites in Automobiles ...... 155 Chapter 8. Industrial Criteria for Investment ...... 187 Chapter 9. International Business Trends ...... 203 Chapter 10. Collaborative R&D: A Solution? ...... 251 Chapter 11. The Military Role in Advanced Materials Development ...... 269 Chapter 12. Policy Issues and Options ...... 291 Appendix A. Contractors and Workshop Participants ...... 315 Appendix B. Glossary ...... 320 Index ...... 329 —
Overview
New structural materials technologies will be onstrated in large-scale commercial applications. a determining factor in the global competitive- Potential end users in the United States have ness of U.S. manufacturing industries in the 1990s adopted a “wait and see” attitude, pending the and beyond. Today, for instance, materials ac- solution of remaining technical and economic count for as much as 30 to 50 percent of the costs problems. However, through well-coordinated of most manufactured products. New materials government-industry efforts, several countries, that can reduce overall production costs and im- notably Japan, have initiated more aggressive pro- prove performance can provide a competitive grams to commercialize their evolving materials edge in many products, including aircraft, auto- technologies. These programs have succeeded mobiles, industrial machinery, and sporting goods. in bringing advanced material products to the market years in advance of comparable U.S. Remarkable advances in structural materials products. Concern about the U.S. competitive technologies have been made in the past 25 position has led Congress to seek a coherent na- years. New materials such as ceramics and com- tional program to ensure that the United States posites offer superior properties (e.g., high-tem- will be able to capitalize on the opportunities perature strength, high stiffness, and light weight) offered by advanced materials. compared with traditional metals such as steel Advanced materials can be classified as metals, and aluminum. What is more, the materials them- ceramics, polymers, or composites, which gen- selves can be designed to have the properties erally consist of fibers of one material held to- required by a given application. Use of such de- gether by a matrix of a second material. Com- signed materials, which are often called “ad- posites are designed so that the fibers provide vanced,” can lead to higher fuel efficiencies, strength, stiffness, and fracture toughness, and the lower assembly costs, and longer service life for matrix binds the fibers together in the proper ori- many manufactured products. entation. This assessment focuses on three prom- ising categories of structural materials: ceramics Although the United States has achieved a (including ceramic matrix composites), polymer strong position in advanced materials technol- matrix composites, and metal matrix composites. ogies, largely as a result of military programs, it The principal purpose is to describe the major is by no means certain that the United States will opportunities for use of ceramics and composites, lead the world in the commercialization of these and to identify steps that the Federal Government materials. The technologies are still in their in- could take to accelerate the commercialization fancy, and cost-effective use of advanced mate- of advanced materials technologies in the United rials and fabrication processes is yet to be dem- States.
THE U.S. ADVANCED MATERIALS ENVIRONMENT
The current value of components produced petitive posture, is improved by use of the mate- from advanced structural ceramics and compos- rials. When the overall value of these products ites in the United States is less than $2 billion per is taken into account, use of advanced structural year. However, by the year 2000, U.S. produc- materials is likely to have a dramatic impact on tion is expected to grow to nearly $20 billion. This gross national product, balance of trade, and em- estimate includes only the value of the materials ployment. and structures; it does not include the value of the finished products (e.g., aircraft and automo- Military demand for high performance materi- biles), whose performance, and therefore com- als in the United States has already created a
1 2 ● Advanced Materials by Design thriving community of advanced materials sup- “market pull” on advanced materials technol- pliers. These suppliers are also seeking commer- ogies in the United States. cial applications for their materials. At present, In contrast to the market pull orientation of though, advanced materials developed for mili- firms in the United States, end users in foreign tary applications are expensive, and fabrication competitor nations, notably in Japan, are pursu- processes are poorly suited for mass production. ing a “technology push” approach, in which Potential U.S. commercial end users believe near-term profits are sacrificed in favor of gain- that major use of these materials will not be prof- ing the production experience necessary to se- itable within the next 5 years, the typical plan- cure a share of the large future markets. This ag- ning horizon of most firms. In many cases, 10 to gressive approach will probably give these firms 20 years will be required to solve remaining tech- a significant advantage in exploiting global mar- nical problems and to develop rapid, low-cost kets as they develop. OTA finds that manufac- manufacturing methods. Investment risks are turing experience over time with advanced ma- especially high for commercial end users because terials will be a prerequisite for competing in the costs of scaling up laboratory processes for those markets; U.S. companies should not expect production are enormous, and the rapid pace of to be able to step in and produce competitive technology evolution could make these processes advanced materials products after the manufac- obsolete. Hence, there is very little commercial turing problems have been solved by others.
THE ROLE OF THE FEDERAL GOVERNMENT
The Federal Government directly affects the de- two major factors. First, the high cost of military velopment of advanced materials through fund- materials and fabrication processes limits their ing of basic research, technology demonstration acceptance in the commercial sector. Second, to programs, and military and aerospace procure- deny these advanced materials to the U.S.’s ad- ment of advanced materials and structures. The versaries, the government imposes restrictions on U.S. Government currently spends about $167 the export of the materials and on access to re- million per year for R&D on structural ceramics lated technical data. and composites, more than any other nation. About 40 percent ($69 million) of Federal Counting only basic and early applied research, spending for structural ceramics and composites the Department of Defense (DoD) sponsors about R&D is nonmilitary in nature, including most of 60 percent ($98 million) of this total. In the case that funded by the Department of Energy, the Na- of the military, the government itself is the cus- tional Aeronautics and Space Administration, the tomer for materials technology and hardware. National Science Foundation, the National Bu- Advanced materials are truly enabling technol- reau of Standards, and the Bureau of Mines. ogies for many military systems such as the Na- These agencies generally do not act as procurers tional Aerospace Plane, Stealth aircraft, and mis- of hardware. Rather, they sponsor materials re- siles; they can also enhance the mission capability search ranging from basic science to technology of a host of less exotic systems such as tanks, demonstration programs, according to their vari- ships, submarines, and ground vehicles. Trans- ous mission objectives. Where appropriate, they fer of DoD-funded materials technology to the openly seek to transfer materials technology to commercial sector, however, is discouraged by the private sector.
FOUR KEY POLICY OBJECTIVES
OTA’s analysis suggests four key Federal pol- cialization of advanced materials technologies. icy objectives that could accelerate the commer- Options for implementing these objectives range from those that have a broad scope, and affect 3. Facilitate more effective commercial exploi- many technologies, to those that specifically af- tation of military R&D investments where feet advanced materials technologies. possible. 1. Encourage potential end users to make long- ln the next 5 to 10 years, military demand for term capital investments in advanced ma- advanced materials is likely to grow at a faster terials. pace than commercial demand, so that military policies and requirements will strongly influence Greater investment in advanced materials by the agenda for advanced materials development potential end users would help to generate more in the United States. It is evident that government commercial market pull on these materials in the restrictions on advanced materials and associated United States. The climate for investment in long- technical data in the interests of national secu- term, high-risk technologies such as advanced rity can cause conflict with U.S.-based firms seek- materials could be improved by Federal Govern- ing unrestricted access to markets and informa- ment implemention of a variety of policy options tion. Furthermore, these conflicts are likely to designed to make more patient investment cap- become more severe as commercial applications ital available. These would include providing tax grow and as the companies involved become incentives for long-term capital investment, re- more multinational. ducing taxes on personal savings, and changing tort law to make product liability proportional to Ultimately, both national security and a com- proven negligence. . petitive manufacturing base will depend on a strong domestic advanced materials capability. 2. Facilitate government/university/industry col- Therefore, a major goal of U.S. policy should be laboration in R&D for low-cost materials fab- to strike an appropriate balance between mili- rication. tary and commercial interests+ Among the options The high cost of advanced materials develop- that could be considered are: updating export ment and the small near-term markets are forc- control lists so that they are applied only to tech- ing companies to seek collaborative R&D ar- nologies that provide important military advan- rangements to spread the risks and raise the large tage to the United States and that are not avail- amounts of capital required. Three major reser- able to our adversaries from other sources; voirs of materials expertise are available to U.S. greater support for military programs aimed at de- companies: 1) universities, 2) Federal labora- veloping low-cost materials fabrication processes tories, and 3) small high-technology firms. Among that could be adapted for commercial use; and industry/university and industry/Federal labora- clarification &military domestic sourcing policies tory collaborative centers in advanced materials, for advanced materials. OTA finds that industry generally participates to 4. Build a strong advanced materials technol- gain access to new ideas and trained graduate ogy infrastructure. students. up costs too high and the payofffs too uncertain Through acquisitions, joint ventures, and li- to justify commercialization of collaborative re- censing agreements, materials technology is flow- search results. The government could encourage ing rapidly among firms and across national the commercialization step by establishing col- borders. Critical advances continue to come from Iaborative centers in which government and in- abroad, and the flow of materials technology into dustry would share the costs of downstream ma- the United States may already be as important terials fabrication technology development. - as that@ It is essential that an adequate Another option would be to provide incentives technology be in place for rapidly for large companies to work with those small, capitalizing on research results, whether they high technology firms that have advanced ma- originate in the United States or abroad. Policy terials fabrication expertise, but lack the capital options for building up this infrastructure include: to explore its commercial potential. increasing funding for research on reliable, low- cost manufacturing method5;,~theti1J&BOddis pOrt for multidisciplinary materials engineering seminating information on foNn, ~nd domes programs in universities and for retraining of engi tic research efforts; acceieratins development of neers in the field who are unfamiliar with the new materials testing standards and. materials prop . materials .. erty databases for desianers; and iritreasingsup.
TWO VIEW$eOF'ADvANCED MATERIALS POLICIES , '. '-~:::-- . ,~. ~ ,~:.' ," '-:. ',~ . congr~~the Admin~ '~atioPted . .,ninals seen as putting the government in a posi- : con~na views of poficym~kMgWftIi'·repratQ," i tion of upickinl winners" -a role that is best left advClOced: matfitriafs. The crut'e)ftfte cor1!fict:is' :,: t(.} the private sector. According to this view, the w~:~:'~ral'COvern_t~uld"adOpf·'.~of Science and Technology Policy's Com a nationafPlari ,for advanced materials,fectmol- mittee on Materials (COMAT), and other inter ogy deVel~t, orwhet~er :jqals and .principal funding agencies. L . ~'e,!c~sive (iupUcation and waste. The NCMC is '" ',. ,.,.c, '" . ,<;onsidere(l redundant with these committees. According. to.t~e congressiOri~r~~w;~ twi9nal' goals and prIoritieS should ,beestabhsh~atiove OTA finds that it is more difficult to define na- the agency level, and agency SPftjdink.on ma- tional poJjey goals for advanced materials than terials programs should be m~de·tonsist~ntwith for more traditional critic~1 materials. To succeed them. This view is expres~ in the Na~ICrlt.. in its task, the NCMC will need to establish a ical Materials Act of 1984; in Whi~h Congr~ss more precise definition of the goals that would established the National Critical Materials CoUncil motivate suth a national materials policy, as well (NCMq in the Executive Office of the PreSident. . as 'to develop high~tevel Administration commit- The NCMC is charged with t.~ 'responsibility of ment to the ,concept of such a policy. working with 'th,~ principal furidfn8ase~cie~.nd ,Pending the resolution of these differences, th~ Offic~ 'of ~"ageme"t andBu:d~,t~define there are three further functions that the NCMC natio~I'prio~ for materiafsJ~&~and to co- .couldperform. First, it could serve as a point of ordinate the various agenc;y effo{B; " contact fo~ mol'1~oring industry concerns and rec- In the Administration's view; I)nOdtie$ for ad- ommendation$regarding joint industry/govern- vanced materials R&D cannot be se.panifedfmm ".ment initiatives .. Second, it could gather informa- the,functionafrequirements5)f t~ ·.ru4UJes'in ,.tion on dQrnestic and foreign materials R&D which they are 'Used. 'Because differ~t.ncies efforts and· disseminate it to industry. Third, it have different requirements for materials', 'deter- could act as a broker for resolving conflicts be- mination of R&D priorities is best made at the tween military and commercial agency goals for agency level. Strategic advanced materials plan- advanced materials. ADVANCED MATERiAlS POLICIES IN A BROADER CONTEXT In fllany respects, thecQmpe~hi~cha!len~s other technologies. Such policy options cannot facing advanced :materials",I,,'a:nj~~,otthe be adequately addressed at the agency level or challert&esfadns theU.S~·",~nuf"'~~,r . "> ;in interagency ~ommjttees; they c!early must be as a wttole;fheteiOJ!e, ~neeal~:poI- initiated 'in the highest councils of government. icy cannot be viewed as a,whQHy separate isSue. Adyanced materials policies ~herefore, can most Policy options such as tax incenti\'esJor·lOng-term effectively be treated as one facet of a high-level, capital investments or revision of export controls high-priority policy of strengthening the Nation's could also serve to stimulate a broad range' of entire industrial and manufacturing base. Chapter 1 Executive Summary CONTENTS Page Page Introduction ...... 7 Build a Strong Advanced Materials New Structural Materials ...... 8 Technology Infrastructure ...... 30 Ceramics ...... 10 Two Views of Advanced Materials Policies. . . . 31 Polymer Matrix Composites ...... 12 Advanced Materials Policies in a Broader Metal Matrix Composites...... 13 Context ...... 33 Research and Development Priorities...... 15 Factors Affecting the Use of Advanced Figures Materials ...... 15 Integrated Design and Manufacturing ...... 15 Figure No. Page 1-1. The Family of Structural Materials ...... 9 Automation...... 16 1-2. Multidisciplinary Approach ...... 16 Composite Reinforcement Types ...... 9 Education and Training ...... 16 1-3. Maximum Use Temperatures of Various Systems Approach to Costs ...... 17 Structural Materials ...... + ...... 10 1-4. Energy Costs...... 17 Comparison of the Specific Strength and Stiffness of Various Composites and Metals 10 impacts of Advanced MateriaIs on 1-5. Projected U.S. Markets for Structural Manufacturing ...... 18 Substitution, .,...... 18 Ceramics in the Year 2000 ...... 11 1-6. innovative Designs and New Products ...... 18 Typical Body Construction Assembly Using Industry Investment Criteria for Advanced Two Major PMC Moldings ...... 19 Materials ...... 19 1-7. Relative lmportance of Cost and Performance in Advanced Materials User Cost and Performance ...... 20 International Business Trends...... 21 Industries ...... 20 Ceramics ...... 21 Polymer Matrix Composites ...... 22 Tables Metal Matrix Composites...... 23 Table No. Page Government/University/Industry Collaboration 1-1. U.S. Materials and Minerals Legislation . . . 7 and Industrial Competitiveness ...... 24 1-2. Hypothetical Multidisciplinary Design Military Role in Advanced Materials Team for a Ceramic Component ...... 16 Development ...... 25 1-3. Estimated Production Value of Advanced Policy issues and Options ...... 26 Ceramics, 1985 ...... 21 Projections Based on a Continuation of the 1-4. Estimated Government Funding in Several Status Quo...... 27 Countries for Advanced Ceramics R&D in Encourage Long-Term Investment by 1985 ...... 22 Advanced Materials End Users ...... 28 1-5. Breakdown of Regional Markets for Facilitate Government/University/Industry Advanced Composites by End Use...... 22 Collaboration in R&D for Low-Cost 1-6. Distribution of Advanced PMC Production Materials Fabrication Processes ...... 28 in Western Europe...... 23 Facilitate More Effective Commercial 1-7. U.S. Government Agency Funding for Exploitation of Military R&D Investments Advanced Structural Materials in Where Possible...... 28 Fiscal Year 1987...... 26 Chapter 1 Executive Summary INTRODUCTION During the past 25 years, unprecedented progress Table 1-1 .—U.S. Materials and Minerals Legislation has been made in the development of new struc- Strategic War Materials Act–1939 tural materials. These materials, which include 53 Stat. 811 advanced ceramics, polymers, metals, and hy- Established the National Defense Stockpile, intended brid materials derived from these, called compos- to accumulate a 5-year supply of critical materials for use in wartime or national emergency. ites, open up new engineering possibilities for the Strategic and Critical Materials Stockpiling Act—1946 designer. Their superior properties, such as the 60 Stat. 596 high temperature strength of ceramics or the high Authorized appropriation of money to acquire metals, stiffness and light weight of composites, offer the oils, rubber, fibers, and other materials needed in wart i me. opportunity for more compact designs, greater Defense Production Act— 1950 fuel efficiency, and longer service life in a wide 64 Stat. 798 variety of products, from sports equipment to Authorized the President to allocate materials and fa- high performance aircraft. In addition, these cilities for defense production, to make and guarantee loans to expand defense production, and to enter into materials can lead to entirely new military and long-term supply contracts for scarce materials. commercial applications that would not be fea- Resource Recovery Act— 1970 sible with conventional materials. A graphic ex- Public Law 91-512 ample is the construction of the composite air- .Established the National Commission on Materials Policy to develop a national materials policy, including plane Voyager, which flew nonstop around the supply, use, recovery, and disposal of materials. world in December 1986. Mining and Minerals Policy Act– 1970 Public Law 91-631 In the next 25 years, new structural materials Encouraged the Secretary of the Interior to promote in- will provide a powerful leverage point for the volvement of private enterprise in economic develop- manufacturing sector of the economy: not only ment, mining disposal, and reclamation of materials. can ceramic and composite components deliver Strategic and Critical Stockpiling Revision Act—1979 Public Law 96-41 superior performance, they also enhance the per- Changed stockpile supply period to 3 years, limited to formance and value of the larger systems–e.g., national defense needs only; established a stockpile aircraft and automobiIes—i n which they are in- transaction fund. corporated. Given this multiplier effect, it is likely National Materials Policy, Research and Development Act– 1980 that the application of advanced structural ma- Public Law 96-479 terials will have a dramatic impact on gross na- Directed the President to assess material demand, sup- tional product, balance of trade, and employment plies, and needs for the economy and national securi- ty; and to submit a program plan to implement the in the United States. All of the industrialized findings of the assessment. countries have recognized these opportunities National Critical Materials Act— 1984 and are competing actively for shares of the large Public Law 98-373 commercial and military markets at stake. Established the National Critical Materials Council in the Executive Office of the President; the Council was As indicated in table 1-1, Congress has long authorized to oversee the development of policies relating to both critical and advanced materials; and to been concerned with materials issues, dating develop a program for implementing these policies. back to the Strategic War Materials Act of 1939. SOURCE Office of Technology Assessment, 1988 Through the 1950s, legislation continued to fo- cus on ensuring access to reliable supplies of stra- tegic materials in time of national emergency. The In 1984, these concerns were extended to en- 1970s saw legislative interest broaden to include compass advanced materials with the National the economic and environmental implications of Critical Materials Act (Public Law 98-373, Title II). the entire materials cycle, from mining to disposal. In this Act, Congress established the National Crit- 7 8 ● Advanced Materials by Design ical Materials Council in the Executive Office of factors will affect the time required to real- the President and charged it with the responsi- ize these opportunities? bility of overseeing the formulation of policies re- 2. What will be the impact of advanced mate- lating to both “critical” and “advanced” mate- rials on manufacturing industries in the United rials. The intent was to establish a policy focus States? above the agency level to set responsibilities 3. What is the competitive position of the United for developing materials policies, and to coordi- States in these technologies, and what trends nate the materials R&D programs of the relevant are likely to affect this position? agencies. 4. How can the federally funded advanced ma- terials R&D in universities and Federal lab- With the passage of the National Critical Ma- oratories be used more effectively to boost terials Act, Congress formally recognized that a the competitiveness of U.S. firms? domestic advanced materials manufacturing base 5. What are the implications of the large mili- will be critical for both U.S. industrial competi- tary role in advanced materials development tiveness and a strong national defense, and that for the commercial sector? progress in achieving this objective will be strongly 6. What policy options does the Federal Gov- influenced by Federal policies. Congressional in- ernment have to accelerate the commerciali- terest in advanced materials technologies has zation of advanced materials technologies? centered on several key issues: 1. What are the major potential opportunities These questions comprise the framework of this for advanced structural materials, and what assessment. NEW STRUCTURAL MATERIALS New structural materials can be classified as forced engineering plastics, which may also legiti- ceramics, polymers, or metals, as shown in fig- mately be considered advanced materials, are not ure 1-1. Two or more of these materials can be covered. combined together to form a composite that has properties superior to those of its constituents. Figure 1-3 compares the maximum use temper- Composites generally consist of fibrous or par- atures of the three primary categories of struc- ticulate reinforcements held together by a com- tural materials. Organic materials such as poly- mon matrix, as illustrated in figure 1-2. Continu- mers generally melt or char above 600° F (3160 ous fiber reinforcement enhances the structural C); the most refractory metals lose their useful properties of the composite far more than par- strength above 1900° F (10380 C); ceramics, how- ticles do. However, fiber-reinforced composites ever, can retain their strength above 30000 F are also more expensive and difficult to fabricate. (1649° C) and can potentially be useful up to 5000° F (2760° C). In applications such as heat Composites are classified according to their ma- engines and heat exchangers, in which efficiency trix phase. Thus, there are ceramic matrix com- increases with operating temperature, ceramics posites (CMCs), polymer matrix composites (PMCs), offer potential energy savings and cost savings and metal matrix composites (MMCs). Materials through simpler designs than would be possible within these categories are often called “advanced” with metals. if they exhibit properties, such as high tempera- ture strength or high stiffness per unit weight, Figure 1-4 compares the “specific” strength and that are significantly better than those of more stiffness (strength and stiffness per unit weight) conventional structural materials, such as steel of some advanced materials with those of con- and aluminum. This assessment focuses on ad- ventional metals. The specific stiffness of alumi- vanced structural ceramics (including CMCs), num can be increased by a factor of 3 by mixing PMCs, and MMCs. New metal alloys and unrein- the metal with. 50 percent by volume silicon car- Ch. 1—Executive Summary . 9 Figure 1-1 .—The Family of Structural Materials Figure 1-2.—Composhe Reinforcement Types , Includes ceramics, polymers, and metals. Reinforcements added to these materials produce ceramic matrix composites (CMCs), polymer matrix composites (PMCs), and metal matrix composites (MMCs). Materials in the shaded regions are dis- cussed in this assessment. SOURCE: Office of Technology Assessment, 1968. bide fibers to form an MMC. Even more impres- sive are PMCs such as graphite fiber-reinforced epoxy (graphite/epoxy), which may have specific strengths and stiffnesses up to 4 times those of steel and titanium (measured along the direction of fiber reinforcement). Such properties make it possible to build composite structures having the same strength and stiffness as metal structures but with up to 50 percent less weight, a major advan- tage in aircraft and space applications. Although the physical and mechanical prop- erties of ceramics and composites are impressive, the true hallmark of these advanced materials is that they are “tailored” materials; that is, they are built up from constituents to have the prop- erties required for a given application. Further- more, a composite structure can be designed so SOURCE: Carl Zweben, General Electric Co. that it has different properties in different direc- tions or locations. By judicious use of fiber or most needed. Great efficiencies of design and other reinforcement, strength or stiffness can be cost are made possible by this selective place- enhanced only in those locations where they are ment of the reinforcement.. 10 ● Advanced Materials by Design Figure 1-3.—Maximum Use Temperatures of Various Structural Materials ments and literally creates the necessary materi- als and the structure in an integrated manufac- turing process. Thus, with tailored materials, the old concepts of materials, design, and fabrication processes are merged together into the new con- I cepts of integrated design and manufacturing. I . These technologies differ greatly in their levels of maturity; e.g., PMCs are by far the most de- veloped, whereas CMCs are still in their infancy. In addition, the applications and market oppor- tunities for these materials vary widely. For these reasons, the three primary categories of materi- als treated in this assessment are discussed sep- arately below. Ceramics Ceramics encompass all solids that are neither organic nor metallic. Compared with metals, cer- . amics have superior wear resistance, high tem- Polymers Metals Ceramics perature strength, and chemical stability; they SOURCE: “Guide to Selecting Engineered Materials,” a special issue of Advanced also generally have lower thermal conductivity, Materials and Processes, vol. 2, No. 1, 1967. thermal expansion, and lower toughness (i.e., Figure 1-4.–Comparison of the Specific Strength they tend to be brittle). This brittleness causes a and Stiffness of Various Composites and Metals them to fail catastrophically when applied stress is sufficient to propagate cracks that originate at microscopic flaws in the material. Flaws as small as 20 micrometers (about one one-thousandth of an inch) can reduce the strength of a ceramic component below useful levels. Several approaches have been taken to improve the toughness of ceramics. The most satisfactory is to design the microstructure of the material to resist the propagation of cracks. Ceramic matrix composites, which contain dispersed ceramic Specific tensile strength (relative units) particulate, whiskers, or continuous fibers, are Silicon carbide fiber-reinforced aluminum and graphite fiber- reinforced epoxy composites exhibit many times the strength an especially promising technology for toughen- and stiffness of conventional metals. ing ceramics. Another approach is the applica- aSpecific properties are ordinary properties divided by density. Properties are tion of a thin ceramic coating to a metal substrate; measured along the direction of fiber reinforcement. bSteel: AISI 304; Aluminum: 6061-T6; Titanium: Ti-6A1-4V). this yields a component with the surface prop- SOURCE: Carl Zweben, General Electric Co. erties of a ceramic combined with the high tough- ness of metal in the bulk. The development of advanced materials has opened a whole new approach to engineering Market Opportunities for Ceramics design. In the past, the designer has started with a material and has selected discrete manufactur- Market demand for structural ceramics is not ing processes to transform it into the finished driving their development in most applications structure. With the new tailored materials, the at the present time. In 1987, the U.S. market for designer starts with the final performance require- advanced structural ceramics was estimated at Ch. 1—Executive Summary ● 11 only $171 million, primarily in wear-resistant ap- Figure 1-5.— Projected U.S. Markets for Structural plications. Projections to the year 2000, though, ‘Ceramics in the Year 2000 (billions of dollars) 1.0 ‘ place the U.S. market between $1 billion and $5 billion annually, spread among many new appli- cations discussed below. Early estimates that projected a $5 billion U.S. market for ceramics i n automotive heat engines (gasoline, diesel, or gas turbine) by the year 2000 now appear to have been too optimistic. More recent estimates indicate that the U.S. ceramic heat engine market in the year 2000 will be less than $1 billion, However, a large number of other 0.5 commercial applications for ceramics are possi- ble over this time period; examples are given in figure 1-5. Current Production Ceramics such as aluminum oxide, silicon ni- tride, and silicon carbide are in production for wear parts, cutting tool inserts, bearings, and coatings. The market share for ceramics in these applications is generally less than 5 percent, but substantial growth is expected. The U.S. markets SOURCES: a U S Department of Commerce, “A Competitive Assessment of the for the ceramic components alone could be over U S Advanced Ceramics Industry” (Washington, DC, U S Govern- ment Printing Office, March 1964) b $2 billion by the year 2000. R&D funding is cur- E.P. Rothman, J. Clark, and H.K. Bowen, Ceramic Cutting TooIS: A Production Cost Model and an Analysts of Potential Demand,” Ad- rently being provided by industry and is driven vanced Ceramic Materials, American Ceramics Society, Vol 1, No 4, October, 1986, pp. 325-331 by competition in a known market. Current mil- c High Technology, March 1986, p. 14 itary applications i n the United States include ra- d Business Communications Co, Inc, as reported in Ceramic Indus- try, Jan 1988, p 10 domes, armor, and infrared windows. e David W Richerson, “Design, Processing Development, and Manu- facturing Requirements of Ceramics and Ceramic Matrix Compos- ites,” contractor report prepared for the Office of Technology Ceramics are also in limited production (in Ja- Assessment, December 1965 pan) in discrete engine components such as tur- f Assumes a doubling from 1986 Paul Hurley, ‘New Filters Can Clean bochargers, glow plugs, rocker arms, and pre- Up in New Markets,” High Technology, August 1987 combustion chambers, as well as a number of achieve a production capability competitive with consumer products. foreign sources. Far-Term Production Near-Term Production Far-term applications (beyond 15 years) of ce- Near-term production (the next 10 to 15 years) ramics will require solution of major technical is expected in advanced bearings, bioceramics and economic problems. These include an ad- (ceramics used inside the body), construction ap- vanced automotive turbine engine, an advanced plications, heat exchangers, electrochemical de- ceramic diesel (although ceramics could be used vices, discrete components in automobile en- in military versions of these engines at an earlier gines, and military applications, Large markets are date), some electrochemical devices, military at stake. The technical feasibility has been dem- components, and heat exchangers. A variety of onstrated, but scale-up, cost reduction, and de- other turbine engines, especially turbines for air- sign optimization are required before U.S. indus- craft propuIsion and for utiIity-scale power gen- try will invest large sums in the needed research. eration, shouId also be categorized as far-term. In the meantime, government funding will be re- In general, the risks are perceived by U.S. indus- quired to supplement industry R&D in order to try to be too high to justify funding the needed 12 ● Advanced Materials by Design research. Advances in these applications are annually for the remainder of the century, in- likely to be driven by government funding. creasing from a 1985 value of $1.4 billion to nearly $12 billion by the year 2000. The indus- Polymer Matrix Composites try continues to be driven by aerospace markets, with defense applications projected to grow by PMCs consist of high strength short or contin- as much as 22 percent annually in the next few uous fibers which are held together by a com- years. mon organic matrix. The composite is designed so that the mechanical loads to which the struc- Current Production ture is subjected in service are supported by the fiber reinforcement. Aerospace applications of polymer composites account for about 50 percent of current PMC PMCs are often divided into two categories: sales in the United States. Sporting goods, such reinforced plastics and so-called “advanced com- as golf clubs and tennis rackets, account for 25 posites. ” The distinction is based on the level of percent. The PMC sporting goods market is con- mechanical properties (usually strength and stiff- sidered mature, however, with projected annual ness); however, there is no clear-cut line sepa- growth rates of only 3 percent. Automobiles and rating the two. Plastics reinforced with relatively industrial equipment round out the current list low-stiffness glass fibers are inexpensive, and they of major uses of advanced composites, with a 25 have been in use for 30 to 40 years in applica- percent share. tions such as boat hulls, corrugated sheet, pipe, automotive panels, and sporting goods. Ad- Near-Term Production vanced composites, which are used primarily in the aerospace industry, have superior strength Advanced PMCs were introduced into the hori- and stiffness. They are relatively expensive and zontal stabilizer of the F-14 fighter in 1970, and typically contain a large percentage of high- they have since become the baseline materials performance continuous fibers (e.g., high stiffness in high-performance fighter and attack aircraft. glass, graphite, aramid, or other organic fibers). The major near-term challenge for composites In this assessment, only market opportunities for will be use in large military and commercial trans- advanced composites are considered. port aircraft. Advanced PMCs currently comprise about 3 percent of the structural weight of com- Chief among the advantages of PMCs is their mercial aircraft such as the Boeing 757, but that light weight coupled with high stiffness and fraction could eventually rise to more than 65 per- strength along the direction of reinforcement. cent in new transport designs. Other desirable properties include superior re- sistance to corrosion and fatigue. One generic The single largest near-term opportunity for limitation of PMCs is temperature. An upper limit PMCs is in the manufacture of automobiles. Com- for service temperatures with present composites posites currently are in limited production in is about 600° F (316 o C). With additional devel- body panels, drive shafts, and leaf springs. By the opment, however, temperatures near 800° F late 1990s, composite automobile bodies could (427° C) may be achieved. be introduced by Detroit in limited production. The principal advantage of a composite body Market Opportunities for would be the potential for parts consolidation, Polymer Matrix Composites which could result in lower assembly costs. Com- posites can also accommodate styling changes About 85 percent of PMCs used today are glass with lower retooling costs than wouId be possi- fiber-reinforced polyester resins. Currently, less ble with metals. than 2 percent of PMCs are advanced compos- ites such as those used in aircraft and aerospace Additional near-term markets for polymer com- applications. However, U.S. production of ad- posites include medical implants, reciprocating vanced PMCs is projected to grow by 15 percent industrial machinery, storage and transportation Ch. 1—Executive Summary ● 13 of corrosive chemicals, and military vehicles and temperature window in which MMCs have an weapons. advantage. Also, because the density of the metal matrix is higher than that of a polymer matrix, Far-Term Production the strength-to-weight ratio of MMCs is generally less than that of PMCs (figure 1-4). Beyond the turn of the century, PMCs could be used extensively in construction applications A second source of uncertainty relates to cost. such as bridges, buildings, manufactured hous- MMCs tend to cluster around two extreme types: ing, and marine structures where salt water cor- one type consists of high-performance compos- rosion is a problem. Realization of this potential ites reinforced with expensive continuous fibers will depend on development of cheaper materi- and requiring expensive processing methods; the als, changes in building codes, and of designs that other consists of relatively low-cost, low-perform- take advantage of compounding benefits of PMCs, ance composites reinforced with relatively inex- such as reduced weight and increased durabil- pensive particulate and fibers. The cost of the ity. I n space, a variety of composites will be used first type is too high for any but military or space in the proposed National Aerospace Plane, and applications, whereas the cost/benefit advantages they are also being considered for the tubular of the second type over metal alloys remain in frame of the National Aeronautics and Space Ad- doubt. ministration’s (NASA) space station. Composites of all kinds, including MMCs, PMCs, and CMCs would be a central feature of space-based weap- ons systems, such as those under consideration for ballistic missile defense. Metal Matrix Composites MMCs usually consist of a low-density metal such as aluminum or magnesium reinforced with particulate or fibers of a ceramic material, such as silicon carbide or graphite. Compared with the unreinforced metal, MMCs have significantly greater stiffness and strength, as indicated in fig- ure 1 -4; however, these properties are obtained at the cost of lower ductility and toughness. Market Opportunities for Metal Matrix Composites At present, metal matrix composites remain pri- marily materials of military interest in the United States, because only the Department of Defense’s (DoD) high-performance specifications have justi- fied the materials’ high costs. The future commer- cial markets for MMCs remain uncertain for two reasons. First, their physical and mechanical properties rarely exceed those of PMCs or CMCs. For example, the melting point of the metal ma- trix keeps the maximum operating temperature for MMC components to a level significantly be- Photo credit United Technologies Research Center low that of ceramics; as new high-temperature Fracture surface of boron fiber-reinforced aluminum PMCs are developed, this squeezes further the metal matrix composite. 14 ● Advanced Materials by Design Thus, it is unclear whether MMCs will become The most significant commercial application of the materials of choice for a wide variety of ap- MMCs to date is an aluminum diesel engine pis- plications or whether they will be confined to ton produced by Toyota that is locally reinforced specialty niches in which the combinations of with ceramic fibers. Toyota produces about properties required cannot be satisfied by other 300,000 annually. The ceramic reinforcement materials. The key factors will be whether the provides superior wear resistance in the ring costs of the reinforcements and of the manufac- groove area. Although data on the production turing processes can be reduced while the prop- costs of these pistons are not available, this de- erties are improved. Costs could be reduced sub- velopment is significant because it suggests that stantially if net-shape processes currently used MMC components can be reliably mass-produced with metals, such as casting or powder tech- to be competitive in a very cost-sensitive appli- niques, can be successfully adapted to MMCs. cation. Current Production Current markets for MMCs are primarily in mil- Future Production itary and aerospace applications. Experimental Based on information now in the public do- MMC components have been developed for use main, the following military and aerospace ap- in aircraft, jet engines, missiles, and the NASA plications for MMCs appear attractive: high-tem- space shuttle. The first production application of perature fighter aircraft engines and structures; a particulate-reinforced MMC is a set of covers the National Aerospace Plane skin and engines; for a missile guidance system. high-temperature missile structures; high-speed mechanical systems, and electronic packaging. Applications that could become commercial in the next 5 to 15 years include automotive pistons, brake components, connecting rods, and rocker arms; rotating machinery, such as propeller shafts and robot components; computer equipment, prosthetics, electronic packaging, and sporting goods. However, the current level of develop- ment effort appears to be insufficient to bring about commercialization of any of these appli- cations in the United States in the next 5 years, with the possible exception of diesel engine pistons, MMC materials with high specific stiffness and strength could be used in applications in which an important factor is reducing weight. Included in this category are land-based vehicles, aircraft, ships, and high-speed machinery. The relatively high cost of MMCs will probably prevent their extensive use in commercial land-based vehicles and ship structures. However, they may well be used in specific mechanical components such as Photo credit: Toyota Motor Corp. propeller shafts, bearings, pumps, transmission Aluminum diesel engine piston with local fiber housings and components, gears, springs, and reinforcement in ring groove area. suspensions. Ch. 1—Executive Summary ● 15 Research and Development Priorities are more complex than metals, the relationships among the internal structure, mechanical prop- In spite of the fact that ceramics, PMCs, and erties, and failure mechanisms are less well un- MMCs are at different stages of technological derstood. A better understanding of the effects maturity, the R&D challenges for all three cate- of an accumulation of dispersed damages on the gories are remarkably similar. The four most im- failure mechanisms of composites is especially portant R&D priorities are given below. desirable. Processing Science Behavior in Severe Environments This is the key to understanding how process- Many applications may require new materials ing variables such as temperature, pressure, and to withstand high-temperature, corrosive, or ero- composition influence the desired final proper- sive environments. These environments may ex- ties. The two principal goals of processing science acerbate existing flaws or introduce new flaws, should be to support development of new, low- leading to failure. Progress in this area would fa- cost manufacturing methods, and to help bring cilitate reliable design and life prediction. about better control over reproducibility so that large numbers of components can be manufac- Matrix= Reinforcement Interface tured within specification limits. in Composites The poorly understood interracial region has Structure-Property Relationships a critical influence on composite behavior. Par- The tailorable properties of advanced materi- ticularly important would be the development of als offer new opportunities for the designer. How- interracial coatings that would permit the use of ever, because advanced materials and structures a single fiber with a variety of matrices. FACTORS AFFECTING THE USE OF ADVANCED MATERIALS Broader use of advanced structural materials materials. Accordingly, it becomes essential to will require not only solutions to technical prob- have a design process capable of producing lems, but also changes in attitudes among re- highly integrated and multifunctional structures. searchers and end users who are accustomed to Consider the body structure of an automobile. thinking in concepts more appropriate to con- A metal body currently has between 250 and 350 ventional materials. distinct parts. Using PMCs, this number could be reduced to between 2 and 10. Traditionally, materials are considered to be one (usually inexpensive) input in a long chain Because composites can be tailored in so many of discrete design and manufacturing steps that ways to the various requirements of a particuIar result in the output of a product. The new tai- engineering component, the key to optimizing lored materials require a new paradigm. The ma- cost and performance is a fully integrated design terials and the end products made from them be- process capable of balancing all of the relevant come indistinguishable, joined by an integrated design and manufacturing variables. Such a de- design and manufacturing process. This neces- sign process requires an extensive database on sitates a closer relationship among researchers, matrix and fiber properties, sophisticated software designers, and production personnel, as well as capable of modeling fabrication processes, and new approaches to the concept of materials costs. three-dimensional analysis of the properties and Integrated Design and Manufacturing behavior of the resulting structure. Perhaps the most important element in the development of Advanced ceramics and composites should integrated design algorithms will be an under- really be considered as structures rather than as standing of the relationships among the constit- 16 ● Advanced Materials by Design uent properties, microstructure, and the macro- scopic properties of the structure. The R&D priorities listed above are intended to provide this information. Automation The need for integrated design and manufac- turing sheds light on the extent to which auto- mation will be able to reduce the costs of ad- vanced materials and structures. Automation can be used for many purposes in advanced materi- als manufacturing, including design, numerical modeling, materials handling, process controls, Photo credit: Cincinnati Milacron Co. assembly, and finishing. Automation technologies Composite tape-laying machine shown applying 3-inch- that aid in integrating design and manufacturing wide tape to compound-angle “tool” in the will be helpful. For example, computer-aided de- manufacture of an aircraft part. sign (CAD) and numerical modeling are likely to help bring the designer and production engineer in closer contact. typical ceramic component, an industry team Automation in the form of computer control could include one or more professionals from of advanced materials processing equipment is each of the disciplines in table 1-2. an important evolving technology for solving cur- rent manufacturing problems. In ceramics, new Education and Training processes controlled by microprocessors or com- puters will be critical in minimizing flaw popu- The expanding market opportunities for cer- lations and increasing process yields. In PMCs, amics and composites will require more scien- the costly process of hand lay-up will be replaced tists and engineers with broad backgrounds in by computer-controlled tape laying machines and these fields. At present, only a few universities filament winding systems. However, large-scale offer comprehensive courses in ceramic or com- process automation will be effective in reducing posite materials. There is also a shortage of prop- costs only if the process is well characterized and the allowable limits for processing variables are well understood. In general, manufacturing proc- Table 1-2.—Hypothetical Multidisciplinary Design esses for advanced materials are still evolving, and Team for a Ceramic Component attempts to automate them in the near term could Specialist Contribution be premature. Systems engineer ...... Defines performance Designer ...... Develops structural concepts Multidisciplinary Approach Stress analyst ...... Determines stress for local environments and difficult shapes Advanced materials development lends itself Metallurgist...... Correlates design with metallic naturally to—and probably will demand—relaxing properties and environments the rigid disciplinary boundaries among different Ceramist ...... Identifies proper composition, reactions, and behavior for fields. This is true whether the materials devel- design opment is performed in government laboratories, Characterization analyst . . Utilizes electron microscopy, universities, or industry. For example, the neces- X-ray, fracture analysis, etc. to characterize material sity for integrating design and manufacturing of Ceramic manufacturer . . . Defines production feasibility advanced materials and structures implies closer and costs working relationships among industry profession- SOURCE: J.J. Mecholsky, “Engineering Research Needs of Advanced Ceramics and Ceramic Matrix Composites,” contractor report for OTA, Decem- als involved in manufacturing a product. For a ber 1985. Ch. 1—Executive Summary ● 17 erly trained faculty members to teach such costs less than $20, and new processes based on courses. The job market for graduates with ad- synthesis from petroleum pitch promise to reduce vanced degrees in ceramic or composite engi- the cost even further. However, these advanced neering is good, and can be expected to expand materials will always be more expensive than i n the future. Stronger relationships between in- basic metals. Therefore, end users must take dustry and university laboratories are providing advantage of potential savings in fabrication, in- greater educational and job opportunities for stallation, and life-cycle costs to offset the higher students. material costs; in other words, a systems ap- proach to costs is required. There is a great need for continuing education and training opportunities for designers and engi- As the example of the PMC automobile body neers in industry who are unfamiliar with the new cited above demonstrates, savings in tooling, as- materials. I n the field of PMCs, for instance, most sembly, and maintenance costs could result in of the design expertise is concentrated in the lower cost, longer lasting cars in the future. aerospace industry. Small businesses, professional Viewed from this systems perspective, advanced societies, universities, and Federal laboratories materials may become more cost-effective than could all play a role in providing this training. conventional materials in many applications. Continuing education regarding the potential of advanced materials is particularly important in relatively low-technology industries such as con- Energy Costs struction, which must purchase, rather than de- velop, the materials they use. The cost of energy used in the manufacture of advanced materials and structures is generally only 1 to 2 percent of the cost of the finished Beyond the training of professionals, there is product. However, the energy cost savings ob- a need for the creation of awareness of advanced tained over the service life of the product is a materials technologies among corporate execu- major potential advantage of using the new ma- tives, planners, technical media personnel, and terials. For example, the high temperature capa- the general public. In recent years, the number bilities of ceramics can be used to increase the of newspaper and magazine articles about the thermal efficiency of heat engines, heat ex- remarkable properties of ceramics and compos- changers, and furnace recuperators. Fuel savings ites has increased, as has the number of techni- also result from reducing the weight of ground cal journals associated with these materials. The vehicles and aircraft through the use of light- success of composite sports equipment, includ- weight composites. ing skis and tennis rackets, shows that such ma- terials can have a high-tech appeal to the pub- lic, even if they are relatively expensive. The decline of fuel prices in recent years has reduced energy cost savings as a selling point for new products, and has therefore reduced the at- Systems Approach to Costs tractiveness of new materials. For example, in the early 1980s one pound of weight saved in a com- Without question, the high cost per pound of mercial transport aircraft was worth $300 in fuel advanced materials will have to come down be- savings over the life of the aircraft, but is now fore they will be widely used in high-volume, low- worth less than $100. At $300 per pound of cost applications. This high cost is largely at- weight saved, the higher cost of using compos- tributable to the immaturity of the fabrication ites could be justified; at a premium of only $100 technology and to low production volumes, and per pound, aluminum or aluminum-lithium al- can be expected to drop significantly in the fu- loys are more attractive. Persistently low fuel ture. For example, a pound of standard high- prices would delay the introduction of advanced strength carbon fiber used to cost $300, but now materials into such applications. 18 ● Advanced Materials by Design IMPACTS OF ADVANCED MATERIALS ON MANUFACTURING The advent of advanced structural materials are willing to employ advanced materials more raises questions concerning their impact on ex- aggressively in the near term, thereby gaining pro- isting manufacturing industries in the United duction experience. States. This impact can be conceptually divided It is sometimes suggested that substitution of into two categories: substitution by direct replace- advanced materials for steel and aluminum will ment of metal components i n existing products, soon become a significant factor affecting the de- and use in new products that are made possible mand for these metals. OTA’s analysis indicates by the new materials. Compared with other sup- that this is highly unlikely. Because of their low ply and demand factors affecting basic metals cost and manufacturability, these metals are manufacturing, the impact of direct substitution ideally suited for many of the applications in of advanced materials for these metals is likely which they are now used, and will not be re- to be relatively minor. In contrast, more innova- placed by advanced materials. Moreover, the tive application of the materials to new or re- threat of substitution has led to the development designed products could have substantial impact of new alloys with improved properties, such as on manufacturing industries, including develop- high-strength, low-alloy steel and aluminum- ment of more competitive products, and new in- Iithium. The availability of these and other new dustries and employment opportunities, as de- alloys wiII make it even more difficuIt for new, scribed below. nonmetallic materials to substitute for metals. As new materials technologies mature and costs Substitution come down, significant displacement of metals From the viewpoint of the commercial end user could occur in four markets: aircraft, automo- considering the introduction of a new material biles, containers, and construction. However, in into an existing product, the material must per- those applications where substitution is substantial, form at least as well as the existing material, and by far the greatest volume of steel and aluminum do so at a lower cost. This cost is generally cal- will be displaced by relatively low-performance, culated on the basis of direct substitution of the low-cost materials, such as unreinforced plastics, new material for the old material in a particular sheet molding compounds, and high-strength component, without redesign or modification of concrete. surrounding components. in fact, if substantial redesign is necessary, this is likely to be consid- Innovative Designs and New Products ered a significant disincentive for the substitution. The automotive industry provides an excellent Generally, advanced materials cannot compete paradigm for understanding the potential impact with conventional materials on a dollars-per- of using advanced materials in cost-sensitive man- pound substitution basis. Direct substitution of ufacturing applications. Design teams at the ma- a ceramic or composite part for a metal part does jor automakers are currently evaluating the use not exploit the superior properties and design of PMCs in primary body structures and chas- flexibility inherent in advanced materials, key ad- sis/suspension systems, as illustrated in figure 1-6. vantages which can offset their higher cost. Yet The potential advantages of using PMCs include: direct substitution is frequently the only option weight reduction and resulting fuel economy; im- considered by end users, who are wary of mak- proved overall quality and consistency in man- ing too many changes at once. This Catch-22 sit- ufacturing; lower assembly costs due to parts con- uation is a major barrier to the use of advanced solidation; improved ride performance; product materials in large volume applications. However, differentiation at a reduced cost; lower invest- commercial end users who wish to exploit the ment costs for plant, facilities, and tooling; im- long-term opportunities offered by advanced ma- proved corrosion resistance; and lower operat- terials may fail to achieve their goal unless they ing costs. These advantages reflect a systems Ch. 1—Executive Summary ● 19 Figure 1-6.—TypicaI Body Construction Assembly Large-scale adoption of PMC automotive struc- Using Two Major PMC Moldings tures would have a major impact on the fabrica- tion and assembly of automobiles. For instance, metal forming presses would be replaced by a much smaller number of molding units, the cur- rent large number of welding machines would be replaced by a limited number of adhesive bonding fixtures, and the assembly sequence wouId be modified to reflect the tremendous re- duction in parts. Factories would be smaller be- cause fewer assembly machines require less floor space. The overall labor content of producing a PMC automobile body would be reduced as numer- ous operations would be eliminated. However, \ it is important to note that body assembly is not a labor-intensive segment of total assembly. Other SOURCE P. Beardmore, C F Johnson, and G G Strosberg, Ford Motor Co , “Im- pact of New Materials on Basic Manufacturing Industries: Case Study assembly operations that are more labor-intensive Composite Automobile Structure,” contractor report for OTA, March 1987 (e.g., trim) would not be significantly affected. Thus, the overall decreases in direct labor due to adoption of PMCs may be relatively small. The approach to costs, as described above. However, kinds of skills required of factory personnel would major challenges remain that will require exten- be somewhat different, and significant retraining sive R&D to resolve. These include: lack of high- would be necessary. However, the overall skill speed, high-quality, low-cost manufacturing proc- levels required are likely to be similar to those esses; uncertainties regarding performance re- in use today. quirements, particularly crash integrity and long- Extensive use of PMCs by the automotive in- term durability; lack of adequate technologies for dustry would cause completely new industries to repair and recycling of PMC structures; and un- arise, including a comprehensive network of PMC certain customer acceptance. repair facilities, molding and adhesive bonding There is a growing body of evidence that glass equipment suppliers, and a recycling industry fiber-reinforced composites are capable of meet- based on new technologies. Current steel vehi- ing the functional requirements of the most highly cle recycling techniques will not be applicable loaded automotive structures. However, major to PMCs, and cost-effective recycling technol- innovations in fabrication technologies are still ogies for PMCs have yet to be developed. With- required. There are several candidate fabrication out the development of new recycling methods, methods, including resin transfer molding, com- incineration could become the main disposal pression molding, and filament winding. At this process for PMC structures. The lack of accept- time, none of these methods can satisfy all of the able recycling and disposal technologies could production requirements; however, resin trans- translate into higher costs for PMC structures rela- fer molding seems the most promising. tive to metals. INDUSTRY INVESTMENT CRITERIA FOR ADVANCED MATERIALS The potential for advanced materials in the investment criteria used by advanced materials manufacturing sector will not be realized unless companies vary depending on whether they are companies perceive that their criteria for invest- materials suppliers or users; whether the intended ment in R&D and production will be met. The markets are military or commercial; and whether 20 “ Advanced Materials by Design the end use emphasizes high materials perform- Figure 1-7 provides a schematic view of the ance or low cost. relative importance placed on high materials per- formance versus cost in a spectrum of industrial Suppliers of advanced structural materials tend end uses. in commercial aircraft, automotive, and to be technology-driven; they are focused primar- construction markets, acquisition costs and oper- ily on the superior technical performance of ad- ating expenses are the major purchase criteria, vanced materials and are looking for both mili- with progressively less emphasis on high mate- tary and commercial applications. Suppliers tend rial performance. In military aerospace and bio- to take a long-term view, basing investment de- medical markets, functional capabilities and per- cisions on qualitative assessments of the techni- formance characteristics are the primary purchase cal potential of advanced materials. On the other criteria. hand, users of advanced materials tend to be market-driven; they are focused primarily on Because advanced materials may cost as much short-term market requirements, such as return as 100 times more on a per-pound basis than me- on investment and time to market. tals such as steel and aluminum, their first use has generally been in the less cost-sensitive end Frequently, advanced materials suppliers and uses of figure 1-7, particularly in the military. users operate in both military and commercial However, because military production runs are markets. However, the investment criteria em- typically small, there is little incentive to develop ployed in the two cases are very different. De- low-cost, mass production manufacturing proc- fense contractors are able to take a longer term esses that would make the materials more attrac- perspective because they are able to charge tive for commercial applications such as automo- much of their capital equipment to the govern- biles. The lack of such processes is a major barrier ment, and because the defense market for the preventing more widespread commercial use of materials and structures is well-defined. Commer- advanced structural materials. This suggests that cial end users, on the other hand, must bear the greater emphasis on military R&D programs to full costs of their production investments, and develop low-cost fabrication techniques could fa- face uncertain returns. Their outlook is therefore cilitate the diffusion of military materials technol- necessarily shorter term. This difference in mar- ogy into the commercial sector. ket perspective has hampered the transfer of tech- The major potential sales value of advanced nology from advanced materials suppliers (who materials lies in the commercial industries in the frequently depend on defense contracts to stay middle of figure 1-7; i.e., in aircraft, automobiles, in business) to commercial users, and it under- industrial machinery, etc. This is because con- lines the importance of well-defined markets as struction materials are used in high volume but a motivating force for industry investments in ad- must have a very low cost, and military and bio- vanced materials. medical materials can have high allowable costs, Figure 1-7.—Relative Importance of Cost and Cost and Performance Performance In Advanced Materials User Industries The many applications of advanced structural materials do not all have the same cost and per- I formance requirements. Accordingly, the invest- Emphasis ment criteria of user companies specializing in on cost different product areas are different. In general, I barriers to investment are highest in cost-sensitive i I areas such as construction and automobiles, I I wherein expensive new materials must compete with cheap, well-established conventional mate- Barriers to the use of advanced materials decrease from upper rials. Barriers are lowest for applications in which left to lower right. a high materials cost is justified by superior per- SOURCE: Technology Management Associates, “industrial Criteria for invest- ment Decisions in R&D and Production Facilities,” contractor report formance, such as medical implants and aircraft. for OTA, January 1987. Ch. 1—Executive Summary . 21 but are used in relatively low volume. However, no market pull on these technologies in the end users in these “middle” industries do not per- United States. This suggests that an important pol- ceive that use of the new materials will be profit- icy tool for accelerating the commercialization able within the next 5 years, the planning hori- of advanced materials is to increase incentives zon of most companies. Thus, there is virtually for investment by commercial end users. INTERNATIONAL BUSINESS TRENDS Advanced structural materials industries have 1-3. (U.S. production data were not available.) become markedly more international in charac- In each geographic region, electronic applica- ter in the past several years. In collaboration with tions, such as capacitors, substrates, and in- industry, governments around the world are in- tegrated circuit packages, accounted for over 80 vesting large sums in multi-year programs to fa- percent of the total. Structural applications, in- cilitate commercial development. Through acqui- cluding wear parts and cutting tool inserts, ac- sitions, joint ventures, and licensing agreements, counted for the remainder. the firms involved have become increasingly mul- By a margin of nearly 2 to 1, the U.S. ceramics tinational, and are thereby able to obtain access companies interviewed by OTA felt that Japan is to growing markets and achieve lower produc- the world leader in advanced ceramics R&D. tion costs. Critical technological advances con- Without question, Japan has been the leader in tinue to be made outside the United States; e.g., actually producing advanced ceramic products the carbon fiber technology developed in Great for both industrial and consumer use. Japanese Britain and Japan, and hot isostatic pressing tech- end users exhibit a commitment to the use of nology developed in Sweden. these materials not found in the United States. This trend toward internationalization of ad- This commitment is reflected in the fact that vanced structural materials technologies has although the U.S. and Japanese Governments many important consequences for government spend comparable amounts on ceramics R&D and industry policy makers in the United States. (roughly $100 to$125 million in fiscal year 1985, They can no longer assume that the United States see table 1-4), estimated spending by Japanese will dominate the technologies and the resultant industry is about four times that of its government, applications. The flow of technology coming into while in the United States, industry investment the United States from abroad may soon be just in advanced ceramics R&D (estimated at $153 as significant as that flowing out. Moreover, the million in fiscal year 1986) is only slightly higher increasingly muItinational character of materials than government spending. Ceramics technology industries suggests that the rate of technology has a high profile in Japan, due in part to pro- flow among firms and countries is likely to in- duction of advanced ceramic consumer goods, crease. The United States will not be able to rely such as fish hooks, pliers, scissors, and ballpoint on a superior R&D capability to provide an pen tips. advantage in developing commercial products. Furthermore, if there is no existing infrastructure in the United States for quickly appropriating the Table l-3.—Estimated Production Value of Advanced Ceramics, 1985 (millions of dollars) R&D results for economic development, the re- sults will quickly be used elsewhere. Electronic Structural Region applications applications Total Japan...... 1,920 360 2,280 Ceramics United Statesa ...... 1,763 112 1,875 Western Europe ...... 390 80 470 The value of advanced ceramics consumed in aConsumptlon in 1985, according to Business Communications Co., Inc., Nor- the United States, and produced in Japan and walk, CT. SOURCE: Strategic Analysis, Inc., “Strategies of Suppliers and Users of Advanced Western Europe in 1985 are estimated in table Materials,” contractor report for OTA, March 1987. 22 “ Advanced Materials by Design Table l-4.—Estimated Government Funding tween 1987 and 1991. Overall, industry invest- in Several Countries for Advanced Ceramics R&D ment in advanced ceramics in Western Europe a b in 1985 (millions of dollars) is thought to be roughly in the same proportion United States ...... $125 to government spending as in the United States, Japan ...... 100 i.e., far less than in Japan. Western Europe ap- West Germany ...... 75 pears to have all of the necessary ingredients for France ...... 64 United Kingdom ...... 51 developing its own structural ceramics industry. Sweden ...... 7 Italy ...... 6 Polymer Matrix Composites Finland ...... 5 The Netherlands ...... 4 Belgium ...... 1.5 The value of advanced PMC components pro- Other ...... 3 duced in the United States, Western Europe, and alncludes funding for electronic and structural applications. Japan in 1985 was $2.1 billion, divided roughly blnclides government funding for materials, office expenses (e.g. salaries) and facilities in research centers, universities, and private industry. as follows: the United States, $1.3 billion; West- clncludes Denmark, Ireland, Norway, and Switzerland. ern Europe, $600 million; and Japan, $200 mil- SOURCE: Strategic Analysis, lnc., ’’Strategies of Suppliers and Users of Advanced Materials,” contractor report for OTA, March 1987. lion. As shown in table 1-5, the U.S. and European markets are dominated by aerospace applica- tions. In the United States, PMC development is Japanese ceramics companies are far more ver- being driven by military and space programs, tically and horizontally integrated than U.S. corn- whereas in Western Europe development is be- panies, a fact that probably enhances their abil- ing keyed more heavily to commercial aircraft ity to produce higher quality ceramic parts at use. In contrast, the Japanese market is domi- lower prices. However these companies are still nated by sporting goods applications. Iosing money on the structural ceramic parts they produce. This reflects the long-term view of Jap- On the strength of its military aircraft and aero- anese companies regarding the future of ceramics space programs, the United States leads the world technologies. in advanced PMC technology. Due to the attrac- tiveness of PMCs for new weapons programs, the The Japanese market for advanced structural military fraction of the market is likely to increase ceramics is likely to develop before the U.S. mar- in the near term. However, this military technol- ket. However, given the self-sufficiency of the Jap- ogy leadership will not necessarily be translated anese ceramics industry, this market is likely to into a strong domestic commercial industry. Due be difficult to penetrate by U.S. suppliers. In con- to the high cost of such military materials and trast, Japanese ceramics firms, which already structures, they find relatively little use in com- dominate the world market for electronic ceram- mercial applications. ics, are strongly positioned to exploit the U.S. structural ceramics market as it develops. One Commercialization of advanced PMCs is an such firm, Kyocera, the largest and most highly area in which the United States remains vulner- integrated ceramics firm in the world, has already able to competition from abroad. U.S. suppliers established subsidiaries and, recently, an R&D center in the United States. Table 1-5.—Breakdown of Regional Markets for Advanced Composites by End Use West Germany, France, and the United King- dom all have initiated substantial programs in ad- End use (percentage)a vanced ceramics R&D, as indicated in table 1-4. Region Aerospace Industrialb Recreational West German companies have a strong position United States . . . . . 50 25 25 in powders and finished products, whereas Western Europe . . . 56 26 18 Japan ...... 10 35 55 a France has developed a strong capability in Based on the value of fabricated components. CMCs. Meanwhile, the European Community blncludes automotive, medical, construction, and non-aerospace military appli- (EC) has earmarked about $220 million for R&D cations. SOURCE: Strategic Analysis, Inc., “Strategies of Suppliers and Users of Advanced on advanced materials (including ceramics) be- Materials,” contractor report for OTA, March 1987. Ch. 1—Executive Summary ● 23 of PMC materials report that foreign commercial business. A secondary benefit for the European end users (particularly those outside the aero- companies is likely to be a transfer of U.S. PMC space industry) are more active in experimenting technology to Europe such that in the future, Eur- with the new materials than are U.S. commer- ope will be less dependent on the United States cial end users. For example, Europe is considered for this technology. to lead the world in composite medical devices. Although Japan is the world’s largest producer It should be noted, however, that the regulatory of carbon fiber, a key ingredient in advanced environment controlling the use of new materi- composites, it has been only a minor participant als in the human body is currently less restric- to date in the advanced composites business. tive in Europe than in the United States. One reason for this is that Japan has not devel- France is by far the dominant force in PMCs oped a domestic aircraft industry, the sector that in Western Europe, producing more than all other currently uses the largest quantities of advanced European countries combined, as shown in ta- composites. Another reason is that Japanese com- ble 1-6. The United Kingdom, West Germany, panies have been limited by licensing agreements and Italy make up the balance. The commercial from participating directly in the U.S. market. aircraft manufacturer Airbus Industrie, a consor- tium of European companies, is the single largest Few observers of the composites industry ex- consumer of PMCs. At the European Community pect this situation to continue. Change could level, significant expenditures are being made to come from at least two directions. First, Japanese facilitate the introduction of PMCs into commer- fiber producers could abrogate existing agree- cial applications through the BRITE and EURAM ments and sell their product directly in the U.S. programs. In addition, the EUREKA program market. Second, based on technology gained called Carmat 2000 has proposed to spend $60 through their increasing involvement in joint ven- million over 4 years to develop PMC automobile tures with Boeing, Japan could launch its own structures. commercial aircraft industry. In the past few years, the participation of West- Metal Matrix Composites ern European companies in the U.S. PMC mar- The principal markets for MMC materials in the ket has increased dramatically. This has occurred United States and Western Europe are in the de- primarily through their acquisitions of U.S. com- fense and aerospace sectors. Accordingly, over panies. One result is that they now control 25 90 percent of the U.S. funding for MMC R&D be- percent of resins, 20 percent of carbon fibers, and tween 1979 and 1986 came from DoD. The struc- 50 percent of prepreg (fibers pre-impregnated tures of the U.S. and European MMC industries with polymer resin, the starting point for many are similar, with small, undercapitalized firms fabrication processes) sales in the United States. supplying the formulated MMC materials. Cur- These acquisitions appear to reflect their desire rently, the matrix is supplied by the large alumi- to participate more directly in the U.S. defense num companies, which are considering forward market and to establish a diversified, worldwide integration into composite materials. There are also in-house efforts at the major aircraft com- panies to develop new composites and new proc- Table l-6.–Distribution of Advanced PMC essing methods. Many analysts feel that the inte- Business in Western Europe, 1986 gration of the MMC suppliers into larger concerns Country Percent of total having access to more capital and R&D resources France ...... 55% will be a critical step in producing reliable, low- United Kingdom ...... 15 cost MMCs that could be used in large-volume West Germany ...... 10 commercial applications. Italy ...... 10 All other ...... 10 A potential barrier to the commercial use of Total ...... 100% MMCs in the United States arises from restrictions SOURCE Strategic Analys!s Inc , “Strategies of Suppliers and Users of Advanced Materials contractor report for OTA, March 1987 imposed on the flow of information about MMCs 24 . Advanced Materials by Design for national security reasons. Because MMCs are nies. Another difference is that the Japanese MMC classified as a technology of key military impor- suppliers focus primarily on commercial appli- tance, exchanges of technical data on MMCs are cations, including electronics, automobiles, and severely restricted in the United States and ex- aircraft and aerospace. One noteworthy Japanese ports of data and material are closely controlled. development is Toyota’s introduction of an MMC diesel engine piston consisting of aluminum lo- Unlike the situation in the United States and cally reinforced with ceramic fibers. This is an im- Western Europe, the companies involved in man- portant harbinger of the use of MMCs in low-cost, ufacturing MMCs in Japan are largely the same high-volume applications, and it has stirred con- as those involved in supplying PMCs and ceram- siderable worldwide interest among potential ics; i.e., the large, integrated materials compa- commercial users of MMCs. GOVERNMENT/UNIVERSITY/lNDUSTRY COLLABORATION AND INDUSTRIAL COMPETITIVENESS Through the years, the United States has built they do not systematically track commercial out- up a strong materials science base in its univer- comes. Many of the university-based programs sities and Federal laboratories. Many observers concentrate on publishable research and gradu- believe that U.S. industry, universities, and Fed- ate training. Those programs based at Federal fa- eral laboratories need to work together more cilities are only now beginning to move away effectively to translate this research base into from their primary agency missions toward a competitive commercial products. Collaborative broader concern with U.S. industrial competitive- programs offer a number of potential contribu- ness. Generally, industrial participants value their tions to U.S. industrial competitiveness, includ- access to skilled research personnel and graduate ing an excellent environment for training stu- students more highly than the actual research re- dents, an opportunity to leverage stakeholder sults generated by the collaboration. This strongly R&D investments, and research results that could suggests that such collaborative programs should lead to new products. not be viewed as engines of commercialization and jobs, but rather as a form of infrastructure Since the early 1980s, numerous collaborative support, providing industry with access to new R&D centers have been initiated. These centers ideas and trained personnel. follow a variety of institutional models, includ- ing industry consortia, university-based consor- Industrial participants often have only a mod- tia such as the National Science Foundation’s est amount of involvement in the planning and Engineering Research Centers, quasi-independent operation of the collaborative programs. For the institutes (often funded by State government most part, they approach their relationship with sources), and Federal laboratory/industry programs. research organizations as being a “window to the future.” Furthermore, “collaboration” may be an In advanced materials technologies, most cur- inaccurate description of many of the programs. rent collaborative programs are based at univer- In large measure, the programs studied by OTA sities or Federal laboratories. OTA’s survey of a did not involve intense, bench-level interaction sample of these programs suggests that such pro- between institutional and industrial scientists; grams are more successful in training students rather, the nature of the collaboration seemed and leveraging R&D investments than they are to be mostly symbolic. in stimulating commercial outcomes. There are exceptions to these general obser- The collaborative research programs and their vations in some of the newer “hybrid” initiatives, industrial participants surveyed by OTA do not which combine both generic and proprietary re- rank commercialization as a high priority, and search in the same program. Often undertaken Ch. 1—Executive Summary . 25 in conjunction with State government funding, Rather, they saw the principal barriers as being these hybrid organizations seem to incorporate internal corporate problems: how companies can a greater commitment to commercialization and justify major investments in new manufacturing economic development as their mission. facilities in light of uncertain markets, how to adopt longer term planning horizons, and how For the results of collaborative research to be to facilitate better communication between their commercialized, there must be a corresponding R&D and manufacturing functions. capacity and incentive on the part of the indus- trial participants to do so. Fewer than 50 percent Thus, there appears to be a significant gap be- of the industrial participants interviewed reported tween the point at which government/univer- any follow-on work stimulated by the collabora- sity/industry collaborative materials research tions. Overwhelmingly, OTA’s industrial respond- leaves off and the point at which industry is will- ents did not feel that changes in institutional ar- ing to begin to explore the commercial poten- rangements with the research performing centers tial. Policy options that could help bridge this gap would facilitate the commercialization process. are discussed in the policy section below. MILITARY ROLE IN ADVANCED MATERIALS DEVELOPMENT Just as universities and Federal laboratories rep- als is expected to grow rapidly. DoD has com- resent unique resources available to U.S. ad- mitted itself to purchase 80 billion dollars’ worth vanced materials companies, the substantial DoD of weapons systems that will incorporate ad- and NASA investments in advanced materials for vanced composite components. military and space applications can also contrib- Composites have already been used in the ute to the commercial competitiveness of U.S. Army’s Apache and Black Hawk helicopters, firms. Navy aircraft such as the AV-8B, the F-18, and At present, the military establishment is one of the F-14, and the Air Force’s F-1 5 and F-16. PMCs the largest customers of advanced materials, es- are currently in full-scale development for the pecially composites, and its use of these materi- Navy’s V-22 Osprey, and are under considera- Photo credit: McDonnell Douglas The Navy AV-8B Aircraft. 26 . Advanced Materials by Design tion for several systems including the Army’s LHX tors. These include basic research in materials helicopters and the Air Force’s Advanced Tacti- synthesis, properties, and behavior, as well as cer- cal Fighter. Ceramics and composites of various tain applications, such as aircraft, in which the kinds will also be enabling technologies in such military and commercial performance require- new programs as the National Aerospace Plane ments are similar. DoD has also instituted pro- (NASP) and the Strategic Defense Initiative (SDI). grams such as the Manufacturing Technologies (ManTech) program to develop low-cost manu- Counting only basic and early applied R&D facturing methods, a critical need for both mili- (budget categories 6.1-6.3A), DoD sponsors tary and commercial structures. about 60 percent ($98 million of a total of $167 million in fiscal year 1987) of Federal advanced As a principal supporter of advanced materi- structural materials R&D in the United States, as als R&D, the military has two primary policy goals shown in table 1-7. If military development, test- relating to the technologies. The first is to pre- ing, and evaluation funds (as well as funds for vent or slow their diffusion to Eastern bloc coun- classified programs) were included, this fraction tries, and the second is to secure viable domestic would be much higher. Military research in ad- sources of supply. In an era of rapid technology vanced structural materials has aimed at achiev- diffusion across national borders and the grow- ing such goals as higher operating temperatures, ing multinational character of advanced materi- higher toughness, lower radar observability, and als industries, these policy goals are increasingly reduced weight. in conflict with commercial interests. Major issues that will require resolution include export con- Today, it is clear that U.S. leadership in ad- trols, controls on technical information, and gov- vanced composites technologies of all types stems ernment procurement practices. from the substantial DoD and NASA investments in these materials over the past 25 years. U.S. As commercial markets for these materials con- companies have been able to leverage their re- tinue to grow, effective balancing of military and sources by using DoD funds for R&D in these commercial interests in advanced materials could technologies. There are some areas of strong become a critical factor in U.S. companies’ com- overlap between military and commercial sec- petitiveness in these technologies. Table 1-7.—U.S. Government Agency Funding for Advanced Structural Materials in Fiscal Year 1987 (millions of dollars) Ceramics and ceramic matrix Polymer matrix Metal matrix Carbon/carbon Agency composites composites composites composites Total Department of Defensea...... $21.5 $33.8 $29.7 $13.2 $98.2 Department of Energy...... 36.0 — — — 36.0 National Aeronautics and Space Administration ...... 7.0 5.0 5.6 2.1 19.7 National Science Foundation ...... 3.7 3.0 — — 6.7 National Bureau of Standards ...... 3.0 0.5 1.0 — 4.5 Bureau of Mines ...... 2.0 — — — 2.0 Department of Transportation ...... — 0.2 — — 0.2 Total...... $73.2 $42.5 $36.3 $15.3 $167.3 alncludes only budget categories 6.1-6.3A. SOURCE: OTA survey of agency representatives. POLICY ISSUES AND OPTIONS Perhaps the central finding of this assessment determined by expected profits, do not believe is that potential commercial end users of ad- that use of advanced materials will be profitable vanced materials, whose investment decisions are within their planning horizon of 5 years. Thus, Ch. 1—Executive Summary ● 27 there is virtually no market pull on these tech- Currently, many such collaborative centers are nologies in the United States. While U.S. com- springing up across the United States. These mercial end users have placed themselves in a centers will provide an excellent environment for relatively passive, or reactive role with respect conducting generic research and training of stu- to use of advanced materials, their competitors, dents. However, because of the high risks in- notably the Japanese, have adopted a more ag- volved, they will not necessarily lead to more ag- gressive, “technology push” strategy. gressive commercialization of advanced materials by participating companies. Ultimately, the future competitiveness of U.S. advanced materials industries in worldwide com- Through acquisitions, joint ventures, and li- mercial markets depends on the investment de- censing agreements, the advanced materials in- cisions made within the industries themselves. dustries will continue to become more multina- These decisions are strongly affected by a vari- tional in character. Technology will flow rapidly ety of Federal policies and regulations. between firms and across national borders. Crit- ical advances will continue to come from abroad, It is useful to begin the policy discussion by and the flow of materials technology into this considering what outcomes are likely if current country will become as important as that flow- trends continue. ing out. U.S. efforts to regulate these flows for national security reasons will meet increasing re- Projections Based on a Continuation sistance from multinational companies intent on of the Status Quo achieving the lowest production costs and free access to markets. Because U.S. military markets will expand faster than commercial markets in the near term, the These scenarios suggest that there is reason to military role in determining the development doubt whether the United States will be a world agenda for advanced materials is likely to broaden. leader in manufacturing with advanced materi- As explained above, military investments in ad- als in the 1990s and beyond. The commerciali- vanced materials can be an asset to U.S. firms; zation of these materials is essentially blocked be- however, they could also tend to direct resources cause they do not meet the cost and performance toward development of high-performance, high- requirements of potential end users. OTA finds cost materials that are inappropriate for commer- that there are four general Federal policy objec- cial applications. tives that could help to reduce these barriers: Meanwhile, the reluctance of U.S. commercial 1. Encourage long-term investment by ad- end users to commit to advanced materials sug- vanced materials end users; gests that foreign firms will have an advantage 2. Facilitate government/u niversity/industry in exploiting global markets as they develop. collaboration in R&D for low-cost materials Almost certainly, a successful product using an fabrication processes; advanced material produced abroad would stim- 3. Facilitate more effective commercial exploi- ulate a flurry of R&D activity among U.S. com- tation of military R&D investments where panies. However, given the lack of experience possible; and in this country with low-cost, high-volume fabri- 4. Build a strong advanced materials technol- cation technologies, it is not obvious that the ogy infrastructure. United States could easily catch up. The high cost of R&D, scale-up, and produc- Policy options for pursuing these objectives tion of advanced materials, together with the range from those with a broad scope, affecting poor near-term commercial prospects, will drive many technologies, to those specifically affect- more and more U.S. companies to pool resources ing advanced materials. These options are not and spread risks through a variety of joint ventures, mutually exclusive, and most could be adopted consortia, and collaborative research centers. without internal contradiction. 28 ● Advanced Materials by Design Encourage Long-Term Investment by Creation of a small number of collaborative Advanced Materials End Users centers in which manufacturing research and scale-up costs would be shared by government, Greater investment in advanced materials by university, and industry stakeholders, could in- potential end users would generate more mar- crease industry incentives to invest in commer- ket pull on these technologies in the United cialization. These centers need not be new; they States. The shortfall of long-term investment in couId be based at existing centers of excellence. advanced materials by potential end user com- Option 2: Encourage large companies to work panies is only one example of a more widespread with small advanced materials firms, which shortfall found in many U.S. industries. have materials fabrication expertise, but lack The climate for long-term industry investment the capital to explore its commercial potential. is strongly affected by Federal policies and regu- Small advanced materials companies represent lations, including tax policy, intellectual property a technology resource that could make large law, tort law, and environmental regulations. materials supplier and user companies more Public debate regarding the relationships be- competitive in the future. Whether through ac- tween these Federal policies and regulations and quisitions, joint ventures or other financial ar- U.S. industrial competitiveness has given rise to rangements, relationships with small materials a voluminous literature. Suggested policy changes companies can provide large companies with ac- include: providing tax incentives for long-term cess to technologies that have commercial prom- capital investments, reducing taxation on per- ise, but that are too risky for the large company sonal savings in order to make more investment to develop in-house. Expanding the Small Busi- capital available and thus reduce its cost, and ness Innovation Research (SBIR) program is one comprehensive tort law reform aimed at making option for cultivating this resource. product liability costs proportional to proven negligence. These policy options have implications far be- Facilitate More Effective Commercial yond advanced materials technologies, and an Exploitation of Military R&D analysis of their effects is beyond the scope of Investments Where Possible this assessment. Military policy will continue to have a major impact on the domestic advanced materials in- Facilitate Government/University/ dustry. More effective exploitation of the military Industry Collaboration in R&D for investment for commercial purposes, while pro- Low-Cost Materials Fabrication tecting national security concerns, could lead to Processes significant competitive advantages for U.S. firms involved in these technologies. More than any other single barrier, the lack of reliable, low-cost fabrication processes inhibits Export Controls the use of advanced structural materials in com- Early in 1987, the Department of Commerce mercial applications. Due to the high costs of de- proposed several changes in the administration veloping these processes, it is a fruitful area for of export controls intended to alleviate their im- collaborative research. Three major reservoirs of pact on U.S. high-technology trade. Among these materials expertise are available to United States are proposals to remove technologies that have companies: 1 ) universities, 2) Federal labora- become available from many foreign sources tories, and 3) small high-technology firms. from the control lists, and to reduce the review Option 1: Establish a limited number of collabora- period for export license applications. These tive centers dedicated to advanced materials changes could be helpful, but some further steps manufacturing technology. should be considered. Ch. 1—Executive Summary “ 29 Option 1: increase representation by nondefense semination of advanced materials technical in- materials industries in policy planning for ex- formation can be controlled by: International port controls. Traffic in Arms Regulations (ITAR) of the Depart- Currently, advice for making export control pol- ment of State; the dual-use technology restrictions icy decisions comes primarily from defense of the Department of Commerce; the Defense agency personnel and defense contractors. To Authorization Act of 1984; government contract achieve a better balance between military and restrictions; and Federal document classification commercial concerns, greater non-defense indus- systems. There are so many ways to restrict in- try participation in this process is desirable. An formation that actual implementation of restric- industry advisory group such as the Materials tions can appear arbitrary. Under some of these Technology Advisory Council at the Department laws, regulations, and clauses, one can file for of Commerce could provide this perspective. a license to export, and under others, there is no mechanism to permit export of the information. Option 2: Eliminate or loosen reexport controls. These controls have led to disruption of scien- The United States is currently the only nation tific meetings and to restriction of some advanced that imposes controls on the reexport by other materials conference sessions to “U.S. only” par- countries of products containing U.S.-made ma- ticipation. terials or components. Many countries view U.S. Option 1: Simplify and clarify the various infor- reexport controls as unwarranted interference in mation restriction mechanisms. their political and commercial affairs, and this has Excessive restrictions on information flow can led to a process of “de-Americanization” in inhibit technology development and prevent which foreign companies avoid the use of U. S.- technology transfer between the military and made materials and components. One option commercial sectors. Relying more on classifica- wouId be to eliminate the U.S. reexport restric- tion and less on the other more tenuous mecha- tions entirely, while encouraging foreign trading nisms of control (such as the Defense Authori- partner nations to develop and maintain their zation Act or contract clauses), could clarify some own export controls for these products. of the confusion. Option 3: Streamline and coordinate the various Option 2: Make military materials databases more export control lists. available to U.S. firms. All of the various lists under which technologies The most comprehensive and up-to-date infor- are controlled should receive careful review for mation on advanced materials is now available correctness and current relevance. These lists only to government contractors through the De- could also be coordinated more effectively. For fense Technical Information Center (DTIC). DTIC example, the Departments of Commerce and contains a significant amount of information that State have overlapping legal and regulatory au- is neither classified nor proprietary, but is still thority to control the export of MMC technology. limited to registered users. Such information The present system is extremely confusing to U.S. could be of value to U.S. commercial firms that companies, which have experienced long delays are not government contractors. in obtaining approval for export licenses. One op- tion would be to have a single agency regulate both the export of MMC materials and technical Military Research in data related to them. Manufacturing Technologies Although military applications for advanced Information Controls materials can generally tolerate higher costs for Technical information about advanced mate- materials and processes than commercial appli- rials is controlled under a complex regime of laws cations, both could benefit greatly from research and regulations administered by the Departments on low-cost processing methods. The desire to of State, Commerce, and Defense. Currently, dis- reduce procurement costs led DoD to implement 30 . Advanced Materials by Design its ManTech program, which includes projects craft or other high-technology systems receives devoted to development of many different ma- materials production technology from the U.S. terials and manufacturing technologies. system supplier as part of the sale. This can lead to a production capability abroad that is detri- Option: Increase support for advanced materi- mental to the U.S. advanced materials technol- als manufacturing research through the Man- ogy base. Technology offsets are commonly re- Tech program. quired by foreign governments before bids from Development of low-cost manufacturing tech- U.S. (or other) systems suppliers will be consid- nologies would not only reduce military procure- ered. In recent years, little attention has been paid ment costs, but could also hasten the commer- to the effects of offsets. cial use of advanced materials technologies Option: Initiate a thorough study on the effects developed for the military, One mechanism to of offsets on the competitiveness of U.S. ad- achieve this would be to augment the ManTech vanced materials industries. budget for those programs aimed at decreasing production costs and increasing reproducibility and reliability of advanced materials structures. Build a Strong Advanced Materials Procurement Practices Technology Infrastructure DoD constitutes a special market with unique For U.S. advanced materials suppliers and users materials requirements. However, like other cus- to exploit technological developments rapidly, tomers, DoD seeks the widest variety of materi- whether they originate in the United States or als available at the lowest possible cost. It there- abroad, an infrastructure must be built up to re- fore employs regulatory means to simulate the duce barriers to their use. In this context, a tech- conditions of commercial markets. This makes nology infrastructure encompasses the availability the participation by materials suppliers extremely of basic scientific knowledge, technical data to dependent on defense regulations and policies, support design and fabrication, and an adequate rather than on conventional economic criteria. supply of trained personnel. Through its policies on dual sourcing, materials Option 1: Increase R&D funding levels to reduce qualification, and domestic sourcing of advanced the costs of advanced materials and improve materials, DoD has a profound influence on the their performance. cost and availability of a variety of high-perform- ance materials and technologies. The development of low-cost fabrication proc- esses that are capable of making large numbers Option: Provide a clear plan for implementing of structures with reproducible properties is of legislation aimed at establishing domestic primary importance. sources of advanced materials technology. Option 2: Develop a comprehensive and up-to- Uncertainties about how recent domestic date database of collaborative R&D efforts in sourcing legislation (particularly that relating to advanced materials at the Federal, regional, procurement of polyacrylonitrile (PAN) -based and State levels, including program goals and carbon fibers) will be implemented have caused funding. much concern in the advanced composites com- munity. In order to make intelligent investment In recent years, a large number of research decisions, U.S. carbon fiber suppliers will require centers of excellence in advanced materials have a clear DoD pIan including information on quan- sprung up with the aid of government funding tities to be purchased and the specific weapons at Federal, regional, and State levels. Although systems involved. there are advantages to such a decentralized ap- proach, the resulting dispersion of talent and re- Offsets sources also could preclude the formation of a Offsets are a foreign policy-related marketing “critical mass” necessary to solve the remaining arrangement in which the foreign buyer of air- technical and economic problems. Such a data- Ch. l—Executive Summary ● 31 base would be an essential first step in bringing lish accounts of their experiences, and to dissem- greater coordination to these efforts. inate this information to U.S. industry. Option 3: Gather comprehensive information on Option 6: Increase support for the development current activities in government-funded R&D of standards for advanced materials. on advanced structural materials. It is very difficult to set standards in a field such One persistent need identified by many indus- as advanced materials in which technologies are try sources is a central source of information on evolving rapidly. However, timely development government projects in advanced materials. In of standard test methods, production quality con- general, this information does exist, but it is rarely trol standards, and product specification stand- in a form that is readily accessible to research- ards would greatly facilitate the manufacture of ers. An oversight organization such as the Na- high-quality products at a lower cost. Several gov- tional Critical Materials Council could help to ernment and private sector organizations have gather and disseminate such information. begun to address this problem, but progress has been slow. Particularly important may be greater Option 4: Establish a mechanism for gathering Federal support of efforts to establish international business performance statistics on advanced standards. If the United States fails to agree on materials industries. standards or is forced to accept standards devel- It is difficult to evaluate the business trends of oped abroad, this could become a significant U.S. advanced materials industries because the competitive disadvantage for U.S. companies. statistics are aggregated with those of traditional Option 7: Increase the pool of trained materials materials industries. One alternative for correct- scientists and engineers by providing increased ing this situation would be to create separate funding for multidisciplinary university pro- Standard Industrial Classification (SIC) codes for grams in advanced structural materials, and by advanced ceramics and composites so that sta- providing retraining opportunities for techni- tistics on production, imports, and exports can cal personnel in the field. be systematically tracked. Advanced materials industry sources contacted Option 5: Step up person-to-person efforts to by OTA were nearly unanimous in their recom- gather and disseminate data on international mendation that more trained personnel are developments in advanced materials. needed. Because materials science cuts across As several competitor countries around the many traditional academic disciplines, multidis- world approach and exceed U.S. capabilities in ciplinary materials programs for students will be advanced materials, it becomes imperative for very important. Another important source of U.S. companies to have prompt and reliable ac- manpower will be retraining of designers and cess to these overseas developments. Rather than manufacturing engineers in the field who are un- engage in massive translation of technical pub- familiar with the new materials. Small businesses, lications, which may compete with private sec- professional societies, universities, and Federal tor efforts, the best Federal approach may be to laboratories could all play a role in providing such provide increased funding for U.S. scientists to retraining services. visit laboratories abroad, encourage them to pub- TWO VIEWS OF ADVANCED MATERIALS POLICIES Congress and the Reagan Administration have materials technology development, or whether adopted conflicting views of policymaking with goals and priorities should be established in a de- respect to advanced materials. The crux of the centralized fashion by the principal funding agen- conflict is whether the Federal Government cies according to their various missions. shouId establish a high-level plan for advanced 32 ● Advanced Materials by Design The United States has long had a decentralized folio of technologies, including machine tools, approach to advanced materials policy. To a great bearings, castings, semiconductors, and advanced extent, the major agencies that engage in mate- composites, for support. Issues such as techno- rials R&D (DoD, DOE, NASA, and NSF) sponsor logical obsolescence, availability of trained per- projects in the context of their distinct missions. sonnel, foreign acquisitions of U.S. companies, international cooperation, and government/uni- In the congressional view, the growing techno- versity/industry collaboration are being ad- logical capabilities of the United States’ compet- dressed. itors have underscored the urgency of a nation- ally coordinated approach to advanced materials A national approach to a materials program has R&D. This view is expressed in the National Crit- several potential advantages. It can provide a fo- ical Materials Act of 1984, in which Congress cus for the efforts of individual agencies and col- established the National Critical Materials Council laborative government/industry projects. It can (NCMC) in the Executive Office of the President. provide a continuity of funding in a given area The NCMC is charged with the responsibility of as fashionable R&D areas change from year to working with the principal funding agencies and year. Finally, it can provide a rationale for com- the Office of Management and Budget to define mitting large amounts of resources for expensive national priorities for materials R&D, and to co- manufacturing development and demonstration ordinate the various agency efforts. Advocates of programs. To be successful, such a national pro- a national materials policy point to the apparent gram should not be a “top-down” approach, but capacity of Japan to identify key technologies for should be structured with consultation and par- the future and pursue their development by ticipation of the university, Federal laboratory, means of a coordinated, government/industry ef- and industry community which will ultimately im- fort. Advanced ceramics have been a high-visi- plement it. bility example. Such a national approach also has disadvan- In the Administration’s view, it is not appro- tages. It may focus on the wrong materials, and priate for the government to engage in advanced be too inflexible to capitalize on new opportu- materials planning; this is viewed as putting the nities that arise. It may tie up resources and man- government in a position of “picking winners”- power in long-term programs that are better in- which, according to current thinking, is best left vested elsewhere. Finally, because it cannot to the private sector. Because different agencies address the cost and performance requirements have different missions and requirements for ma- of materials in actual commercial markets, it may terials, determination of R&D priorities is best fail to produce materials or processes that are made at the agency level. Administration critics economically attractive to end users. of the national materials policy concept maintain that attempts to make materials policy above the The debate surrounding national materials pol- agency level risk the worst aspects of Japanese icy has suffered from the lack of a clear defini- policies, the overbearing bureaucracy, without tion of what such a policy would entail. Whereas achieving the best effect, the commitment and policy goals such as conservation of scarce ma- coordination of industry. In their view, the con- terials or reliable access to strategic minerals are gressionally mandated NCMC is redundant with easily understood in the context of conventional existing interagency committees. materials, it is much more difficuIt to define na- tional goals for advanced materials. To succeed While the Reagan Administration has resisted in its task, the NCMC will need to establish a the concept of strategic advanced materials plan- more precise definition of these goals, and to de- ning for commercial competitiveness, it has em- velop high-level Administration commitment to braced it with regard to national defense needs. the concept of a national materials policy. DoD is currently preparing a comprehensive pol- icy initiative aimed at preserving the U.S. defense Pending the resolution of differences between industrial base. This initiative will target a port- Congress and the Administration regarding the Ch. 1—Executive Summary ● 33 role of the NCMC, there are three further func- agencies and laboratories. There is currently no tions that the NCMC could perform: definitive source of information that can provide an overview of ongoing efforts. An organization ● Serve as a point of contact to receive and such as the NCMC could gather this information monitor industry concerns relating to ad- from the relevant agencies, analyze it, and dis- vanced materials seminate it. An organization such as the NCMC could pro- ● Serve as a broker for resolving conflicts be- vide a forum for interaction between industry and tween military and commercial agency goals the Federal Government on issues relating to ad- for advanced materials vanced materials, particularly those that tran- scend the purview of any particular Federal There are materials issues that transcend indi- agency. This could promote better mutual under- vidual agencies and that could be resolved by an standing of industry and government perspectives organization above the agency level. For in- on advanced materials development, and could stance, the export control responsibility for reg- eventually lead to the development of a con- ulating advanced materials and information re- sensus on promising future directions. lating to them is currently spread over the Departments of Commerce, State, and Defense, ● Serve as an information source and a refer- a situation that is very confusing to industry. An ral center regarding advanced materials organization such as the NCMC could work with U.S. advanced materials programs and exper- the National Security Council to help simplify and tise are widely dispersed throughout various clarify the various agencies’ responsibilities. ADVANCED MATERIALS POLICIES IN A BROADER CONTEXT Ceramic and composite structural materials competitive challenges, and many of the policy clearly represent great potential opportunities for objectives and options discussed above could the U.S. economy. However, advanced materi- benefit all of them. As such, it may be most als are not unique in their importance to the future appropriate to address the commercialization of competitiveness of U.S. manufacturing industries. advanced materials technologies as part of a Other technologies, including microelectronics, broader policy package aimed at achieving computers, robotics, and biotechnology will also greater investment and productivity in the man- be important. These technologies face similar ufacturing sector as a whole. .—. ● Chapter 2 Ceramics . . . , . , -. * .. . . . . . , CONTENTS Page f‘age Findings . ● . , ● . ● . ● . . . . ● . , . . , . . 37 2-3. Projected U.S. Markets for Structural > * ****.*.*****.***...... *.*.* 38 Ceramics in the Year 2000 ...... 53 ...... 38 2-4. Load-Deflection Curve for a Nicalon Fiber- Ceramic Matrix Composites ●☛ ● ● .., . . . ● 40 Reinforced Silicon Nitride Composite. . . . . 65 Ceramic Coatings . ● . ● . . . . ● . . . ● .,. ● . . . . . 4? Tables ...... 42 “ Page 2-1. Some Future Applications of Structural Ceramics ...... ?, ...... 38 2-2. Comparison of Physical and Mechanical Properties of Common Structural Ceramics . . ● ● . . . . , . . . with Steel and Aluminum Alloys ...... 39 ● ● * ’ * . * * . . . . , ● , ● . . 2-3. Fracture Toughness and Critical Flaw l Ceramics ...... 50 , Size of Monolithic and Composite Ceramic * * * . * * * * * * * ...**.... 50 Materials Compared with Metals ...... 41 s...... ● ...... 52 Far-Term Applications....,,,...,.,... .., 52 2-4 Common Processing Operations for Advanced Ceramics ...... , *need Stuctural 43 --- 2-5. Selected Processes for the Production of %. .., ,+ ..,..,6,”,.....,,...,,. 52 ,::; ~ ns, and Production ...... 64 Ceramic Coatings and for the Modification of Ceramic Surfaces...... 46, : : ● ‘ . . . . ● “ , ● .. ..+, . 64 2-6. Characteristics and Properties of Ceramic compodtw . . . ● . ● . . . . ● * . . 64 Coatings Often Considered Desirable. . . . 47 ‘j; I%& @r Ceramics ....., ...... 6!5 2-7. Comparison of the Mechanical Properties . . . . * . * * . * . .,, ...... 65 of Various Cements and Aluminum . . . . . , ‘ .;+ I%04Wion . * * * * . ., * . . . . .***,*... 66 48 2-8. Comparison of Some Possible Production- ‘“.i~amh’md 04weloprmmt Priorities ...... 66 Level NDE Techniques for Structural 7- ;; VW knpottant...... : . . . . . e ...... 67 Ceramics...... 50 ‘ ~ wnpO&Rt* * . ., . ., + * ...... ,, * .,, ***..*. ● 68 w .,, H* ...... 69 2-9. Future Diesel Engine Technology . Development Scenario ...... 60 .,. ,.. .’ ‘ , -. ‘ 2-10. Structural Ceramic Technology: Federal . . . Figures Government Funded R&D...... 67 Figure. . No. Page 2-11. Breakout of the Fiscal Year 1985 Structural 2-1. ~--Faikm? of a Ceramic Ceramics Budget According to the R&D “ .*** **6 * S , ” ”,, ...... 40 Priorities Cited in the Text ...... 70 2-2. 2-Z for of . Ceramic Components in Structural Application Categories . . ● . ● . . . ● . ● 51 . ._.” . . . -. . .’ . Chapter 2 Ceramics FINDINGS The broad class of materials known as ceram- ings of a high-performance ceramic on a metal ics includes all solids that are neither metallic nor substrate may offer the best compromise between organic. Advanced structural ceramics differ from cost and performance. conventional ceramic consumer goods in that they are made from extremely pure, microscopic powders that are consolidated at high tempera- Applications and Market tures to yield a dense, durable structure. Com- Opportunities pared with metals, advanced structural ceramics Advanced structural ceramics are in produc- have superior wear resistance, high-temperature tion for wear parts, cutting tools, bearings, filters, strength, and chemical stability. They generally and coatings. Ceramics are also in limited pro- have lower electrical and thermal conductivity, duction (in Japan) in discrete engine components and lower toughness. The low toughness of ce- such as turbocharger rotors, glow plugs, and pre- ramics (brittleness) causes them to fail suddenly combustion chambers. Current military applica- when the applied stress is sufficient to propagate tions in the United States include radomes, ar- cracks that originate at flaws in the material. The mor, and infrared windows. actual stress level at which this occurs can be very high if the flaw sizes are small. However, unpre- dictable failure caused by poor control over flaw Near-term production (next 10 to 15 years) is populations remains a major handicap to the use expected in advanced bearings, bioceramics, of structural ceramics in load-bearing applications. construction applications, heat exchangers, elec- trochemical devices, discrete components in au- There are several methods that can reduce the tomobile engines, and military engines. Especially sensitivity of ceramics to flaws. Incorporation of high growth may be seen in bioceramics for den- ceramic particulate, whiskers, or continuous tal and orthopedic implants, and chemically fibers in a ceramic matrix can produce a com- bonded ceramics for construction applications. posite that absorbs more energy during fracture than the matrix alone, and is therefore tougher. Far-term applications (beyond 15 years) are A different approach is the application of a thin those that require solution of major technical and ceramic coating to a metal substrate. This yields economic problems. These include an advanced a component with the surface properties of a ce- automotive turbine engine, an advanced ceramic ramic combined with the high toughness of metal diesel (although ceramics could be used in mili- in the bulk. tary versions of these engines at an earlier date), Advanced ceramic components are more ex- some electrochemical devices, military compo- nents, and heat exchangers. A variety of other pensive than the metal components they would turbine engines, especially turbines for aircraft replace. This is primarily due to the high cost of processes that are capable of fabricating ceram- propulsion and for utility-scale power generation, ics reliably and reproducibly. Finishing and machin- should also be categorized as far-term. ing operations to form the part to its final shape are expensive due to the extreme hardness of the Research and Development Priorities tnaterial. Nondestructive testing to ensure relia- bility is also a major component of production The following hierarchy of R&D priorities is costs. Therefore, development of processes that based on the technical barriers that must be over- can reliably fabricate a component to final net come before ceramics can be used in the appli- shape is crucial, In many applications, thin coat- cations discussed above. 37 38 ● Advanced Materials by Design Processing Science Reliability This is the key to understanding how process- The reliability of advanced ceramics and ce- ing variables such as temperature, composition, ramic composites is the single most important de- and particle size distribution are connected to the terminant of success in any application. Progress desired final properties of the ceramic. requires advances in design of brittle materials, process control, nondestructive evaluation, un- Environmental Behavior derstanding crack growth processes, and life prediction. In many applications, ceramics are required to withstand high-temperature, corrosive, or erosive Ceramic Composites environments. Information on the behavior of ce- ramics in these environments is essential to pre- These novel materials offer an exciting oppor- dict the service life of ceramics in those appli- tunity to increase the strength and toughness of cations. ceramics. INTRODUCTION Ceramics are nonmetallic, inorganic solids. By ics as structural materials is the sensitivity of their far the most common of terrestrial materials, strength to extremely small flaws, such as cracks, ceramics made of sand and clay have been used voids, and inclusions. Flaws as small as 10 to 50 for many thousands of years for brick, pottery, micrometers can reduce the strength of a ceramic and artware. However, modern structural ceram- structure to a few percent of its theoretical ics bear little resemblance to these traditional ma- strength. Because of their small sizes, the strength- terials; they are made from extremely pure, controlling flaws are usually very difficult to de- microscopic powders that are consolidated at tect and eliminate. high temperatures to yield a dense and durable The flaw sensitivity of ceramics illustrates the structure. importance of carefully controlled processing and The U.S. market for advanced structural ceram- finishing operations for ceramic components. ics in 1987 was $171 million. ’ In the next 10 to However, even with the most painstaking efforts, 15 years, however, the market opportunities for a statistical distribution of flaws of various sizes structural ceramics are expected to expand rap- idly (table 2-1 ) such that by the year 2000, the Table 2-1.—Some Future Applications of U.S. market alone is projected to be between $1 Structural Ceramics billion and $5 billion per year.2 Application Performance advantages Examples Properties of Ceramics Wear parts High hardness, low friction Silicon carbide, seals alumina bearings The properties of some common structural ce- valves ramics are compared with those of metals in ta- nozzles ble 2-2. In general, ceramics have superior high- Cutting tools High strength, hot hardness Silicon nitride Heat engines Thermal insulation, high Zirconia, silicon temperature strength, higher hardness, lower diesel components temperature strength, fuel carbide, sili- density, and lower thermal conductivity than me- gas turbines economy con nitride tals. The principal disadvantage of using ceram- Medical implants Biocompatibility, surface Hydroxylapatite, hips bond to tissue, corrosion bioglass, teeth resistance alumina, ‘Up from $112 million in 1985, according to data supplied by joints zirconia Business Communications Co., Inc. of Norwalk, CT. This includes Construction Improved durability, lower Advanced ce- wear parts, cutting tools, heat exchangers, engine components, highways overall cost ments and bioceramics, and aerospace applications. bridges concretes 2Greg Fischer, “Strategies Emerge for Advanced Ceramic Busi- buildings ness,” American Ceramic Society Bulletin 65(1):39, 1986. SOURCE Off Ice of Technology Assessment, 1988 Ch. 2—Ceramics “ 39 Table 2-2.—Comparison of Physical and Mechanical Properties of Common Structural Ceramics With Steel and Aluminum Alloys. SiC: silicon carbide; Si3N4: silicon nitride; ZrO2: zirconia Strength a Thermal Densitya Room temperature at 1,095° C Hardnessb conductivity Material (g/cm3) strength (MPa) (M Pa) (kg/mm2) 25°/1,100° (W/m° C) Various sintered SiC materials . . . . 3.2 340-550 (flexure) 340-550 (flexure) 2,500-2,790 85/175 C Various sintered Si3N 4 materials . . 2.7-3.2 205-690 (flexure) 205-690 (flexure) 2,000 17/60 c — C Transformation toughened ZrO2 . . . 5.8 500-1,250 (flexure) 1,300-1,635 1.713.5 Steels (4100, 4300, 8600, and 5600 series) ...... 7-8 1,035-1,380 (tensile yield) useless 450-650 43 Aluminum alloy ...... 2.5 415-895 (tensile yield) useless 100-500 140-225 NOTE: 1 MPa = 145 psi = 0.102 Kg/mm2. SOURCES: aR. Nathan Katz, “Applications of High Performance Ceramics in Heat Engine Design,” Materials Science and Engineering 71:227-249, 1985. bElalne P. Rothman, “Ultimate Properties of Ceramics and Ceramic Matrix Composites,” contractor report for OTA, December 1985. C"Ceramic Application and Design,” Ceramic Industry, February 1988, pp. 29-50. and locations will always exist in any ceramic ness determines the critical flaw size that will lead structure. Even identically prepared ceramic speci- to catastrophic failure at that stress. In fact, the mens will display a distribution of strengths, rather critical flaw size increases with the square of the than a single value. Design with ceramics, un- toughness parameter; thus, an increase in the ma- like design with metals, is therefore a statistical terial toughness of a factor of three leads to a process, rather than a deterministic process. ninefold increase in the flaw size tolerance. Ceramic failure probability is illustrated in fig- Reduction in the flaw sensitivity of ceramics is ure 2-1. The curve on the right in figure 2-1a rep- especially important for applications involving a resents the distribution of strengths in a batch of hostile environment, which can introduce strength- identically prepared ceramic components. The degrading defects and thus negate all efforts to curve on the left is the distribution of stresses that ensure reliability by identifying or eliminating the these components are subjected to in service. largest preexisting flaws. The overlap between the two curves, in which Three recent developments have been shown the stress in service exceeds the strength of the to improve the toughness of ceramics: micro- ceramic, determines the probability that the part structure design, transformation toughening, and will fail. composite reinforcement. There are several ways to reduce the probabil- ity of failure of the ceramic. One is to shift the Microstructure Design strength distribution curve to the right by elimi- The toughness of monolithic ceramics can be nation of the larger flaws, as shown in figure 2- improved considerably by refinement of the poly- 1 b. A second way is to use nondestructive testing crystalline grain size and shape. The presence of or proof testing to weed out those components elongated fibrous grains, especially in ceramics with major flaws. This leads to a truncation of the based on silicon nitride, has been shown to in- strength distribution, as shown in figure 2-1c. crease toughness by as much as a factor of 2 over Proof testing of each individual component, al- other monolithic ceramics, such as silicon car- though widely used in the industry today, is ex- bide and aluminum oxide.3 pensive and can introduce flaws in the material that were not there originally. Numerous mechanisms have been proposed to account for the observed toughening: crack A third way to reduce failure probability is to deflection, microcracking, residual stresses, crack design the microstructure of the ceramic so that pinning, and crack bridging. It is likely that sev- it has some resistance to fracture (increased tough- eral of these mechanisms operate simultaneously ness), and hence, some tolerance to defects. Toughness is a measure of the energy required to fracture a material in the presence of flaws. 3Nitrogen Ceramics, F. L. Riley (cd. ) (Boston and The Hague: Mar- For a ceramic component under stress, the tough- tinus Nijhoff Publishers, 1983). 40 . Advanced Materials by Design in these materials. The high toughness is accom- Transformation Toughening panied by high strength, both of which result Transformation toughening, a relatively new from the modified microstructure. approach to achieving high toughness and strength in ceramics, has great potential for increasing the use of ceramics in wear-resistance applications. Figure 2-1 .—Probabiiity of Faiiure of The key ceramic material is zirconia (zirconium a Ceramic Component oxide). Zirconia goes through a phase transformation from the tetragonal to the monoclinic crystal form while cooling through a temperature of about 21 00° F (1 150° C). This phase transformation is accompanied by an increase in volume of 3 per- cent, similar to the volume increase that occurs when water freezes. By control of composition, particle size, and heat treatment cycle, zirconia can be densified at high temperature and cooled such that the tetragonal phase is maintained down to room temperature. When a load is applied to the zirconia and a crack starts to propagate, the high stresses in the vicinity of the crack tip catalyze the transforma- tion of adjacent tetragonal zirconia grains to the monoclinic form, causing them to expand by 3 percent. This expansion of the grains around the crack tip compresses the crack opening, thereby preventing the crack from propagating. Ceramic Matrix Composites A variety of ceramic particulate, whiskers high-strength single crystals with length/diameter ratios of 10 or more), and fibers may be added to the host matrix material to generate a com- posite with improved fracture toughness. The presence of these reinforcements appears to frustrate the propagation of cracks by at least three mechanisms. First, when the crack tip en- counters a particle or fiber that it cannot easily break or get around, it is deflected off in another direction. Thus, the crack is prevented from propagating cleanly through the structure. Sec- ond, if the bond between the reinforcement and The probability of failure of a ceramic component is the over- lap between the applied stress distribution and the material the matrix is not too strong, crack propagation strength distribution,as shown in(a). This probability can be energy can be absorbed by pullout of the fiber reduced by reducing the flaw size (b), or truncation of the from its original location. Third, fibers can bridge strength distribution through proof testing (c). a crack, holding the two faces together, and thus SOURCE: R. Nathan Katz “Applications of High Performance Ceramics In Heat Engine Design,” Materials Science and Engineering 71:227-249,1985. prevent further propagation. Ch. 2—Ceramics ● 41 Table 2-3 presents the fracture toughness and times the values of monolithic ceramics; the tough- critical flaw sizes (assuming a typical stress of 700 ness of some alloys may be much higher. megapascals [MPa], or about 100,000 pounds per square inch [psi]) of a variety of ceramics and The critical flaw size gives an indication of the compares them with some common metals. The minimum flaw size that must be reliably detected toughness of monolithic ceramics generally falls in any nondestructive evaluation (N DE) to ensure in the range of 3 to 6 MPa-m½, corresponding reliability of the component. Most N DE techniques to a critical flaw size of 18 to 74 micrometers. cannot reliably detect flaws smaller than about With transformation toughening or whisker dis- 100 micrometers (corresponding to a toughness persion, the toughness can be increased to 8 to of about 7 MPa-m½). Toughnesses of at least 10 12 MPa-m½ (the critical flaw size is 131 to 294 to 12 MPa-m½ would be desirable for most com- micrometers); the toughest ceramic matrix com- ponents. posites are continuous fiber-reinforced glasses, at 15 to 25 MPa-m½. In these glasses, strength appears to be independent of preexisting flaw size Ceramic Coatings and is thus an intrinsic material property. By com- The operation of machinery in hostile environ- parison, metal alloys such as steel have tough- ments (e. g., high temperatures, high mechanical ½ nesses of more than 40 MPa-m , more than 10 loads, or corrosive chemicals) often results in per- formance degradation due to excessive wear and friction, and productivity losses due to shutdowns Table 2-3.—Fracture Toughness and Critical Flaw caused by component failure. Frequently, the Size of Monolithic and Composite Ceramic a component deterioration can be traced to dele- Materials Compared With Metals. terious processes occurring in the surface region Al2O 3: alumina; LAS: lithium aluminosilicate; CVD: chemical vapor deposition of the material. To reduce or eliminate such ef- fects, ceramic coatings have been developed to Fracture Critical protect or lubricate a variety of substrate materi- toughness flaw size Material (MPa•m ½ ) (micrometers) als, including metals, ceramics, and cermets Conventional microstructure: (ceramic-metal composites). Al 2 O 3 ...... 3.5-4.0 25-33 Sintered SiC...... 3.0-3.5 18-25 The coating approach offers several advan- Fibrous or interlocked microstructure: tages. First, it is possible to optimize independ- Hot pressed Si3N 4 ...... 4.0-6.0 33-74 ently the properties of the surface region and Sintered Si N ...... 4.0-6.0 33-74 3 4 those of the base material for a given application. SiAION ...... 4.0-6.0 33-74 Particulate dispersions: Second, it is possible to maintain close dimen- Al 2O 3TiC ...... 4.2-4.5 36-41 sional tolerances of the coated workpiece in that Si N -TiC...... 4.5 41 3 4 very thin coatings (of the order of a few micro- Transformation toughening: meters) are often sufficient for a given applica- ZrO 2-MgO ...... 9-12 165-294 ZrO 2-Y 2O 3 ...... 6-9 74-165 tion. Third, there are significant cost savings asso- Al O -ZrO ...... 6.5-15 86-459 2 3 2 ciated with using expensive, exotic materials only Whisker dispersions: for thin coatings and not for bulk components. Al 2O 3-SiC ...... 8-10 131-204 Fiber reinforcement:b Use of coatings can thereby contribute to the SiC in borosilicate glass . 15-25 conservation of strategically critical materials. SiC in LAS ...... 15-25 SiC in CVD SiC ...... 8-15 Fourth, it is often cheaper to recoat a worn part Aluminum c ...... 33-44 than to replace it. Steel c ...... 44-66 aAssumes a stress of 700 MPa (-100,000 psi). bThe strength of these composites is independent of preexisting flaw size. These advantages have led to widespread in- cThe toughness of some alloys can be much higher dustry acceptance and applications. For instance, SOURCES: David W. Richerson, “Design, Processing Development, and Manufac- turing Requirements of Ceramics and Ceramic Matrix Composites,” coatings of titanium nitride, titanium carbide, and contractor report for OTA December 1985; and Elaine P. Rothman, alumina are used to extend the useful life of tung- “Ultimate Properties of Ceramics and Ceramic Matrix Composites,” contractor report for OTA, December 1985 sten carbide or high-speed steel cutting tools by 42 ● Advanced Materials by Design a factor of 2 to 5,4 In 1983, annual sales of coated found to improve performance by permitting cutting tools reached about $1 billions.5 combustion gas temperatures to be increased by several hundred degrees Fahrenheit without in- Ceramic coatings are also finding wide appli- creasing the temperature of air-cooled metal cation in heat engines. Zirconia coatings of low 6 components or the complexity of the engine. Ce- thermal conductivity are being tested as a ther- ramic coatings are also being used to provide an mal barrier to protect the metal pistons and oxidation barrier on turbine blades and rings. cylinders of advanced diesel engines. In turbine engines, insulative zirconia coatings have been Progress in the use of ceramic coatings in these and other applications suggest that further re- 4 search on new coatings and deposition processes David W. Richerson, “Design, Processing Development, and Manufacturing Requirements of Ceramics and Ceramic Matrix Com- is likely to yield a high payoff in the future. posites, ” contractor report prepared for the Office of Technology Assessment, December 1985. 6 ‘U.S. Department of Commerce, Bureau of the Census, Census Tom Strangman, Garrett Turbine Engine Co., personal commu- of Manufacturing, Fuels, and Electric Energy Consumed, 1984. nication, August 1986. DESIGN, PROCESSING, AND TESTING It is in the nature of advanced structural mate- principles of brittle material design. Greater em- rials that their manufacturing processes are ad- phasis needs to be placed on brittle materials in ditive rather than subtractive. Ideally, the mate- college curricula. Courses at the college level and rials are not produced in billets or sheets that are minicourses for continuing education on design later rolled, cut, or machined to their final shape; for brittle materials should be offered and pub- rather, in each case the material is formed to its licized. 7 final shape in the same step in which the micro- A second serious barrier is the poor characteri- structure of the material itself is formed. zation of commercially available ceramics for de- Because of the severity of joining problems, the sign purposes. The data are inadequate because ceramics designer is always conscious of the need the mechanical, thermal, and chemical proper- to consolidate as many components as possible ties of ceramic materials vary with the method together in a single structure. Although consoli- of manufacture as well as the test method. Both dation cannot always be achieved (expensive carefully controlled and documented processing grinding or drilling is often required), to a great procedures and standard test methods, as dis- extent, the promise of advanced materials lies in cussed in chapter 5, will be required to give the possibility of net-shape processing, thereby elim- designers the confidence that consistent proper- inating expensive finishing and fastening oper- ties at a useful level can be obtained at a predict- ations. able cost. Ceramics Design Processing of Ceramics Designing with ceramics and other brittle ma- The production of most ceramics, including terials is very different from designing with me- both traditional and advanced ceramics, consists tals, which are much more tolerant of flaws. In of the following four basic process steps: pow- practice, ceramic structures always contain a dis- der preparation, forming, densification, and fin- tribution of flaws, both on the surface and in the ishing. The most important processing techniques bulk. Ceramic designs must avoid local stress con- involved in these steps are identified in table 2-4. centrations under loading, which may propagate cracks originating at the flaws. 7Specific proposals for improving ceramics education are given in the report of the Research Briefing Panel on Ceramics and Ce- One serious barrier to the use of ceramics is ramic Composites (Washington, DC: National Academy Press, the lack of knowledge among designers of the 1985). Ch. 2—Ceramics “ 43 Table 2.4.—Common Processing Operations for and/or faster rates. Dopants are also used to con- Advanced Ceramics trol grain growth or achieve higher final densities. Operation Process Examples The use of dopants, although providing many Powder beneficial results, can also have a detrimental in- preparation Synthesis SiC Sizing Si N fluence on the material properties. Segregation 3 4 of dopants at the grain boundaries can weaken Granulating Zr02 Blending the final part, and final properties such as con- Solution chemistry Glasses ductivity and strength may differ significantly from Forming Slip casting Combustors, stators Dry pressing Cutting tools those of the pure material. Extrusion Tubing, honeycomb Injection molding Turbocharger rotors Forming Tape casting Capacitors Melting/casting Glass ceramics Ceramic raw materials must be formed and Densification Sintering Al203 Reaction bonding Si3N4 shaped before firing. The forming process often Hot pressing Si3N4, SiC, BN determines the final ceramic properties. The im- Hot isostatic pressing Si N , SiC 3 4 portant variables in the forming step are particle Finishing Mechanical Diamond grinding Chemical Etching shape, particle packing and distribution, phase Radiation Laser, electron beam distribution, and location of pores. Electric Electric discharge SOURCE Office of Technology Assessment 1988 Forming processes for ceramics are generally classified as either cold forming or hot forming. The major cold forming processes include slip Powder Preparation casting, extrusion, dry pressing, injection mold- ing, tape casting, and variations of these. The Although most of the basic raw materials for product of such processes is called a green body, ceramics occur abundantly in nature, they must which may be machined before firing. The homo- be extensively refined or processed before they geneity of the cold-formed part determines the can be used to fabricate structures. The entire uniformity of shrinkage during firing. group of silicon-based ceramics (other than sil- ica) does not occur naturally. Compositions of Hot forming processes combine into one step silicon carbide, silicon nitride, and sialon (an al- the forming and sintering operation to produce loy of silicon nitride with aluminum oxide in simple geometric shapes. These processes include which aluminum and oxygen atoms substitute hot pressing (in which pressure is applied along into silicon and nitrogen lattice positions, respec- one direction) and hot isostatic pressing (HI Ping, tively) must all be fabricated from gases or other i n which pressure is applied to the ceramic from ingredients. Even minerals that occur naturally, all directions at once). such as bauxite, from which alumina is made, and zircon sands, from which zirconia is derived, Densification must be processed before use to control purity, Sintering is the primary method for converting particle size and distribution, and homogeneity. loosely bonded powder into a dense ceramic The crucial importance of powder preparation body. Sintering involves consolidation of the has been recognized in recent years. Particle sizes powder compact by diffusion on an atomic scale. and size distributions are critical in advanced ce- Moisture and organics are first burned out from ramics to produce uniform green (unfired) den- the green body, and then, at the temperature sities, so that consolidation can occur to produce range at which the diffusion process occurs, mat- a fully dense, sintered, ceramic part. ter moves from the particles into the void spaces Various dopants or sintering aids are added to between the particles, causing densification and ceramic powders during processing. Sinterabil- resulting in shrinkage of the part. Combined with ity can be enhanced with dopants, which con- forming techniques such as slip casting, sinter- trol particle rearrangement and diffusivities. These ing is a cost-effective means of producing intri- dopants permit sintering at lower temperatures cate ceramic components. Its drawback lies in 75-7920 - 88 - 2 44 ● Advanced Materials by Design the need to use additives and long sintering times plications, near-net-shape processing of ceramics to achieve high densities. The complications in- must continue to be a high-priority research area troduced by dopants have been noted above in if advanced ceramics are to be cost-competitive. the discussion of powders. Ceramic Matrix Composites Finishing Ceramic matrix composites (CMCs) may con- This step involves such processes as grinding sist of: randomly oriented ceramic whiskers within and machining with diamond and boron nitride a ceramic matrix; continuous fibers oriented tools, chemical etching, and laser and electric dis- within a ceramic matrix; or dissimilar particles dis- charge machining. The high hardness and chem- persed in a matrix with a controlled microstruc- ical inertness of densified ceramics make the fin- ture. The potential benefits of ceramic compos- ishing operations some of the most difficult and ites include increased fracture toughness, high expensive in the entire process. Grinding alone hardness, and improved thermal shock resistance. can account for a large fraction of the cost of the Processing methods for particulate-reinforced component. In addition, surface cracks are often composites are similar to those for monolithic ce- introduced during machining, and these can re- ramics, and so are not discussed in this section. duce the strength of the part and the yields of the fabrication process. Whisker Reinforcement Ceramic whiskers are typically high-strength Near-Net-Shape Processing single crystals with a length at least 10 times Near-net-shape processing describes any form- greater than the diameter. Silicon carbide is the ing process that gives a final product that requires most common whisker material. Currently, whisker- little or no machining. Typically, ceramics shrink reinforced CMCs are fabricated by uniaxial hot to about two-thirds of their green body volume pressing, which substantially limits size and shape upon sintering. This shrinkage makes it extremely capabilities and requires expensive diamond difficult to fabricate ceramics to final net shape. grinding to produce the final part. Although hot However, if the green body ceramic is machined isostatic pressing has the potential to permit fabri- prior to densification, a near-net-shape part can cation of complex shapes at moderate cost, this be obtained. Hot isostatic pressing and ceramic technique requires procurement of expensive coatings can also yield parts that do not require capital equipment and extensive process devel- subsequent machining. opment. Reaction bonding is a near-net-shape process Continuous Fiber Reinforcement that has undergone considerable development, particularly for silicon nitride. In this process, The primary fibers available for incorporation green body compacts of finely divided silicon into a ceramic or glass matrix are carbon, silicon powder are reacted with nitrogen gas to produce carbide, aluminum borosilicate, and mullite. Cur- silicon nitride. In reaction bonding, the spaces rently, glass matrix composites are more devel- between the silicon powder particles in the green oped than their ceramic analogs. These compos- body are filled with silicon nitride reaction prod- ites are far tougher than unreinforced glasses, but uct as the reaction proceeds, so no shrinkage are limited to service temperatures of 11 00° to occurs. Reaction bonding can also be used to 1300° F (5930 to 704° C). Service temperatures produce ceramic composites with excellent prop- up to 2000° to 2200° F (1 0930 to 1204° C) may erties because this process avoids damage to rein- be obtained with glass-ceramic matrices that crys- forcement fibers or whiskers caused by shrink- tallize upon cooling from the process tempera- 8 age during the sintering step. ture. Carbon matrix composites have the highest potential use temperature of any ceramic, ex- Near-net-shape processes that are currently ceeding 3500° F (1 9270 C). However, they oxi- used for metals include powder metallurgy and 8Karl M. Prewo, J.J. Brennan, and G.K. Layden, “Fiber-Reinforced advanced casting techniques. Because metals are Glasses and Glass-Ceramics for High Performance Applications, ” in direct competition with ceramics in many ap- American Ceramic Society Bulletin 65(2):305, 1986. Ch. 2—Ceramics . 45 Photo credit: United Technologies Research Center Tensile fracture surface for Nicalon SiC fiber-reinforced glass ceramic. Fabrication of CMCs reinforced with continu- ous fiber is currently of a prototype nature and is very expensive. Several approaches are under development: the fibers are coated with ceramic or glass powder, laid up in the desired orientation, and hot pressed; fibers or woven cloth are laid up, and are then infiltrated by chemical vapor deposition (CVD) to bond the fibers together and fill in a portion of the pores; fibers are woven into a three-dimensional preform, and are then infiltrated by CVD; and 50 µM a fiber preform is infiltrated with a ceramic- t i yielding organic precursor, and is then heat- Photo credit: Los Alamos National Laboratory treated to yield a ceramic layer on the fibers. Fracture surface of a composite formed by hot- This process is repeated until the pores are pressing silicon nitride powder with 30 percent by minimized. volume silicon carbide whiskers. Considerable R&D will be necessary to op- timize fabrication and to decrease the cost to dize readily in air at temperatures above about levels acceptable for most commercial appli- 11 00° F (593° C), and require protective ceramic cations. coatings if they are to be used continuously at high temperature.9 Ceramic Coatings 9Joel Clark, et. al., “Potential of Composite Materials To Replace Many different processes are used in the fabri- Chromium, Cobalt, and Manganese in Critical Applications,” a con- tractor report prepared for the Office of Technology Assessment, cation of ceramic coatings and in the modifica- 1984. tion of surfaces of ceramic coatings and mono- . 46 “ Advanced Materials by Design Iithic ceramics. Table 2-5 lists some of the more ing process include the purity, physical state, and important processes. toxicity of the material to be deposited; the depo- sition rate; the maximum temperature the sub- The choice of a particular deposition process strate can reach; the substrate treatment needed or surface modification process depends on the to obtain good coating adhesion; and the over- desired surface properties. Table 2-6 lists some all cost. of the coating characteristics and properties that are often considered desirable. Additional con- For most coating processes, the relationships siderations that can influence the choice of coat- between process parameters and coating prop- Table 2-5.—Selected Processes for the Production of Ceramic Coatings and for the Modification of Ceramic Surfaces Process category Process class Process Ceramic coating processes: Low gas pressure (“vacuum”) Chemical vapor deposition (CVD) Pyrolysis processes Reduction (plasma assisted) Decomposition (plasma assisted) Polymerization (plasma induced) Physical vapor deposition (PVD) Evaporation (reactive, plasma assisted) Sputtering (reactive, plasma assisted) Plasma-arc (random, steered) Ion beam assisted co-deposition Low pressure plasma spraying Plasma discharge spraying Processes at elevated gas pressures Plasma spraying Plasma arc spraying Flame spraying Combustion flame spraying Liquid phase epitaxy processes Wetting process Dip coating (e.g., Sol-Gel) Brush coating Spin-on coatings Reverse-roller coating Electrochemical processes Electrolytic deposition Cation deposition Electrophoretic deposition Charged colloidal particle deposition Anodization Anion oxidation in electrolytes Electrostatic deposition Charged liquid droplet deposition Processes for the modification of ceramic surfaces: Particle implantation processes Direct particle implantation Energetic ion or atom implantation in solids Recoil particle implantation Recoil atom (ion) implantation in solids Densification and glazing processes Laser beam densification and CW-laser power deposition glazing Pulsed-laser power deposition Electron beam densification and Energetic electron beam power glazing deposition Chemical reaction processes Gaseous anodization processes Ion nitriding Ion carburizing Plasma oxidation Disproportionation processes Deposition of molecular species Formed in gas phase Conversion processes Thermal diffusion Diffusion of material from surface into bulk of substrate Etching processes Chemical etching Acidic solutions; lye etching Ion etching Sputter process Mechanical processes Grinding Peening Polishing SOURCE: Manfred Kaminsky, Surface Treatment Science International, Hinsdale, IL Ch. 2—Ceramics . 47 Table 2-6.—Characteristics and Properties of Cements Ceramic Coatings Often Considered Desirable Cements are chemically active binders that may Good adhesion be mixed with inert fillers such as sand or gravel Precise stoichiometry (negligible contamination) Very dense (or very porous) structural morphology to form concrete. Cement pastes containing mi- Thickness uniformity nor additives such as organic polymers can also High dimensional stability be used as structural materials. By far the most High strength High fracture toughness common cement used in making CBCs is port- Internal stresses at acceptable levels Iand cement. Portland and related cements are Controlled density of structural defects hydraulic; that is, they react with water to form Low specific density High thermal shock resistance a relatively insoluble aggregate. In hydraulic ce- High thermal insulating properties ments, excess water is usually added to improve High thermal stability the working characteristics, but this causes the Low (or high) coefficient of friction High resistance to wear and creep hardened structures to be porous (the minimum High resistance to oxidation and corrosion porosity of fully-hydrated cements is about 28 Adequate surface topography percent) and of low strength.10 SOURCE: Manfred Kaminsky, Surface Treatment Science International, Hinsdale, IL. Recently, workability of such cements has been improved by using a high-shear processing tech- nique together with pressing or rolling to remove erties and performance in various environments pores from a low-water calcium aluminate ce- are poorly understood. Coating providers tend ment paste containing 5 to 7 percent (by weight) to rely on experience gained empirically. Work organic polymers. The dense paste, which is is in progress to establish these relationships for 10 certain processes, e.g., ion beam- or plasma- Richard A. Helmuth, Portland Cement Association, Personal assisted physical vapor deposition. In addition, communication, August 1986. improved deposition processes are required, par- ticularly for the coating of large components or those having a complex shape. In view of the cur- rent widespread use of coated machinery com- ponents and projected future requirements for components with advanced ceramic coatings, re- search in processing science for ceramic coatings remains an important priority. [ ● ✎ * Chemically Bonded Ceramics Hardened cement pastes and concretes fall in the category of chemically bonded ceramics (CBCs) because they are consolidated through chemical reactions at ambient temperatures rather than through densification at high temper- ature. Owing to their low strength (compared with dense ceramics), concrete and other cemen- titious materials are not normally considered to be advanced materials. However, in recent years, Photo credits: lmperial Chemical Industries PLC new processing methods have led to significant Top photo: Conventional Portland cement paste improvements in the strength of chemically microstructure, showing large flaws (pores). Bottom photo: Advanced cement paste microstructure, bonded ceramics, and further development will illustrating the absence of large pores provide additional improvements. (magnification x 100). 48 ● Advanced Materials by Design sometimes called macro-defect-free (MDF) ce- be made to net shape. Due to the low process- ment, has the consistency of cold modeling clay, ing temperature, it is possible to use any of a wide and can be molded or extruded by techniques variety of reinforcing fibers, including metal similar to those used for plastics. fibers. However, the presence of organics makes them unsuitable for use above 200° F (93° C). The hardened cement paste has a compressive Further work is needed to improve the long-term strength approaching that of aluminum (table 2- stability of these materials. 7) and much lower permeability than ordinary portland cement paste.11 Although MDF cement Concrete pastes cost 20 to 30 cents per pound (compared with 3 cents per pound for portland cement As chemical additives, such as organic poly- mers, have improved the properties of cement paste), they are still significantly cheaper than me- tals and plastics. pastes, chemical and mineral additives have had a similar effect on concrete. Minerals such as fly The processing of hydraulic CBCs is very cheap ash and microscopic silica particles help to fill in because it involves only adding water, mixing, the pores in the concrete and actually improve casting or molding, and permitting the material the bonding in the cementitious portion. This re- to set at room temperature or slightly elevated sults in greater strength and reduced permeabil- temperature. Very little dimensional change oc- ity.12 In a recently developed concrete, molten curs during the set and cure, so that parts can sulfur is used as a binder in place of cement. Sul- 11 According to product Iiterature supplied by Imperial Chemical fur concrete has superior corrosion resistance in Industries, “New Inorganic Materials. ” acidic environments and can be recycled by remelting and recasting without loss of the me- chanical properties.13 The compressive strength of typical concretes today is around 5,000 psi (34 MPa), although con- cretes with strengths of 10,000 to 15,000 psi (69 to 103 MPa) are becoming common. Under lab- oratory conditions, compressive strengths of at least 45,000 psi (310 MPa) have been achieved, and there is no indication that the ultimate strength is being approached .14 In concrete high- 12For a recent review, see Jan Skalny and Lawrence R. Roberts, “High Strength Concrete, ” Annual Review of Materials Science 17:35, 1987. 13 U.S. Department of Interior, Bureau of Mines,Bulletin 678, "Sul - fur Construction Materials,” by W.C. McBee, T.A. Sullivan, and Photo credit: CEMCOM Research Associates, Inc. H.L. Fike, 1985. This tool, made from a cement-based composite, 14 Sidney Mindess, “Relationships Between Strength and Micro- is used for autoclave forming of a fiber-epoxy structure for Cement-Based Materials: An Overview, ” Materials Re- jet engine component. search Society Symposium Proceedings 42:53, 1985. Table 2-7.—Comparison of the Mechanical Properties of Various Cements and Aluminum Material Density (g/cm3) Flexural strength (psi)a Compressive strength (psi) Fracture energy (J/m2) b Portland cement paste . . . . . 1.6-2.0b 725-1,450 4,000-5,000 20 Cement/asbestos ...... 2.3 5,075 — 300 Advanced cementsc...... 2.3-2.5 14,500-21,750 22,000-36,000 300-1,000 Aluminum ...... 2.7 21,750-58,000 42,000 10,000 a1 MPa = 145 psi. bAccording to information supplied by the Portland Cement Association. cThe advanced cement has the followingcomposition: 100 parts high alumina Cement; 7 parts hydrolyzed potyvinylacetate; 10-12 parts water. SOURCE: Imperial Chemical Industries. Ch. 2—Ceramics . 49 rise buildings, the higher compressive strengths characterization, in-process control, and life-cycle permit use of smaller columns, with consequent monitoring. It will be applied to the starting mate- savings in space and materials. rials, during the process, and to the final product. Two deficiencies in concrete as a structural ma- A key goal will be the evolution of NDE tech- terial are its low tensile strength and low tough- niques amenable to automation and computeri- ness. A typical concrete has a tensile strength be- zation for feedback control. Powder and green low 1,000 psi (7 MPa). Steel reinforcement bars body characterization will be critical tor materi- are added to the concrete to provide tensile als processed from powders. For in-process strength. In prestressed concrete, high-strength characterization, it will be essential to determine steel wires under tension are used to keep the the relation between measurable quantities, ob- concrete in a state of compression. To improve tained through the use of contact or noncontact strength and toughness, a variety of reinforcing sensors, and the desired properties. This will re- fibers, including steel, glass, and polymers, have quire developments in sensor technology as well been tried, with varying degrees of success. 15 as theories that can quantitatively relate the meas- Compared with unreinforced materials, fiber rein- u red N DE signal to the specific properties of in- forcement can increase the flexural strength by terest. a factor of 2.5 and the toughness by a factor of In the past, a great deal of emphasis has been 5 to 10.16 This reinforcement technology, which placed on the sensitivity of an NDE technique, dates back to the straw-reinforced brick of the that is, the size of the smallest detectable flaw. ancient Egyptians, requires fiber concentrations However, experience has shown that most qual- that are sufficiently low (usually 2 to 5 percent ity problems result not from minute flaws but by volume) to preserve the flow characteristics from relatively gross undetected flaws introduced of the concrete, plus a chemically stable inter- 18 during the fabrication process. Therefore, a face between the fiber and the concrete over more relevant criterion for reliabiIity purposes is time. Asbestos fibers served this function for many perhaps the size of the largest flaw that can go years; however, because of the health hazards, undetected. To date, though, there has been very new fibers are now being sought. little emphasis on the reliability of NDE tech- In recent years, several Japanese firms have de- niques, that is, the probability of detecting flaws veloped concretes reinforced with carbon and of various sizes. aramid fibers, and pitch-based carbon fiber- Cost-of-production estimates for high-perform- reinforced concrete curtain walls have been used ance ceramic components typicalIy cite inspec- in Tokyo office buildings. Although the carbon tion costs as accounting for approximately 50 per- fiber concrete panels cost 40 percent more than 19 cent of the manufacturing cost. Successful NDE precast concrete, their light weight permits the techniques for ceramic components, therefore, use of a lighter weight structural steel frame, re- should meet two major criteria. First, they should sulting in overall construction cost savings. ’ 7 reliably detect gross fabrication flaws to ensure that the material quality of the component is Nondestructive Evaluation equal to that of test specimens. Second, they Nondestructive evaluation (NDE), which is a should be able to evaluate the quality of a com- means of determining properties of a structure plex-shaped component in a practical manner. without altering it in any way, has long been used No single NDE technique for ceramics completely for flaw detection in ceramic materials to improve satisfies these criteria. However, those that could the reliability of the final product. In the future, be cost-effective for production-level inspections NDE will be used for defect screening, material are identified in table 2-8. IBR, Nathan Katz and Altred L. Broz, ‘‘Nondestructive Evaluation ‘ 51bld Conslderatlons for Ceramtcs and Ceramic Matrix Composites, ” a 16Am~rlCan Cc)ncrete I nStlt Ute, ‘ ‘State-of-the-Art Report on Fiber contractor report prepared for the Off Ice of Technology Assessment, Reinforced Concrete, ” Report No, ACI 544.1 R-82, 1982. November 1985. 17Englneerlng fQe\v5 Record, Au~. 1, 1985, P. 16 19Ibid 50 ● Advanced Materials by Design Table 2.8.—Comparison of Some Possible Production-Level NDE Techniques for Structural Ceramics Adaptability to Extent of development NDE technique Detected flaw type Sensitivity complex shapes required for commercialization Visual (remote) ...... surface fair good none Dye penetrant ...... surface good good none Radiographic ...... bulk 1-20/0 of specimen excellent none thickness Ultrasonic ...... bulk and surface good poor some Holographic ...... surface good fair large Thermographic...... surface poor excellent some Proof test ...... any good, but may excellent none introduce flaws SOURCE: Office of Technology Assessment, 1988. HEALTH AND SAFETY The most serious health hazard involved with posed to the fibers develop an increased num- ceramics appears to stem from use of ceramic ber of lung cancers over time compared with a fibers and whiskers. Studies carried out at the Na- control group.21 tional Cancer Institute have indicated that virtu- No data on the effects of ceramic fibers or ally all durable mineral fibers having a diameter whiskers on humans are available, and no indus- of less than 1 micrometer are carcinogenic when try standards for allowable fiber and whisker con- introduced into the lining of the lungs of labora- centrations in the workplace have been estab- tory rats.20 The carcinogenicity drops with in- lished. Until such data become available, the creasing diameter, such that fibers having di- animal studies suggest that these fibers should be ameters greater than 3 micrometers do not produce considered carcinogenic, and they should be tumors. Recent studies on commercially available treated in a manner similar to asbestos fibers. aluminosilicate fibers suggest that animals ex- 20 Mear] F. Stanton, et al., journal of the National cancer /f?Sti- ZI Phillp j. Landrigan, M. D., The Mount Sinai Medical Center, per- ture 67:965-75, 1981. sonal communication, August 1986. APPLICATIONS OF STRUCTURAL CERAMICS Figure 2-2 shows an estimated timetable for the small (generally less than 5 percent).22 However, introduction of ceramic products in various cat- substantial growth in ceramics production is ex- egories. It shows that some advanced structural pected to occur over the next 25 years in re- ceramics are in production, some have near-term sponse to increasing overall market demand, in- potential for production, and some are far from crease in the ceramics market share, and spin-off production. applications. Current U.S. military applications for ceramics Current Applications include radomes, armor, and infrared windows in the United States, ceramics such as alumina (see section entitled, Military Applications and and silicon carbide are already well established Production). In Japan, ceramics are in limited pro- in commercial production for many structural ap- duction in discrete automotive engine compo- plications in the categories of wear parts, cutting 22 U.S. Department of Commerce, A Competitive Assessment of tools, bearings, membranes, filters, and coatings. the U.S. Advanced Ceramics Industry (Washington, DC: U.S. Gov- The ceramics portion of these markets is currently ernment Printing Office, March 1984), pp. 38-39. Figure 2.2.—Estimated Scenario for Implementation of Ceramic Components in Structural Application Categories 1960 1965 1970 1975 1980 1985 1990 1995 2000 2005 2010 1 I I I I I Al O PSZ Si N Composites Wear parts 2 3 sic 3 4 TTA TZP Si3N4-BN Al O Al O -TiC Si N Al O -SiC Cutting tools 2 3 2 3 3 4 2 3 I coating TTA Advanced materials chemically Composites Advanced construction products bonded ceramics B4C Armor Coatings Bearings Diesels Turbines Military applications Radomes Isolated components Bearings I AI2O3 Si3N4 Military Bioceramics Al2O3 FDA hip Orthopedic Advanced clinical approval and dental materials Tubular Cogeneration Fhwd Heat exchangers Recuperated Rotary furnaces Military Industrial boundary 02 sensors Electrochlorination Na-S battery Fuelrod Electrochemical devices 02 pump Heat engines: F Exhaust port liner Piston pin Gasoline automotive Turbocharger Cam follower Pre-chamber, coatings Isolated parts Diesel automotive Glow plug Uncooled engine Automotive turbine Isolated Other turbines components Wear and Cutting Turbine Minimum—cookd Coatings corrosion toots components diesel I resistance SOURCE: David W. Richerson, “Design, Processing Development, and Manufacturing Requirements of Ceramics and Ceramic Matrix Composites, ” contractor report prepared for the Office of Technology Assessment, December 1985. 52 . Advanced Materials by Design nents such as turbocharger rotors, glow plugs, Far-Term Applications and precombustion chambers for diesel engines. In West Germany, the automobile manufacturer Some potential applications of ceramics require Porsche uses ceramic exhaust port liners on one solution of major technical and economic prob- model. To gain experience in fabricating advanced lems. These high-risk categories are categorized ceramics, Japanese firms use advanced manufac- as far-term (greater than 15 years away). The ulti- turing techniques to produce such consumer mate payoff may be large, but it is not possible products as ceramic ballpoint pen tips, tools, and to predict confidently that the problems will be scissors. These products also help to promote overcome to achieve the benefits. familiarity with the new materials among the Jap- Far-term applications include the automotive anese public. gas turbine engine, the advanced diesel, some electrochemical devices such as fuel cells, some In the United States, research funding for heat exchangers, and some bearings. A variety known near-term markets is currently being pro- of other turbines, especially those for aircraft vided by industry. Much of the funding is directed propulsion and utility-scale power generation, toward development of new or improved ceramic should also be categorized as far-term. or CMC materials. Key objectives are to achieve Substantial design, material property, and man- improved toughness, higher reliability, and lower ufacturing advances are necessary to achieve pro- cost. Development of silicon nitride, transforma- duction of applications in the far-term category. tion-toughened ceramics, and composites has In general, risk is perceived by industry to be too yielded materials with enhanced toughness and high and too long-range to justify funding the reliability, but costs are still high and reliability needed developments. Advancement will likely remains a problem. Currently, progress is being be driven by government funding. In many of made in resolving these limitations, and forecasts these categories, military use will predate com- indicate there will be large increases in the mar- mercial use. ket share for ceramics. Markets for Advanced Structural Near-Term Applications Ceramics U.S. production in the near term (the next 10 Estimated structural ceramics markets in the to 15 years) is projected in advanced construc- year 2000 for several of the categories listed tion products, bearings, membranes for food above are shown in figure 2-3. processing applications, bioceramics, heat ex- changers, electrochemical devices, isolated com- Wear Parts ponents for internal combustion engines, and mil- itary applications. The technology feasibility for Wear parts include such applications as seals, these applications has generally been demon- valves, nozzles, wear pads, grinding wheels, and strated, but scale-up, cost reduction, or design liners. The Department of Commerce has esti- optimization are required. mated that by the year 2000 ceramics could cap- ture roughly 6 percent of the wear-parts market, which is currently dominated by tungsten car- Although much of the feasibility demonstration bide, cermets, and specialty steels. With the to- has occurred in the United States, foreign industry tal market estimated at $9 billion, the ceramic and government/industry teams, particularly in portion would be $540 million.23 Japan, have more aggressive programs to com- mercialize the near-term applications. Large mar- kets are at stake; foreign dominance of these mar- kets would adversely affect the U.S. balance of trade. ‘] Ibid., p. 35, Ch. 2—Ceramics ● 53 Figure 2-3.—Projected U.S. Markets for Structural used successfully in the limited operations of turn- ‘Ceramics in the Year 2000 (billions of dollars) ing and milling. A further impediment to the use 1.0 of ceramics, especially in the United States, has been equipment limitations; much of the produc- tion metal machining equipment does not have the rigidity or speed capability to use ceramics. A 1986 projection for ceramic and ceramic- coated cutting tools (the largest portion of which are inserts) places the growth rate at about 6 per- cent per year from a present market of $600 mil- lion to a market of over $1 billion by 1995. 24 The 0.5 vast majority of this market is coated carbide tool- ing. A second projection, for only the solid ce- ramic insert cutting tool market, is $128 million overall market by the year 2000. 25 Bearings High-performance ceramic bearings have been developed for military applications such as mis- siles. The primary candidate material is hot pressed silicon nitride. Ceramics offer resistance to low-temperature corrosion, high-temperature stability, low density, and the ability to operate for a moderate length of time with little or no lu- SOURCES: aU.S. Department of Commerce, “A Competitive Assessment of the brication. Hot isostatic pressing is being devel- U.S. Advanced Ceramics Industry" (Washington, DC, U.S. Govern- ment Printing Office, March 1984) oped to improve properties and to decrease cost bE.P. Rothman, J. Clark, and H.K. Bowen, "Ceramic Cutting Tools: A by permitting near-net-shape fabrication. Production Cost Model and an Analysis of Potential Demand," Ad- vanced Ceramic Materials, American Ceramics Society, Vol 1, No. 4, October, 1986, pp 325-331. The military developments will yield a technol- C High Technology, March, 1988, p. 14. d Business Communications Co., Inc., as reported in Ceramic Indus- ogy base that can be applied to commercial prod- try, Jan 1988, p. 10. ucts such as instrumentation bearings, hydrau- eDavid W. Richerson, "Design, Processing Development, and Manu- facturing Requirements of Ceramics and Ceramic Matrix Compos- lic and pneumatic activator systems, and ceramic ites," contractor report prepared for the Office of Technology Assessment, December 1985 coatings on the foils in gas bearings. Potential ce- f Assumes a doubling from 1986. Paul Hurley, "New Filters Can Clean ramic bearing markets have been estimated to Up in New Markets," High Technology, August 1987 be $300 million per year.26 Cutting Tools Membranes Ceramics have demonstrated capability as cut- ting tools, especially in competition with tung- Membrane filters are used in a wide variety of sten carbide-cobalt cermets as inserts for metal separation and purification processes, and mar- turning and milling operations. The advantage of kets are projected to increase from $500 million ceramics compared with carbides is retention of in 1986 to $2 billion by 1995. Some of the fastest high hardness, strength, and chemical inertness growing segments are expected to be food and to temperatures in excess of 1000° C (18320 F). 24 G. Shroff, SRI International, “Business Opportunities in Ad- This permits use of the ceramics at much higher vanced Structural Ceramics and Ceramic Coatings, excerpted In machining speeds than can be tolerated by Advanced Ceramic Mater;a/s 1(4):294, October 1986. 25 Elaine P. Roth ma n, Joel Clark, and H. Kent Bowen, ‘‘Ceram IC carbides, Cutting Tools: A Production Cost Model and an Analysis of Poten- tial Demand, ” Advanced Ceramic Materials, American Ceramic So- However, the ceramics have lower toughness ciety 1(4):325-331, October 1986. than the carbide materials, and have only been 26 High Technology/, March 1986 p. 14. 54 “ Advanced Materials by Design generator sets, heat exchangers); agriculture (e.g., plows and tillers); and aerospace (e.g., bearings, power transfer assemblies, and actuator drive systems). The availability of advanced ceramic coatings is expected to be a significant benefit to the U.S. economy. The value of the market for ceramic coatings is not easily assessed because the range of applications is so wide. In 1985, markets for ceramic coating materials were estimated at $1 billion worldwide, of which about 60 to 70 per- cent was domestic.28 This estimated market in- cludes jet engine, printing, chemical, textile, and tool and die applications. This list could be greatly expanded in the future to include wear parts, bearings, biomaterials, heat exchangers, and au- tomotive components. Advanced Construction Products Potential applications of advanced cement- beverage processing, aqueous waste processing, based materials include floors, wall panels, and diesel engine exhaust filters, and gas separation. roof tiles, in addition to pipes, electrical fittings, Although ceramic membranes cost more than the and cabinets. The cements can be laminated with more well-established polymer membranes, ce- wood or foam to form hard, decorative, and pro- ramics offer a number of performance advan- tective surfaces.29 Advanced cement pastes cost tages, including resistance to high temperatures, $0.20 to $0.30 per pound (compared with $0.75 chemical and mechanical stability, and ease of to $2 per pound for metals and plastics), and they cleaning. In 1986, markets for ceramic membranes could displace these materials in the future in were estimated at $200 million, and growth rates many common uses. of up to 30 percent are projected into the 1990s.27 The development of a cost-effective, durable, Coatings high-tensile, and high-compressive strength con- crete would have dramatic implications for the Ceramic coatings should be considered an ex- infrastructure of the United States. It has been tremely important technology for extending the estimated that between 1981 and the end of the performance of metal components, and, in some century, the Nation will spend about $400 bil- cases, they may be an excellent alternative to lion on replacement and repair of pavements and monolithic ceramics. They provide a variety of about $103 billion to correct bridge deficien- benefits, including abrasion resistance, thermal cies. 30 Cost savings of about $600 million per year protection, corrosion resistance, and high-tem- could result from implementing new technol- perature lubrication. Applications include ultra- ogies.31 hard coatings for cutting tools, thermal insulation and lubricating coatings for adiabatic diesel en- Zsjulie M. schoerrung, Elaine P. Rothman, and Joel P. Clark, “prop- gines and cooled gas turbines, and bioactive glass erties, Costs, and Applications of Ceramics and Ceramic Matrix Composites,” a contractor report prepared for the Office of Tech- coatings for metal orthopedic implants. The list nology Assessment, December 1985. could be expanded to include other sectors such Zglmperial Chemical Industries, “New Inorganic Materials” (prod- drills); utilities (e.g., turbine- uct literature). as mining (e.g., JoNational Research Council, Transportation Research Board, America’s Highways: Accelerating the Search for Innovation, spe- 27Paul Hudey, “New Filters Clean Up in New Markets,” High cial report No. 202, 1984. Technology, August 1987. 31 Ibid. Ch. 2–Ceramics “ 55 Photo credits: CEMCOM Research Assiciates, Inc. A spring made from a high-strength cement, formed by extrusion processing. Left: natural length. Right: compressed. The spring is not Intended for any practical use, but demonstrates the versatility and resilience of the material. 56 . Advanced Materials by Design In addition to reducing repair and maintenance the next decade.36 Ceramics could account for costs, new materials would provide other bene- 25 to 30 percent of this market.37 However, not fits. For instance, high compressive strength con- all estimates are so optimistic. One projection crete can be used to reduce the number and places the U.S. bioceramics market at $8 million thickness of concrete bridge girders, significantly in 1987, increasing to $60 million by 2000.38 reducing the structural weight.32 In concrete high- Bioceramics may be grouped into three cate- rise buildings, the use of such materials permits gories: nearly inert, surface-active, and resorba- a reduction in the diameter of the columns, thus 39 ble. Nearly inert ceramics can be implanted in freeing up additional floor space. the body without toxic reactions. These materi- There are major barriers to the development als include silicon nitride-based ceramics, trans- and implementation of new technologies in the formation-toughened zirconia, and transforma- construction industry. Some of those most often tion-toughened alumina. cited are industry fragmentation (e.g., some Surface-active ceramics form a chemical bond 23,000 Federal, State, and local agencies oper- with surrounding tissue and encourage ingrowth. ate the Nation’s highway system); an arrangement They permit the implant to be held firmly in place that awards contracts to the lowest bidder; and and help prevent rejection due to dislocation or low industry investment in research as a percent- to influx of bacteria. Surface-active ceramics that age of sales (the steel industry, by contrast, in- will bond to bone include dense hydroxyapatite, vests eight times more).33 The low investment is surface-active glass, glass-ceramic, and surface- due in part to the fact that the principal benefits active composites. The function of resorbable of the use of better materials accrue to the owner bioceramics is to provide a temporary space filler of the highway or bridge (the taxpayer) rather 34 or scaffold that will serve until the body can grad- than to the cement producer. ually replace it. The Surface Transportation Assistance Act of Resorbable ceramics are used to treat maxil- 1986 (Public Law 100-1 7) sets aside 0.25 percent Iofacial defects, for filling periodontal pockets, as of Federal aid highway funds for the 5-year, $150 artificial tendons, as composite bone plates, and million Strategic Highway Research Program. The for filling spaces between vertebrae, in bone, program, which is administered by the National above alveolar ridges, or between missing teeth. Research Council, has targeted six priority re- An early resorbable ceramic was plaster of paris search areas for support: asphalt characteristics, (calcium sulfate), but it has been replaced by $50 million; long-term pavement performance, trisodium phosphate, calcium phosphate salts, $50 miIlion; maintenance cost-effectiveness, $20 and polylactic acid/carbon composites.40 million; concrete bridge components, $10 mil- lion; cement and concrete, $12 million; and snow Any new material intended for use in the hu- and ice control, $8 million. 35 man body must undergo extensive testing before it is approved. Preclinical testing, clinical studies, Bioceramics and followup generally take a minimum of 5 years to complete.41 However, ceramics have been in Bioceramics, or ceramics for medical applica- tions such as dental or orthopedic implants, rep- 36 Larry L. Hench and June Wilson Hench, “Biocompatibility of resent a major market opportunity for ceramics Silicates for Medical Use, ” Silicon Biochemistry, CIBA Foundation in the future. The overall worldwide market for Symposium, No. 121 (Chichester, England: John Wiley & Sons, 1986), pp. 231-246. biocompatible materials is currently about $3 bil- 37 lion, and this is expected to double or triple in Larry L. Hench, University of Florida, personal communication, August 1986. 38 According to Business Communications Co., Inc., as reported 32J. E. Carpenter, “Applications of High Strength Concrete for High- in Ceramic Industry, January 1988, p. 10. way Bridges, ” Pub/ic Roads 44(76), 1980. 39 J.W. Boretos, "Ceramics in Clinical Care,” American Ceramics IJNational Research Council, op. cit., 1984. Society Bulletin 64(8):630-636, 1985. 34Ibid. 40 Ibid. 41 35"Construction and Materials Research and Development for the Edwardo March, Food and Drug Administration, personal com- Nation’s Public Works,” OTA staff paper, June 1987. munication, August 1986. Ch. 2—Ceramics . 57 Heat Exchangers Ceramic heat exchangers are cost-effective be- cause they can use waste heat to reduce fuel con- sumption. Heat recovered from the exhaust of a furnace is used to preheat the inlet combus- tion air so that additional fuel is not required for this purpose. The higher the operating tempera- ture, the greater the benefit. Ceramic systems have the potential to reduce fuel consumption by more than 60 percent.43 Ceramic heat exchangers may be used in a va- riety of settings, including industrial furnaces, in- dustrial cogeneration, gas turbine engines, and fluidized bed combustion, The size of the unit, manufacturing technique, and material all vary depending on the specific application. Sintered silicon carbide and various aluminosilicates have been used in low-pressure heat exchangers be- cause of their thermal shock resistance; however, the service temperature of these materials is cur- rently limited to under 2200° F (1204° C). Silicon carbide is being evaluated for higher tempera- tures, but considerable design modifications will be necessary .44 Federal Government support has been neces- sary to accelerate development of the ceramic materials and system technology for heat ex- changers, in spite of the design projections of sig- nificant fuel savings and short payback time. The material manufacturers, system designers, and end users have all considered the risks too high to invest their own funds in the development and implementation of a system. Three of their specific concerns are: 1) the high installed cost (up to $500,000 for a unit that de- livers 20 million British thermal units per hour), which represents a significant financial risk to the user for a technology that is not well proven; 2) many potential end users are in segments of in- dustry that presently are depressed; and 3) de- signs vary according to each installation, leading the user to want a demonstration relevant to his particular situation. 43s. M. Johnson ancj D.J. Rowcliffe, SRI International Report to EPRI, “Ceramics for Electric Power-Generating Systems, ” January 1986. 44 42 Richerson, op. cit., footnote 4 Richerson, op. cit., footnote 4. 58 ● Advanced Materials by Design Many of the ceramic heat exchanger programs $840 million by 2000.47A study by Charles River were initiated in the 1970s when there was a na- Associates estimates U.S. consumption of ceramic tional sense of urgency concerning the energy heat engine parts at $25 to $45 million in 1990 crisis. In recent years, declining fuel prices have and $920 million to $1.3 billion by 2000.48 generally reduced this sense of urgency. As long Some structural ceramic components are al- as low fuel prices persist, this could delay the ready in limited production in automobile en- widespread implementation of ceramic heat ex- gines. Ceramic precombustion chambers and changers for waste heat recovery. glow plugs for diesels, as well as ceramic turbo- charger rotors, are now i n production i n current Electrochemical Devices model Japanese cars. Although not strictly structural applications of Ceramic engine components markets will ceramics, devices in this category use ceramics grow, but not to a level that will account for the for both their electrical and structural properties. projected $1 billion sales for heat engine com- Typically, the ceramic, such as zirconia or beta ponents in the year 2000. Growth to this level alumina, serves as a solid phase conductor for would require material and design technology ions such as oxygen or sodium. Examples include breakthroughs, as well as manufacturing scale- oxygen sensors, oxygen concentration cells, solid up and cost reduction. In view of these techni- oxide fuel cells, the sodium-sulfur battery, sodium cal and economic barriers, the more conserva- heat engine, and electrodes for metal winning tive estimates are likely to be the more accurate. and electrochlorination cells. As a group, these applications could comprise a market of over 45 Gasoline Engines $250 million for ceramics by the year 2000. The automotive internal combustion gasoline Heat Engines engine offers a vast market for materials. Total sales for 1985 of cars and trucks in the free world The advantages of using ceramics in advanced 49 have been estimated at 38,7 million units. Any heat engines have been widely publicized. These part replacement or new part would represent include increased fuel efficiency due to higher a volume market with substantial sales, even if engine operating temperatures, more compact the unit price were small. However, current en- designs, and reduction or elimination of the cool- gine designs are considered by automotive com- ing system.46 Ceramics are being considered in panies to be mature, reliable, and cost-effective. three general categories: 1 ) discrete components such as turbocharger rotors in metal reciprocat- Very few incentives for change exist. Cost re- ing engines; 2) coatings and monolithic hot- duction does remain a significant incentive, but section components in advanced diesel designs; this goal is extremely difficult to satisfy for a new and 3) all-ceramic gas turbine engines. material, whose introduction may require re- design of adjacent parts, retooling, and modifi- Some analysts have predicted that components cation of the production line. for heat engines will be the largest area of growth for structural ceramics over the next 25 years. Another incentive is to develop a new technol- projected market estimates vary widely. Earlier ogy that may be applicable to advanced designs. estimates tended to be more optimistic, with sev- This would involve both generic and directed eral analysts projecting U.S. ceramic heat engine R&D, with the primary objective of maintaining markets around $5 billion by the year 2000. The a competitive position. Ceramics within this Department of Commerce has conservatively esti- category that have potential for production in- mated a U.S. market of $56 million by 1990 and 47 U.S. Department of Commerce, op. cit., footnote 22. qBChar[es River Associates report prepared for the National Bu- 45 Ibid. reau of Standards, “Technological and Economic Assessment ot 46R. Nathan Katz, “Applications of High Performance Ceramics Advanced Ceramic Materials, Vol. 2: A Case Study of Ceramics in in Heat Engine Design, ” Materials Science and Engineering 71 ;227- Heat Engine Applications, ” NBS-GCR 84-4760-2, August 1984. 249, 1985. qgRICherSon, op. cit., footnote 4. Ch. 2—Ceramics . 59 , I* (w 1 2 3 4 5 6 7 8 9 110 11 12 1,3 14 15 119 21( 1 1, ,1 \ ~ , I I I I ! I ~ I 1 ,! t j I ; I , ; ! [ ‘1 ill:ll ’161 l:” 1 ’11 I I Ii Photo credit: The Garrett Corp Ceramic turbocharger turbine rotors elude exhaust port liners, cam followers, and market of $60 million could be generated for ce- turbocharger components. To date, U.S. firms ramic turbocharger rotors by the year 2000.50 have not introduced these products, although The ceramic turbocharger rotor has a signifi- R&D programs continue. cance far beyond its contribution to the perform- The United States remains behind Japan in ance of the engine. it is regarded as a forerun- procuring the advanced production equipment ner technology to far more ambitious ceramic needed to produce ceramic turbocharger rotors. engines, such as the advanced gas turbine. De- U.S. automotive companies do not appear to sign, fabrication, and testing methods developed have the same level of confidence as the Japanese for the turbocharger rotor are expected to serve that a ceramic turbocharger rotor market will de- as a pattern for subsequent ceramic engine tech- velop. In spite of this, U.S. industry is still fund- nology efforts. ing considerable R&D on ceramic turbocharger rotors. One study has estimated that if a ceramic 5’JElaine P. Roth man, “Advanced Structural Ceramics: Techni- cal/Economic Process Modeling of Production and a Demand Anal- rotor price of$15 can be reached and if perform- ysis for Cutting Tools and Turbochargers, ” Materials Systems Lab- ance and reliability are acceptable, a worldwide oratory, Massachusetts Institute of Technology, August 1985. 60 . Advanced Materials by Design Diesel Engines as those in automobiles.51 Level three would re- quire an insulating ceramic, probably zirconia or There are several levels at which ceramics a zirconia-based composite. Level three is the could be incorporated in diesel engines, as shown level at which the most significant improvements in table 2-9. The first level involves a baseline i n fuel efficiency wouId be realized. However, diesel containing a ceramic turbocharger rotor the current zirconia and alumina-zirconia trans- and discrete ceramic components. The second formation-toughened ceramics are not reliable at level adds a ceramic cylinder and piston, and the high stress of the piston cap and do not have eliminates the cooling system, The ceramic used a low enough coefficient of friction to withstand at this level would provide high-temperature the sliding contact stress of the rings against the strength, rather than thermal insulation. cylinder liner. These materials do seem to have The third level would use ceramics for thermal adequate properties, however, for other compo- insulation in the hot section as well as in the ex- nents such as the head plate, valve seats, and haust train. Turbocompounding would be used valve guides. 52 to recycle energy from the hot exhaust gases to Emission requirements will likely affect the size the drive train. The fourth level would use ad- of the diesel market for passenger cars and trucks. vanced minimum friction technology to improve Diesel engines generally produce a high level of the performance of the engine. Appropriate particulate emissions. The higher operating tem- aspects of this technology also could be used at peratures of the adiabatic diesel could reduce levels one, two, or three. emissions or permit emission control devices to The four levels place different demands on the operate more efficiently. The market for ceram- ceramic materials. Levels one and two require ics could also be affected by the fact that one a low-cost, high-strength material, but without in- major candidate for diesel emission control is a suIating properties; sintered silicon nitride or sili- ceramic particle trap. However, such a trap is con carbide would be possibilities here. It has likely to be expensive. been suggested that level two represents the best JI Katz, op. Cit. r footnote 46. compromise for light-duty ceramic diesels such J~Richer50n, op. cit., fOOt nOte 4. Table 2-9.—Future Diesel Engine Technology Development Scenario Technology level Engine configuration Potential ceramic components Potential payoffs 1 State-of-the-art engine, Turbocharger Improved performance turbocharged Valve train components Reduced cost? Prechamber, glow plugs Early manufacturing experience 2 Uncooled, non-adiabatic Turbocharger Reduced weight - efficiency gain (no water or air cooling) Valve train components Gives option to improve aero- (no turbo-compounding) Piston, cap dynamics - efficiency gain Cylinders, liners Reduced maintenance Reduced engine systems cost? Flexibility of engine placement Adiabatic turbo-compound Turbocharger Very significant reduction in Turbo-compound wheel specific fuel consumption Valve train components Improved aerodynamics Piston, cap Reduced maintenance Cylinders, liners Exhaust train insulation Minimum friction technology Air bearings Lower specific fuel consumption (could be combined with 1, High-temperature rings 2 or 3) High-temperature bearings Nongalling wear surfaces Low friction liquid, lubricant-free bearings SOURCE R Nathan Katz, “Applications of High Performance Ceramics in Heat Engine Design,” Materials Science and Engineering 71:227-249, 1985, Ch. 2—Ceramics ● 67 —. Ceramic coatings may be an alternative to Motor Co. also showed a 5- to 9-percent increase monolithic ceramics in diesel applications. Zir- in fuel efficiency in an uncooled test engine fitted conia coatings can be plasma-sprayed onto metal with ceramic inserts, compared to the baseline cylinders to provide thermal insulation. In a joint water-cooled design. 56 program between the U.S. Army Tank Automo- Charles River Associates predicts that the un- tive Command and Cummins Engine Co., the cooled ceramic diesel engine system will be the combustion zone of a commercial Cummins NH first to be commercialized. 57 It projects that the diesel engine was coated with a zirconia-based initial introduction will be in the late 1980s to ceramic and installed in a 5-ton Army truck, early 1990s, and could account for 5 percent of minus the cooling system. The engine accumu- new engines manufactured in 1995. lated over 9,375 miles (1 5,000 kilometers) of suc- cessful road testing. 53 The current state-of-the-a t-t This projection is more optimistic than the thickness of zirconia coatings is 0.03 to 0.05 inch above discussion would imply. Zirconia materi- (0.762 to 1.27 millimeter). It is estimated that als do not yet exist that can be used for level three thicknesses of 0.125 inch (3. 175 millimeter) will technology, wherein the greatest fuel efficiencies be required to provide thermal insulation com- are expected. It remains to be seen whether the parable to monolithic zirconia.54 The coating is elimination of the cooling system will provide not as impermeable or as resistant to thermal sufficient incentives to U.S. automakers to com- shock as the monolithic zirconia. However, the mercialize level two ceramic technology. coated metal part has greater strength and tough- Japan in particular has very active research ness than the all-ceramic part. programs both in material and diesel engine In the past, confusion has arisen because iden- development. IsUzU, the strongest ceramic engine tical configurations of ceramic and metal engines advocate of all of the Japanese auto companies, have not been compared. It is important to sep- has reported more than 300 miles (480 kilome- arate out the configuration options, such as ters) of road testing and is projecting 1990 pro- turbocharging, turbocompounding, heat recov- duction, 58 Toyota has plans to produce an all ce- ery, cooling, etc., from the material options to ramic diesel, using injection molded and sintered isolate the benefits of the use of ceramics. Fail- silicon nitride by 1992. Every part will be proof ure to do this has led to overestimation of the tested. The largest Japanese automakers all main benefits of ceramics. For instance, a recent study tain extensive research activities in the area o of a ceramic diesel design funded by the Depart- ceramic engines.59 ment of Energy indicates that: Automotive Gas Turbines . . . a practical zirconia-coated configuration with a cooled metal liner, intercooled, with combined The major incentive for using ceramics in tur- turbocompounding and Rankine cycle exhaust bines is the possibility of operating the engine at heat recovery{ provides a 26 percent increase in turbine inlet temperatures up to about 2500° F thermal efficiency over a metallic, cooled, tur- 55 (1371° C), compared with superalloy designs, that bocharged, intercooled, baseline engine. are limited to about 1900° F (1038° C) without However, the bulk of the performance im- cooling. This temperature difference translates provement was attributed to the turbocom- into an increased thermal efficiency from around pounding and the Rankine cycle exhaust heat re- covery. Only 5.1 percent was attributed to the improved thermal insulation. Recent work at Ford ‘] Katz, op. ctt,, Iootnote 46. “)’BJ)] Marrcl)er. Cummin\ En~lne Co,, personal c CJmmunic at Ion, Augu\t 1986. “T. ,Morel, et ~1., ‘ ‘lMet hods tor Heat Tra n ster and T herma I Anal- ysis ot lnsulateci Dwwl\, ” Pro( eedlng.$ of the -Y ~r~ ~1 [jtomo[ii tJ T<>< /l- nolog~, Dc’y c’lopment ~-(~ntr,]ctor$ Coord/nat/on ,~leeting ~ IXarhorn, JM I Soc Iety of ,Automotive Engineers, March 1986). 62 . Advanced Materials by Design 40 percent to nearly 50 percent.60 Power in- gas turbine engine is designed to provide about creases of 40 percent and fuel savings of around 100 horsepower with fuel efficiencies of about 10 percent have been demonstrated in research 43 miles per gallon for a 3,000-pound automo- engines containing ceramic components.61 Other bile.65 potential advantages include reduced engine size The automotive gas turbine would be a more and weight, reduced exhaust emissions, and the revolutionary application of ceramics than the capability to burn alternative fuels, such as diesel. The diesel engine is a familiar technology powdered coal. and incorporation of ceramics can occur in Structural ceramics represent an enabling tech- stages, consistent with an evolutionary design. nology for the automotive gas turbine; i.e., ce- The gas turbine, on the other hand, represents ramics are the key to designing and manufactur- a completely new design requiring completely ing an automotive turbine that can compete in new tooling and equipment for manufacture, Be- cost or performance with current gasoline and cause of the remaining technical barriers to ce- diesel engines. Extensive design, materials, and ramic gas turbines and the fact that they repre- engine efforts have been made over the past 15 sent a complete departure from current designs, years in the United States, Europe, and Japan. it is unlikely that a ceramic gas turbine passen- These efforts have resulted in significant progress ger car could be produced commercially before in design methods for brittle materials, the prop- 2010.66 In view of this long development time, erties of silicon nitride and silicon carbide, fabri- it appears possible that this propulsion system cation technology for larger and more complex could be overtaken by other technologies, includ- ceramic components, NDE and proof testing, and ing the ceramic diesel. One factor that would engine assembly and testing. favor the turbine engine would be dramatically increased fuel costs. In the case that traditional Ceramic components have been operated in fuels became scarce or expensive, the turbine’s prototype turbine engines in West Germany, capability to burn alternative fuels could make Sweden, Japan, and the United States. The tests it the powerplant of choice in the future. in the United States have involved highly in- strumented development engines in test cells. 62 In summary, the outlook for ceramic heat en- Current programs have achieved over 100 hours gines for automobiles appears to be highly un- of operation at temperatures above 2000° F certain. The performance advantages of ceramic (1093° C).63 These achievements, although im- engines are more apparent in the larger, more pressive, are still far from the performance re- heavily loaded engines in trucks or tanks than quired of a practical gas turbine engine, which they are in automobiles. Ceramic gas turbines and will involve continuous operation above 2500° adiabatic diesel designs do not scale down in size F (1 3710 C). The limiting component in these en- as efficiently as reciprocating gasoline engines. 67 gines appears to be the rotor, which must spin Thus, if the trend toward smaller automobiles at about 100,000 rpm at these temperatures. The continues, reciprocating gasoline engines are likely most reliable rotors available have generally been to be favored over advanced ceramic designs, manufactured in Japan.64 The target automotive The prevailing approach of U.S. automakers– 60 that of waiting to see if a clear market niche for John Mason, Garrett Corp., presentation at the Society of Au- tomotive Engineers International Congress and Exposition, Detroit, ceramics develops before investing heavily in the Ml, February 1986. technology—is likely to mean that previous fore- 61 David W, Richerson and K.M. johansen, ‘‘Ceramic Gas Tur- casts of the U.S. ceramics heat engine market, bine Engine Demonstration Program, ” final report, DARPA/Navy contract NOO024-76-C-5352, May 1982, which cluster in the $1 to $5 billion range by the b’David W, Richerson, “Evolution in the U.S. of Ceramic Tech- nology for Turbine Engines, American Ceramics Society Bulletin b5Ka{z, op. cit., footnote 46. 64(2):282-286, 1985. bbRicherson, op. cit., fOO{rlOte 4. b~Mason, op. cit. bzu .s. congress, Office of Technology Assessment, Increased Au- bJRic hard Helms, General Motors Corp., presentation at the tomobile Fuel Efficiency and Synthetic Fuels: Alternatives for Re- Society of Automotive Engineers International Congress and Expo- ducing Oil Imports, OTA-E-185 (Washington, DC: U.S. Government sltlon, Detroit, Ml, February 1986. Printing Office, September 1982), p. 145. — Ch. 2—Ceramics ● 63 2. Turbine Shroud 3. Turbine Rotor 4. Inner Diffuser HSG 5. Outer Diffuser HSG 6. Turbine Backshroud 9. Combustor Baffle 10. Bolts 11. Regenerator Shield 12. Alumina-Silica Insulation Photo credit: The Garrett Corp. Prototype ceramic gas turbine engine components 64 . Advanced Materials by Design year 2000, are too optimistic. On the other hand, been tried, but have been successful only in a the Japanese approach, in which ceramics are few components and still require further devel- steadily being incorporated in engines on a more opment. A military diesel with minimal cooling experimental basis, reflects greater faith in the fu- achieved primarily with ceramic coatings could ture of the technology. If a substantial automo- be produced by 1991. Engines containing more tive market for ceramics does develop, heat en- extensive ceramic components are not likely to gine applications for ceramics would be one of appear before about 1995 to 2000.71 the most highly leveraged in terms of economic benefits and jobs.68 69 Turbines Military Applications and Production Turbine engines are in widespread military use for aircraft propulsion, auxiliary power units, and Production of ceramics for military applications other applications. They are being considered for is projected to expand substantially during the propulsion of tanks, transports, and other mili- next 25 years.70 Near-term growth is expected for tary vehicles. Ceramics have the potential to armor, radomes and infrared windows, bearings enable advanced turbines to achieve major im- for missiles, and rocket nozzles (carbon-carbon provements in performance: as much as 40 per- composites and ceramic-coated carbon-carbon cent more power, and fuel savings of 30 to 60 composites). New applications are likely to be percent.72 In addition, they offer lower weight, laser mirrors, gun barrel liners, rail gun compo- longer range, decreased critical cross section, and nents, and turbine and diesel engine compo- decreased detectability. nents. Ceramics and ceramic composites in many cases offer an enabling capacity that will lead to Design and material technologies are available applications or performance that could not other- in the United States to produce high-performance wise be achieved. Some of the resulting technol- ceramic-based turbine engines for short-life ap- ogy will be suitable for commercial spinoffs if plications such as missiles and drones. Further- acceptable levels of fabrication cost and quality- more, it appears that these engines have poten- control cost can be attained. tial for lower cost than current superalloy-based short-life engines.73 Diesels Longer-life engines will require considerable In military diesels, ceramics provide much the development to demonstrate adequate reliabil- same benefits as in commercial diesels. Of par- ity. This development must address both design ticular interest to the military is the elimination and materials in an iterative fashion. Although the of the cooling system to achieve smaller pack- use of ceramic thermal barrier coatings in metal aging volume and greater reliability. Considerable turbines is well under way, new turbines designed progress has been made through the use of ce- specifically for ceramics are not likely to be avail- ramic coatings. Monolithic ceramics have also able before the year 2000, bgLarry f?. Johnson, Arvind T.S. Teotia, and Lawrence G. HiII, “A Structural Ceramic Research Program: A Preliminary Economic Anal- ysis, ” Argonne National Laboratory, ANL/CNSV-38, 1983. 71 Ibid. bgcharles River Associates, op. cit., footnote 48. 721 bid. zORicherSon, op. Cit., footnote 4. 731 bid. FUTURE TRENDS IN CERAMICS Ceramic Matrix Composites Major improvements in the fracture properties that do not fail catastrophically and therefore of ceramics have been obtained by reinforcing have mechanical properties that are very differ- matrices with continuous, high-strength fibers. ent from those of monolithic ceramics, as shown Optimum microstructure result in composites i n figure 2-4. The most developed composites to Ch. 2—Ceramics s 65 Figure 2-4.– Load-Deflection Curve for a Nicalon ods, such as open casting and centrifugal cast- Fiber-Reinforced Silicon Nitride Composite ing; and such new heating methods as microwave and plasma sistering.75 900 a n In the future, however, chemical approaches ~ to the fabrication of ceramics will probably be mu) 700 L preferred to the traditional methods of grinding 500 m and pressing powders. Chemical routes to ceram- ics include such techniques as sol-gel process- ing, chemical vapor infiltration of ceramic fiber ? 300 “ p preforms, and in-situ formation of metal-ceramic 2 composites by reactions between liquid metals UI and appropriate gases.76 77 These techniques af- ford greater control over the purity of the ceramic o 0.6 1.8 3.0 and over its microstructure. it has been estimated Extreme fiber strain (%) that 50 percent of structural ceramics will be Dotted line indicates point at which fracture would occur without fiber reinforcement. processed chemically by the year 2010.78 SOURCE: Joseph N. Panzarino, Norton Co., Personal communication, Sept. 3, 1987. Biotechnology date are silicon carbide fiber-reinforced glass- Structural ceramics could have a significant in- ceramic matrices. teraction with the developing field of biotechnol- Recent analysis suggests that fibers resist the ogy in the future. Ceramics could be used exten- opening of a matrix crack by frictional forces at sively in fermenters, and they are likely to be the matrix-fiber interface.74 One of the important important in a broad range of product separation results is that the strength of the composite be- technologies. comes independent of preexisting flaw size. This means that strength becomes a well-defined Fermenters property of the material, rather than a statistical Most current fermenters are made of316 grade distribution of values based on the flaw popu- stainless steel .79 Steel fermenters suffer from sev- lations. eral disadvantages, including contamination of CMCs present an opportunity to design com- the cultures with metal ions, corrosion caused posites for specific engineering applications. This by cell metabolizes or reagents, and leaks around will require a detailed understanding of the gaskets and seals during sterilization and temper- micromechanics of failure and explicit quantita- ature cycling. tive relations between mechanical properties and Glass-lined steel bowls are sometimes used, microstructural characteristics. The most impor- especially for cell cuItures, which are more sen- tant breakthrough in ceramic composites will sitive to contamination than bacterial cultures. come with the development of new high-temper- However, the thermal expansion mismatch be- ature fibers that can be processed with a wider range of matrix materials. TSRichard po~r, Ceramics Processing Research Laboratory, MIT, personal communication, April 1987. Tssee for example David W. Johnson, Jr., “Sol-Gel Processing of New Processes for Ceramics Ceramics and Glass,” American Ceramic Society L?u//etin 64(1 2): 1597-1602, 1985. Several forming and sintering techniques may zTCommonly ca[l~ the Lanxide process, this technique has re- offer the potential for significant improvements cently been extended to permit the fabrication of ceramic fiber- reinforced composites, See Materials and Processing Repofl, MJT in the microstructure of ceramics produced from Press, vol. 2, June 1987. powders. These include advanced casting meth- Z13R. Nathan Katz, presentation at the Society of Automotive Engi- neers International Congress and Exposition, Detroit, Ml, Febru- 74 D.B. Marshall and A.G. Evans, “The Mechanics of Matrix Crack- ary 1986. ing in Brittle-Matrix Fiber Composites,” Acta Meta//urgica zgRichard F. Geoghegan, E.1. du Pent de Nemours & Co., per- 33(1 1):2013-2014, 1985. sonal communication, August 1986. 66 . Advanced Materials by Design tween the glass lining and the metal causes prob- up to production units, there will probably be a lems during steam sterilization. large increase in the demand for specially modi- fied silica and alumina column packing materials. Ceramics offer a solution to these problems be- cause of their chemical stability and low thermal expansion. Ceramics could be used in the bowl Energy Production and agitator, as well as in the peripheral plumb- Power Turbines ing joints and agitator shaft seal to prevent leaking. The performance requirements for power tur- bines are much greater than those for automo- Separation Technology tive gas turbines.84 Power turbines must have a lifetime of 100,000 hours, compared with about Separation and purification of the products of 3,000 hours for the auto turbine. In addition, the cell and bacterial cultures is a key aspect of bio- consequences of power turbine failure are much technology. In general, the separation techniques greater. In light of these facts, a recent report has are based less on filtration than on active inter- concluded that power turbines will be commer- actions between a solid phase and the liquid mix- cialized after automotive gas turbines. 85 ture, as in chromatography. For instance, biolog- ically produced insulin is now being purified with Although some of the processing technology a chromatographic process based on a modified developed for the auto turbine may be applica- silica material. 80 Silica or alumina particles can ble to power turbines, the scale-up from a rotor also be used as a solid support for attaching mon- having a 6-inch diameter to one having a much oclonal antibodies, which bind to specific proteins larger diameter may require completely new and effect a separation by affinity chromatogra- fabrication techniques. The larger ceramic struc- phy.81 tures may also require different NDE techniques to ensure reliability. The strength and hardness of the ceramics are key to the avoidance of deformation of the ce- Thus, use of monolithic ceramics in the criti- ramic particles under conditions of high through- cal hot-section components of power turbines is put.82 In the future, the most efficient processes not anticipated in the next 25 years. However, could be hybrids based on both filtration and ceramics may find applications in less critical chromatography. 83 As these processes are scaled structures, such as combustor linings. in addition, ceramic coatings could be used to augment the high-temperature resistance of cooled superalloy aojoseph ). Kirkland, El. du Pent de Nemours & CO., Personal 86 communication, August 1986. rotor blades, al George WhiteSides, Department of Chemistry, Harvard U niver- sity, personal communication, August 1986. 821 bld . sAJohnson and Rowcliffe, op. Cit., footnote 43 83Mlche[ [e BetrldO, Celanese Research Corp., perSOnal Commu- 851 bid. nication, August 1986. Mlbid. RESEARCH AND DEVELOPMENT PRIORITIES In fiscal year 1987, the U.S. Government spent cent, respectively. The following hierarchy of about $65 million on structural ceramics R&D (ta- R&D priorities are based on the opportunities ble 2-10). R&D expenditures in private industry identified above. These are then correlated with may be roughly comparable.87 88 DOE and DoD the actual spending on structural ceramics R&D spent the largest proportions, at 55 and 28 per- in fiscal year 1985. aTCharles River Associates, op. cit., footnote 48, p. 38. in all advanced ceramics, including structural and electronic ce- 88 A recently completed survey by the United States Advanced ramics, at $153 million in 1986, somewhat greater than the total Ceramics Association places the private industry R&D investments government expenditure of $100 to $125 million. Ch. 2—Ceramics . 67 Table 2-10.—Structural Ceramic Technology: Federal Government Funded R&D (in millions of dollars) FY 1983 FY 1984 FY1985 FY1986 FY1987 Department of Energy: Conservation and renewable energy: Vehicle propulsion ...... 11.4 12.7 11.9 10,0 12.0 Advanced materials , ...... 3.2 5.1 6.0 8.7 14.0 Industrial programs ...... 1.0 2.3 1.7 1.5 1.9 Energy utilization research ...... 0.5 1.5 1.8 1.8 2.0 Fossil energy: Advanced research and technology development ...... 1.0 1.1 1.5 1.2 1.9 Energy research: Basic energy science ...... 3.0 4.4 4.6 4.5 4.2 NASA: Lewis Research Center ...... 3.0 2.5 5.4 4.5a 4.6a National Science Foundation ...... 2.9 3.3 3.6 3.6 3.7 National Bureau of Standards ...... 2.2 3.0 Department of Defense: Defense ARPA ...... 7.7 8.2 9.4 10.0 7,3 U. S. Air Force ...... 3.0 3.4 4.7 4.7 5.1 U.S. Army ...... 4.7 6.0 2.5 4.4b 3.6C U.S. Navy ...... 1.2 —1.3— 1.4 2.3 1.9 Total ...... 42.6 51.8 54.5 59.4 65.2 a lncludes $1 6 million for Manpower Salaries. b lncludes $40 million for TACOM Diesel c lncludes $20 million for TACOM Diesel SOURCE’ Robert B. Schulz, Department of Energy. Very Important Environmental Behavior Processing Science Many of the applications for ceramics men- tioned above require long-term performance in There is a great need for generic research to severe environments. To develop higher temper- support the development of practical manufac- ature, corrosion-resistant materials, it is necessary turing technologies within industry. The agenda to understand the long-term behavior of candi- for such research is long, but includes such topics date ceramic materials in the anticipated envi- as: ronments: ● development of near-net-shape processes; ● For heat engine applications, the general re- ● development of pure, reproducible pow- quirement is to understand the mechanical ders, whiskers, and fibers that can be formed and chemical behavior of advanced ceram- and densified with a minimum of intermedi- ics such as silicon nitride, silicon carbide, zir- ate steps; role of solution chemistry in pow- conia, and CMCs based on these materials der preparation and control of interface in environments of 1000° to 1400° C (1 8320 properties in CMCs; to 2552° F) in air, carbon monoxide, and car- ● development of practical in-process inspec- bon dioxide. tion devices and techniques to identify prob- ● In ceramic wear parts, it is necessary to un- lems at the earliest possible stage in the derstand the interrelationships of wear, ero- process; sion, and toughness in the presence of lu- ● iterative development of new equipment bricating fluids and gases. Generally, wear such as hot isostatic presses (HIPs) and mul- parts include hard materials such as tungsten tistage processes such as sinter-HIP, with em- carbide, titanium diboride, and materials that phasis on scaling up to commercially viable have good lubrication characteristics, such size; and as silicon nitride. ● understanding of the relationships between ● Because heat exchangers generally fail as a coating process variables and final proper- result of slow corrosion at high temperatures, ties and performance of ceramic coatings. it is important to understand the chemical 68 . Advanced Materials by Design processes of corrosion in such environments itself must be tested or additional models must as salts of sodium, potassium, magnesium, be available to predict the effects of a particular calcium, vanadium, and mixed metals. In flaw on a particular structure. addition to existing materials (e. g., silicon carbide, cordierite, and zirconium silicate), Interphase in CMCs newer materials, including silicon nitride and The interphase between ceramic fiber and ma- CMCs, should be investigated. Corrosion- trix is critical to the static strength, toughness, and resistant ceramic coatings may become im- long-term stability of the CMC. Very little is known portant here. about the relationship between the properties of ● Considering the large size of the potential the interphase and these overall CMC properties. markets in bioceramics, it is critical to un- The capability to modify the surface chemistry derstand the long-term effects of body fluids of ceramic fibers and whiskers to provide opti- on chemical structure and mechanical prop- mum compatibility between reinforcement and erties. In view of the many years that ceramic matrix could yield remarkable improvements in implants must serve without failure, the in- ceramic performance and reliability. teraction between slow crack growth and the body environment should be investigated. . The long-term environmental stability of ad- Important vanced chemicalIy bonded ceramics is cru- cial to their effectiveness in construction and Joining of Ceramics other applications. The deterioration of the In most applications, ceramics are not used properties of some advanced cements in the alone; rather, ceramic components are part of presence of moisture remains a problem, larger assemblies. Therefore, the ceramic must and the chemical degradation of the fiber in- be joined to more conventional materials in the terface in reinforced cements and concretes assembly to function properly. Broad research on has limited the structural uses of these ma- joining of ceramics to metals, glasses, and other terials. ceramics could have a decisive impact on future use of monolithic ceramics, coatings, and CMCs. Reliability The key to joining is an understanding of the No factor is more important to the success of surface properties of the two materials and of the ceramics in all of the applications discussed than interface between them. In general, the interface reliability. Because the performance specifica- is a critical point of weakness in discrete ceramic tions and environment of each application are components such as those in heat engines, in ce- different, it is necessary to establish the most ramic coatings on metal substrates, and in ce- appropriate and cost-effective NDE methods for ramic fibers in CMCs. each one. Principal needs in this area are in the strength- To distinguish between critical flaws and harm- ening and toughening of joints, an understand- less flaws, models need to be developed for pre- ing of their high-temperature chemistry, and im- dicting the service life of ceramic parts contain- proved resistance to corrosion in the various ing various kinds of flaws. Such models must environments of interest. As with solution meth- depend heavily on information derived from the ods in powder preparation, chemistry will make categories of environmental behavior of ceram- a crucial contribution in this area. ics and CMC failure mechanisms discussed above. Beyond a dependence on intrinsic flaws in the Tribology of Ceramics material, however, service life also depends on the location and nature of the flaw within the Tribology, the study of friction, wear, and lu- structure itself. it is not sufficient to characterize brication of contiguous surfaces in relative mo- the behavior of a coupon of the material from tion, is of key importance in terms of ceramic which a structure is made; either the structure wear parts and heat engine components. Lubri- Ch. 2—Ceramics ● 69 cation is a particularly serious problem in ceramic fiber-powder combinations. Fundamental under- engines because of their high operating temper- standing of the failure mechanisms in CMCs atures. would provide guidance for development of new, tougher ceramics. This would include investiga- Ordinary engine oils cannot be used above tion of: multiple toughening techniques, such as about 350°F (177°C). For operating tempera- transformation toughening and whisker reinforce- tures of 500° to 700°F (260° to 371° C), synthetic ment; the role of interphase properties in frac- liquids such as polyol esters are available, but are ture; and failure mechanisms in continuous-fiber extremely expensive and require further devel- CMCs. opment. In a low-heat rejection (adiabatic) ce- ramic engine, cylinder liner temperatures may reach 1000° to 1700° F (538° to 927° C), depend- Desirable ing on the insuIating effectiveness of major en- Chemically Bonded Ceramics gine components. For this elevated temperature regime, synthetic lubricants cannot be used ef- Chemically bonded ceramics (CBCs) offer great fectively. promise for low-cost, net-shape fabrication of structures in such applications as wear parts and One approach to this problem is to use solid construction. Recent improvements in the ten- lubricants that would become liquid at elevated sile strength of CBCs suggest that the limits of this temperatures; however, no such lubricants exist key engineering property are far from being real- for use in the environments envisioned (high- ized. Further research is required in reduction of temperature, corrosive gases). Moreover, the dis- flaw size, long-term stability in various environ- tribution of solid lubricant around the engine is 89 ments, and the properties of the interphase in a persistent problem . fiber-reinforced cements and concretes. A second method involves modifications of the * * * surface of the component to produce self-lubri- cation. The lubricant can be introduced through Table 2-11 shows that the actual structural ce- ion implantation directly into the surface (to a ramics R&D spending in fiscal year 1985 for all depth of several micrometers) of the component; government agencies corresponds roughly with it then diffuses to the surface to reduce friction. the priority categories recommended above, al- Some metal or boron oxides show promise as lu- though specific projects differ. Processing re- bricants. Alternatively it is possible to use surface search accounted for the lion’s share, with 76 coatings of extremely hard ceramics such as the percent. No separate estimate was available of carbides and nitrides of zirconium, titanium, or research on the interphase in CMCs; a portion hafnium, without any lubrication. At present, of this work is included under CMC fabrication, these techniques all lead to sliding friction coeffi- listed here as a subcategory of processing. Also, cients that are roughly four times higher than no separate figure was obtained for Federal ex- those achieved at low temperatures with engine penditures on advanced cements and concretes. oils.90 Further research is clearly needed. In fiscal year 1983, however, total U.S. Govern- ment and industry funding of cement research Failure Mechanisms in CMCs was estimated at only $1 million, compared with a portland cement sales volume over $1 billion. 91 CMCs offer the best solution to the problem Assuming that the current breakdown of Federal of the brittleness of ceramics. However, this field ceramics research is similar to that in fiscal year is still in its infancy, and research is character- 1985, a comparison of table 2-11 with the pri- ized by a very empirical approach to mixing, orities listed above suggests that greater empha- forming, densification, and characterization of sis should be placed on joining, tribology, and cement-based materials. 8gManfred Kar-rllnsky, Surface Treatment science International, personal communication, August 1986. 91 National Research Council, Transportation Research Board, op. 901 bld cit., footnote 30. 70 ● Advanced Materials by Design Table 2-11.– Breakout of the Fiscal Year 1985 Structural Ceramics Budget According to the R&D Priorities Cited in the Text FY 1985 Research area budget percentage Processing: Powder synthesis ...... 4 Monolithic fabrication ...... 32 Composite fabrication ...... 32 Component design and testing . . . . 4 Coatings ...... 4 Machining...... <1 Subtotal ...... 76 Environmental behavior ...... 4 Reliability: Modeling...... 2 Time dependent behavior ...... 1 Nondestructive evaluation ...... 3 Microstructure evaluation ...... 4 Subtotal ...... 10 Interphase in composites ...... no separate figure Tribology...... 2 Joining ...... 3 Fracture ...... 5 Standards ...... <1 Total ...... 100% SOURCE: S.J. Dapkunas, National Bureau of Standards, unpublished survey, 1985 Chapter 3 Polymer Matrix Composites ',COHTENTS Page ● ...... 111 it' ••..., • t". f' t ...... " " " •• " 73 . 74 Oi,;~·M.;ir~~P~~::::::::::::::::::::::::::::::::::: :. 76 .'. ".>.)~ +'.\ ta-,',,"' .: •• ~ .. '...... ,;;~.~-~ i ..... "...... ' ...... 76 ~". "'_~ __ , ,cc _ ,," '. " • ~rw:ud".'~',. 'f~.-,._4( ~'~_ ••• ~ ~ .-.~. ""*-,f' -0 ...... 77 . 77 . 78 . 79 . 79 . 79 . 81 . 82 . 82 . 82 . 83 . 84 . 85 • • • • • .. ' ~ .. , ~<, .~' ...... ' .• • N • ... '*' ...... 86 . 86 .', '"' ~ ~, " ...... -.". - ..... Ii' It.' •• iI!I'-" ...... 87 • ~t l' , .....'. ·0 « ., e' ...... ~ ...... 89 ·Pohmter:hI.rtx:~~. "',~ ,., . '...... 90 . 90 . 90 . 91 . 91 .. ' .... ' ...... " ...... 91 . 92 . 93 . 93 . 94 *,- ...... l' " ...' ~ ...... 95 ~_ ", ;. ~ F~rea ~-, .. 1/. " -':~-~~;.t~~~~~:T:~~lc;~.:: Page iJi:,~:~1'~., ., ,. . . r~" ...:.- .. .- ... "...... 75 " '.rison ~~.I-~h~'cs of Thermoset and Thermoplastic Matrices . . 76 l:. . ~sOtf.(1 the Speeific Strength and Stiffness of Various Composites and "'> -.:::':~',' ••• ~ ;...... - .- ...... ".' .... ,. " " •••• " ...... 77 - 'M~toMfJQsjte Aircraft Structure " ...... 83 T.~ •• '" 'Htif.. . ," Page . 79 '~~~'~"'1;~=~~ni;h.;d ~;.d: ~~t::~~d 'Fi~ld~. .• : >.. l~llnspectiomOf Polymer ~tri)(Composite Structures ...... 81 ~a..3 .. 8udaets for Poly,., Matrix Composite-.R&O in Fiscal Years 1985 to 1987 ...... 93 , ''''!.,': ., >.. ~ 0 Chapter 3 Polymer Matrix Composites FINDINGS Polymer matrix composites (PMCs) are com- typically involves placement of sequential layers prised of a variety of short or continuous fibers of polymer-impregnated fiber tapes on a mold bound together by an organic polymer matrix. surface, followed by heating under pressure to Unlike a ceramic matrix composite (CMC), in cure the lay-up into an integrated structure. Al- which the reinforcement is used primarily to im- though automation is beginning to speed up this prove the fracture toughness, the reinforcement process, production rates are still too slow to be in a PMC provides high strength and stiffness. The suitable for high-volume, low-cost industrial ap- PMC is designed so that the mechanical loads to plications such as automotive production lines. which the structure is subjected in service are New fabrication methods that are much faster supported by the reinforcement. The function of and cheaper will be required before PMCs can the matrix is to bond the fibers together and to successfully compete with metals in these appli- transfer loads between them. cat ions. Polymer matrix composites are often divided Applications and Market into two categories: reinforced plastics, and “ad- Opportunities vanced composites. ” The distinction is based on the level of mechanical properties (usually strength Aerospace applications of advanced compos- and stiffness); however, there is no unambiguous ites account for about 50 percent of current sales. line separating the two. Reinforced plastics, which Sporting goods, such as golf clubs and tennis are relatively inexpensive, typically consist of rackets, account for another 25 percent. The polyester resins reinforced with low-stiffness glass sporting goods market is considered mature, with fibers. Advanced composites, which have been projected annual growth rates of 3 percent. Au- in use for only about 15 years, primarily in the tomobiles and industrial equipment round out aerospace industry, have superior strength and the current list of major users of PMCs, with a stiffness, and are relatively expensive. Advanced 25 percent share. composites are the focus of this assessment. The next major challenge for PMCs will be use Chief among the advantages of PMCs is their in large military and commercial transport aircraft. light weight coupled with high stiffness and PMCs currently comprise about 3 percent of the strength along the direction of the reinforcement. structural weight of commercial aircraft such as This combination is the basis of their usefulness the Boeing 757, but could eventually account for i n aircraft, automobiles, and other moving struc- more than 65 percent. Because fuel savings are tures. Other desirable properties include superior a major reason for the use of PMCs in commer- corrosion and fatigue resistance compared to me- cial aircraft, fuel prices must rise to make them tals. Because the matrix decomposes at high tem- competitive. peratures, however, current PMCs are limited to The largest volume opportunity for PMCs is in service temperatures below about 600° F (316° C). the automobile. PMCs currently are in limited Experience over the past 15 years with advanced production in body panels, drive shafts, and leaf composite structures in military aircraft indicates springs. By the late 1990s, PMC unibody struc- that reliable PMC structures can be fabricated. tures could be introduced in limited production. However, their high cost remains a major bar- Additional near-term markets for PMCs include rier to more widespread use in commercial ap- medical implants, reciprocating industrial ma- plications. Most advanced PMCs today are fabri- chinery, storage and transportation of corrosive cated by a laborious process called lay-up. This chemicals, and military vehicles and weapons. 73 74 . Advanced Materials by Design Beyond the turn of the century, PMCs could of these materials. To generate improved mate- be used extensively in construction applications rials and to design and manufacture PMCs more such as bridges, buildings, and manufactured cost-effectively, the following needs should be ad- housing. Because of their resistance to corrosion, dressed: they may also be attractive for marine structures. Realization of these opportunities will depend on ● Processing Science: Development of new, development of cheaper materials and on designs low-cost fabrication methods will be critical that take advantage of compounding benefits of for PMCs. An essential prerequisite to this is PMCs, such as reduced weight and increased a sound scientific basis for understanding durability. In space, a variety of composites could how process variables affect final properties. be used in the proposed aerospace plane, and ● Impact Resistance: This property is crucial PMCs are being considered for the tubular frame to the reliability and durability of PMC of the NASA space station. structures. ● Delamination: A growing body of evidence Research and Development Priorities suggests that this is the single most impor- tant mode of damage propagation in PMCs Unlike most structural ceramics, PMCs have with Iaminar structures. compiled an excellent service record, particularly ● Interphase: The poorly understood interfa- in military aircraft. However, in many cases the cial region between the fiber and matrix has technology has outrun the basic understanding a critical influence on PMC behavior. INTRODUCTION Unlike a ceramic matrix composite, in which 40 years in applications such as boat hulls, cor- the reinforcement is used primarily to improve rugated sheet, pipe, automotive panels, and the fracture toughness, the reinforcement in a sporting goods. polymer matrix composite provides strength and Advanced composites, which have been in use stiffness that are lacking in the matrix. The com- for only about 15 years, primarily in the aero- posite is designed so that the mechanical loads space industry, consist of fiber and matrix com- to which the structure is subjected in service are binations that yield superior strength and stiffness. supported by the reinforcement. The function of They are relatively expensive and typically con- the relatively weak matrix is to bond the fibers tain a large percentage of high-performance con- together and to transfer loads between them, As tinuous fibers, such as high-stiffness glass (S-glass), with CMCs, the reinforcement may consist of par- graphite, aramid, or other organic fibers. This ticles, whiskers, fibers, or fabrics, as shown in fig- assessment primarily focuses on market oppor- ure 3-1. tunities for advanced composites. PMCs are often divided into two categories: Less than 2 percent of the material used in the reinforced plastics, and so-called advanced com- reinforced plastics/PMCs industry goes into ad- posites, The distinction is based on the level of vanced composites for use in high-technology ap- mechanical properties (usually strength and stiff- 1 plications such as aircraft and aerospace. In ness); however, there is no unambiguous line separating the two. Reinforced plastics, which are relatively inexpensive, typically consist of poly- ‘These advanced composites are primarily epoxy matrices rein- forced with carbon fibers. Reginald B. Stoops, R.B. Stoops& Asso- ester resins reinforced with low-stiffness glass ciates, Newport, Rl, “Manufacturing Requirements of Polymer Ma- fibers (E-glass). They have been in use for 30 to trix Composites, ” contractor report for OTA, December 1985. Ch. 3—Polymer Matrix Composites . 75 Figure 3-1.—Composite Reinforcement Types 1985, the worldwide sales of advanced composite materials reached over $2 billion. The total value of fabricated parts in the United States was about $1.3 billion split among three major industry cat- egories: 1) aerospace (50 percent), 2) sports equipment (25 percent), and 3) industrial and au- -——- - tomotive (25 percent).2 It has been estimated that advanced compos- ites consumption could grow at the relatively high rate of about 15 percent per year in the next few years, with the fastest growing sector being the aerospace industry, at 22 percent. By 1995, con- sumption is forecast to be 110 million pounds with a value (in 1985 dollars) of about $6.5 bil- lion. By the year 2000, consumption is forecast to be 200 million pounds, valued at about $12 billion.3 Based on these forecasts, it is evident that the current and near-term cost per pound of advanced composite structure is roughly $60 per pound. This compares with a value of about $1 per pound for steel or $1.50 per pound for glass fiber-rein- forced plastic (FRP). If these forecasts are correct, it is clear that over this period (to the year 2000), advanced composites will be used primarily in high value-added applications that can support this level of material costs. However, use of PMCs can lead to cost savings in manufacturing and service. Thus, the per-pound cost is rarely a use- ful standard for comparing PMCs with traditional materials. 2Strategic Analysis, Inc., “Strategies of Suppliers and Users of Ad- vanced Materials, ” a contractor report prepared for OTA, March 1987. SOURCE: Carl Zweben, General Electric Co J“Industry News, ” SAMPE Journal, July/August 1985, p. 89. 76 . Advanced Materials by Design CONSTITUENTS OF POLYMER MATRIX COMPOSITES Matrix Thermoplastics The matrix properties determine the resistance Thermoplastic resins, sometimes called engi- of the PMC to most of the degradative processes neering plastics, include some polyesters, poly - that eventually cause failure of the structure. etherimide, polyamide imide, polyphenylene sul- These processes include impact damage, delami- fide, polyether-etherketone (PEEK), and liquid nation, water absorption, chemical attack, and crystal polymers. They consist of long, discrete high-temperature creep. Thus, the matrix is typi- molecules that melt to a viscous liquid at the cally the weak link in the PMC structure. processing temperature, typically 500” to 700” F (260° to 3710 C), and, after forming, are cooled The matrix phase of commercial PMCs can be to an amorphous, semicrystalline, or crystalline classified as either thermoset or thermoplastic. solid. The degree of crystallinity has a strong ef- The general characteristics of each matrix type fect on the final matrix properties. Unlike the cur- are shown in figure 3-2; however, recently de- ing process of thermosetting resins, the process- veloped matrix resins have begun to change this ing of thermoplastics is reversible, and, by simply picture, as noted below. reheating to the process temperature, the resin can be formed into another shape if desired. Thermoses Thermoplastics, although generally inferior to Thermosetting resins include polyesters, vinyl- thermoses in high-temperature strength and esters, epoxies, bismaleimides, and polyamides. chemical stability, are more resistant to cracking Thermosetting polyesters are commonly used in and impact damage. However, it should be noted fiber-reinforced plastics, and epoxies make up that recently developed high-performance ther- most of the current market for advanced com- moplastics, such as PEEK, which have a semi- posites resins. Initially, the viscosity of these re- crystalline microstructure, exhibit excellent high- sins is low; however, thermoset resins undergo temperature strength and solvent resistance. chemical reactions that crosslink the polymer chains and thus connect the entire matrix to- Thermoplastics offer great promise for the fu- gether in a three-dimensional network. This proc- ture from a manufacturing point of view, because ess is called curing. Thermoses, because of their it is easier and faster to heat and cool a material three-dimensional crosslinked structure, tend to than it is to cure it. This makes thermoplastic ma- have high dimensional stability, high-temperature trices attractive to high-volume industries such resistance, and good resistance to solvents. Re- as the automotive industry. Currently, thermo- cently, considerable progress has been made in plastics are used primarily with discontinuous- improving the toughness and maximum operat- fiber reinforcements such as chopped glass or car- ing temperatures of thermosets. A bon/graphite. However, there is great potential for high-performance thermoplastics reinforced 4See, for instance, Aerospace America, May 1986, p. 22. with continuous fibers. For example, thermoplas- Figure 3-2.—Comparison of General Characteristics of Thermoset and Thermoplastic Matrices Process Process Use Solvent Resin type temperature time temperature resistance Toughness Thermoset ...... Low I High I High II High 1 Low Toughened thermoset ...... Lightly crosslinked thermoplastic. . . . . t 1 t t 1 Thermoplastic...... High Low 1 I Low Low I High I SOURCE: Darrel R. Tenney, NASA Langley Research Center. — Ch. 3—Polymer Matrix Composites ● 77 tics could be used in place of epoxies in the com- Of the continuous fibers, glass has a relatively posite structure of the next generation of fighter low stiffness; however, its tensile strength is com- aircraft. petitive with the other fibers and its cost is dra- matically lower. This combination of properties Reinforcement is likely to ensure that glass fibers remain the most widely used reinforcement for high-volume com- The continuous reinforcing fibers of advanced mercial PMC applications. Only when stiffness composites are responsible for their high strength or weight are at a premium would aramid and and stiffness. The most important fibers in cur- graphite fibers be used. rent use are glass, graphite, and aramid. Other organic fibers, such as oriented polyethylene, are also becoming important. PMCs contain about Interphase 60 percent reinforcing fiber by volume. The strength and stiffness of some continuous fiber- The interphase of PMCs is the region in which reinforced PMCs are compared with those of loads are transmitted between the reinforcement sheet molding compound and various metals in and the matrix. The extent of interaction between figure 3-3. For instance, unidirectional, high- the reinforcement and the matrix is a design vari- strength graphite/epoxy has over three times the able, and it may vary from strong chemical bond- specific strength and stiffness (specific properties ing to weak frictional forces. This can often be are ordinary properties divided by density) of controlled by using an appropriate coating on the common metal alloys. reinforcing fibers. Figure 3-3.—Comparison of the Specific Strength and Stiffness of Various Composites and Metalsa (0°) Graphite/epoxy / (0°) Kevlar/epoxy . . + (0°,900)Graphite/epoxy / . + (0°) S-glass/epoxy Graphite/epoxy + Sheet molding compound (SMC) 1 2 3 4 Specific tensile strength (relative units) Specific properties are ordinary properties divided by density; angles refer to the directions of fiber reinforcement a Steel: AlSl 4340; Alumlnum: 7075-T6; Titanium: Ti-6Al-4V. SOURCE: Carl Zweben, General Electric Co. 78 . Advanced Materials by Design Generally, a strong interracial bond makes the coupling is often intermediate between the strong PMC more rigid, but brittle. A weak bond de- and weak limits. The character of the interracial creases stiffness, but enhances toughness. If the bond is also critical to the long-term stability of interracial bond is not at least as strong as the ma- the PMC, playing a key role in fatigue properties, trix, debonding can occur at the interphase under environmental behavior, and resistance to hot/ certain loading conditions. To maximize the frac- wet conditions. ture toughness of the PMC, the most desirable PROPERTIES OF POLYMER MATRIX COMPOSITES The properties of the PMC depend on the ma- strength are relatively easy to compare, Advanced trix, the reinforcement, and the interphase. Con- composites have higher specific strengths and sequently, there are many variables to consider stiffnesses than metals, as shown in figure 3-3. In when designing a PMC. These include not only many cases, however, properties that are easily the types of matrix and reinforcement but also defined in metals are less easily defined in ad- their relative proportions, the geometry of the vanced composites. Toughness is such a prop- reinforcement, and the nature of the interphase. erty. In metals, wherein the dynamics of crack Each of these variables must be carefully con- propagation and failure are relatively well under- trolled to produce a structural material optimized stood, toughness can be defined relatively eas- for the conditions for which it is to be used. ily. I n an advanced composite, however, tough- ness is a complicated function of the matrix, fiber, The use of continuous-fiber reinforcement con- and interphase, as well as the reinforcement ge- fers a directional character, called an isotropy, to ometry. 5 Shear and compression properties of ad- the properties of PMCs. PMCs are strongest when vanced composites are also poorly defined. stressed parallel to the direction of the fibers (0°, axial, or longitudinal, direction) and weakest when Another result of the complexity of PMCs is that stressed perpendicular to the fibers (90°, trans- the mechanical properties are highly interdepen- verse direction). In practice, most structures are dent. For instance, cracking associated with shear subjected to complex loads, necessitating the use stresses may result in a loss of stiffness. Impact of fibers oriented in several directions (e.g., 0, damage can seriously reduce the compressive ±45, 90°). However, PMCs are most efficiently strength of PMCs. Compressive and shear prop- used in applications that can take advantage of erties can be seen to relate strongly to the tough- the inherent anisotropy of the materials, as shown ness of the matrix, and to the strength of the in- in figure 3-3. terfacial bond between matrix and fiber. When discontinuous fibers or particles are used for reinforcement, the properties tend to be more isotropic because these reinforcements tend to be randomly oriented, Such PMCs lack the out- standing strength of continuous-fiber PMCs, but they can be produced more cheaply, using the technologies developed for unreinforced plastics, such as extrusion, injection molding, and com- pression molding. Sheet molding compound (SMC) ‘Given that perfect composite toughness cannot be attained, in is such a material, widely used in the automo- some cases a material with lower toughness may be preferable to tive industry; see figure 3-3. one with higher toughness. A brittle composite with low impact resistance may shatter upon impact, while a slightly tougher com- The complexity of advanced composites can posite may suffer cracking. For some applications, even slight crack- ing may be unacceptable, and impossible to repair. If the compos- complicate a comparison of properties with con- ite shatters in the region of impact, but no cracking occurs in the ventional materials. Properties such as specific surrounding material, the damage may be easier to repair. Ch. 3—Polymer Matrix Composites . 79 DESIGN, PROCESSING, AND TESTING Design Manufacturing Advanced composites are designed materials. Given the many different fibers and matrices This is really the fact that underlies their useful- from which PMCs can be made, the subject of ness. Given the spectrum of matrix and reinforce- PMC manufacturing is an extremely broad one. ment materials available, properties can be op- However, more than any other single area, Iow- timized for a specific application. An advanced cost manufacturing technologies are required composite can be designed to have zero coeffi- before advanced composites can be used more cient of thermal expansion. It can be reinforced widely. The basic steps include: 1 ) impregnation with combinations of fiber materials (hybrid PMCs) of the fiber with the resin, 2) forming of the struc- and geometries to maximize performance and ture, 3) curing (thermoset matrices) or thermal minimize cost. The design opportunities of PMC processing (thermoplastic matrices), and 4) fin- materials are only beginning to be realized. ishing. The enormous design flexibility of advanced Depending on the process, these steps may composites is obtained at the cost of a large num- occur separately or continuously. For instance, ber of unfamiliar design variables. In fact, com- the starting material for many PMCs is a prepreg; posites are more accurately characterized as cus- i.e., a fiber tape or cloth that has been preimpreg- tomized structures, rather than materials. Although nated with resin and partially cured. In pultru- the engineering properties of the homogeneous sion, by contrast, impregnation, forming, and cur- resins and fibers can be determined, the prop- ing are done in one continuous process. Some erties of each composite depend on the compo- of the more important fabrication processes for sition, fiber geometry, and the nature of the in- PMCs are listed in table 3-1. terphase. However, the categories of mechanical In the aerospace sector, advanced composite and physical properties used to characterize PMCs structures are commonly fabricated by the slow are carried over from long engineering experi- and labor-intensive process of hand lay-up of ence with metals. A major need in advanced composites technol- ogy is a better capability for modeling structure- Table 3-1 .—Production Techniques for property relationships (discussed in more depth Polymer Composites in ch. 5). In spite of this lack, however, experi- ence to date has shown that designers and man- Technique Characteristics Examples ufacturers can produce reliable PMC structures. Sheet molding Fast, flexible, 1-2” SMC automotive body This is probably due to two factors. First, in the fiber panels Injection molding Fast, high volume Gears, fan blades face of uncertainty, designers tend to overdesign; very short fibers, that is, they are conservative in their use of ma- thermoplastics terial, to avoid any possibility of material failure. Resin transfer Fast, complex parts, Automotive structural molding good control of fiber panels Second, PMC structures are extensively tested orientation before use, ensuring that any potential problems Prepreg tape lay-up Slow, laborious, Aerospace structures show up during the tests. Thus, the PMC materi- reliable, expensive (speed improved by als themselves have been proven, in the sense automation) that structures can be fabricated that are relia- Pultrusion Continuous, constant l-beams, columns ble and meet all design criteria. However, both cross-section parts Filament winding Moderate speed, Aircraft fuselage, overdesign and empirical testing are costly and complex geometries, pipes, drive shafts drive up the prices of PMCs. Thus, a principal hollow parts benefit of enhanced modeling capability will be Thermal forming Reinforced thermoplastic All of above (future) matrices; fast, easy to help make advanced composites more cost- repair, joining competitive. SOURCE: Office of Technology Assessment, 1988. 80 ● Advanced Materials by Design over hand lay-up. One project underway in- house at an airframe manufacturer can lay up to 100 feet of 3- or 6-inch wide prepreg tape per minute, in complex shapes of variable thickness.8 At least one machine tool manufacturer is devel- oping a system of automated tape laying that takes into account the specified contour of the mold, and aligns the tape according to tape width and desired gap between strips, laying the tape along a precomputed path. Most of these processes have been explored for thermosetting advanced composites for air- craft applications such as ailerons, stabilizers, flaps, fins, and wing skins; in addition there has also been some work done in the area of auto- 8“Rockwell Team Demonstrates Automatic Construction of Large Composite Wings,” Aviation Week & Space Technology, June 15, 1987, p. 336. Photo credit: Hercules, Inc. Filament winding of a rocket motor case. prepreg tapes. Hand lay-up involves placement of sheets or tapes of prepreg on a tool (the con- toured surface that defines the shape of the fin- ished part). Labor costs often dominate the pro- duction costs of these PMC structures. In the case of a business aircraft fuselage, material costs have been estimated at about$13,000 per unit; labor costs, about $21,000 per unit; and capital costs, about $1,400 per unit.6 These labor cost estimates include 1,154 person-hours for hand lay-up of the stiffeners and honeycomb core of the fuselage; only 35 person-hours are required to produce the inner and outer advanced composite skins, which can be fabricated by the automated filament winding process. ’ New, more automated processes are now avail- able that offer dramatic increases in productivity GMaterials Modeling Associates, “Properties, Costs, and Appli- Photo credit: Hercules Inc. cations of Polymeric Composites, “ in conjunction with Massachu- setts Institute of Technology, a contractor report prepared for OTA, Graphite fiber reinforcement forms. Top: broadgoods; December 1985. right: prepreg tape; left (front): chopped fiber and 71 bid. carbon fiber rope; left (rear): fabric and fabric prepreg. Ch. 3—Polymer Matrix Composites ● 81 mated tape laying for continuous fiber-reinforced sizes to be detected are not as small, the area of thermoplastic sheets, laid in parallel strips and structure to be investigated is frequently much continuously fused as they are placed.9 larger, up to hundreds of square feet. Thus, NDE techniques are required that can rapidly scan large areas for flaws or damage. Even though Nondestructive Evaluation there are numerous techniques that may be use- In general, PMCs do not have as great a ten- ful in the laboratory for testing small specimens dency to brittle fracture as do ceramics. This for research purposes, relatively few are appro- means that the critical flaw size in large PMC priate to production or field-level inspection. structures may be of the order of centimeters, whereas in ceramics, it is some tens of microns. Several of the more important NDE techniques Advanced composite structures are increasingly that are relevant to production, end product, and used in life-critical structures such as aircraft field level inspection are listed in table 3-2. Ex- wings and fuselages. This places a special bur- cellent progress has been made in production den on nondestructive evaluation (NDE), both in level techniques such as ultrasonics, and manu- the factory and in the field. facturers are confident that large PMC surface areas can be inspected reliably and economically Although NDE is now used primarily for the de- for such flaws as bulk delamination. tection of defects in finished structures, in the fu- ture it could be used increasingly for monitoring The inspection and repair of PMC structures the status of PMCs at intermediate steps in the (e.g., aircraft components) at the depot and field production process. Progress in this field will re- levels will require a substantial training program quire development of sophisticated sensors and for inspectors unfamiliar with PMCs. All proce- feedback control systems. dures must be standardized and straightforward because, in general, PMC experts will not be Requirements for NDE of PMCs differ some- available. In the future, as inspection processes what from those for ceramics. Although the flaw become fully computerized, this could bean ex- cellent application for automated systems that can guide the operator through the process and 9Roger Seifrled, Cincinnati Miliacron, personal communication, June 1, 1987. alert him to any detected anomalies. Table 3-2.—NDE Techniques Appropriate for Production, Finished Product, Depot-, and Field-Level Inspections of Polymer Matrix Composite Structures Complex Development for NDE technique Flaw type Sensitivity shapes commercialization Production: Visual (remote) ...... Fiber orientation, good good none foreign material Ultrasonic ...... Porosity, viscosity good poor extensive during cure Dielectrometry ...... Degree of cure good good some End product: Visual ...... Surface good good none Ultrasonic ...... Bulk good poor some Radiographic ...... Bulk fair excellent none Acoustic emission ...... Bulk fair good extensive Depot level: Ultrasonic...... Bulk delamination good poor some Field level: Ultrasonic ...... Bulk delamination fair poor extensive SOURCE: Joseph A. Moyzis, et al., “Nondestructive Testing of Polymer Matrix Composites,”a contractor report prepared for OTA, December 1985. 82 ● Advanced Materials by Design HEALTH AND SAFETY There are a number of unique health and safety in the area in which they are used, but all elec- issues associated with the manufacture of PMC trical devices in the area should be sealed to materials. The health hazards associated with the make them explosion proof. Because most fac- manufacture of PMC materials stem from the fact tories using carbon fibers are generally involved that chemically active materials are used and with advanced composites and are more sophis- workers handling them may breathe harmful ticated than most reinforced plastics plants, they fumes or come into contact with irritating chem- are able to handle this hazard without undue dif- icals. The chemical of greatest concern is the sty- ficulty. rene monomer used in polyester resins. The prob- lem is most severe when the resin is sprayed, and Recycling and Disposal the monomer evaporates into the air. Inhalation of styrene monomer can cause headaches, diz- Most PMC materials in use today have ther- ziness, or sore throat. In fact, some people be- mosetting matrices; consequently, after they have come sensitized to the vapors and they can no been cured, they have no apparent scrap value. longer work in a reinforced plastics plant. Although attempts have been made to grind them up and use them as fillers, this has not proven The Occupational Health and Safety Adminis- to be economically practical. The reuse of un- tration (OSHA) has specified that styrene mono- cured PMCs offers little economic incentive; most mer concentrations in a plant should not exceed 10 scrap is simply discarded, By contrast, one of the 100 parts per million. In a plant in which spray potential advantages of PMCs with thermoplas- systems are used, extensive air-handling equip- tic matrices is that the scrap can be recycled, ment, spray booths, and air masks are required to maintain these standards. Where polyester Cured PMCs present no particular disposal resins are used for compression molding, resin problem; they are chemically inert and can be transfer molding, or other enclosed mold systems, used for landfill. Incineration is generally avoided the problem can be dealt with by use of simple because it can generate toxic smoke. exhaust systems. The principal problem associated with PMC dis- A new safety hazard was introduced with the posal arises with uncured PMCs. Wet lay-ups, advent of carbon fibers. They tend to float around prepregs, SMC, etc. are still chemically active and the plant in which they are used. Because they pose both health and safety problems. If used in are electrical conductors, they can get into un- landfill, the active chemicals can leach out and protected electrical devices and cause short cir- cause contamination of the soil or water. A more cuits. The fiber concentration in the air can be serious problem is that the catalyzed resins may controlled by a negative pressure exhaust system go on to cure and generate an exotherm that causes spontaneous combustion or self-ignition. The safe way to dispose of uncured PMC mate- IOWor/~ Ofcompos;tes, quarterly publication of the SPI Reinforced rial is to bake it until it is cured and then dispose Plastics/Composites Institute, winter 1986. of it. APPLICATIONS AND MARKETS PMCs area more mature technology than struc- coming the baseline structural material of the de- tural ceramics. With the experience gained in mil- fense/aerospace industry. itary applications such as fighter aircraft and rocket motor casings beginning in the 1970s, ad- Because of their high cost, diffusion of advanced vanced composites now have a good record of composites into the civilian economy is likely to performance and reliability. They are rapidly be- be a top-down process, progressing from rela- Ch. 3—Polymer Matrix Composites ● 83 tively high value-added applications such as air- cent being typical .14 This weight reduction can craft to automobiles and then to the relatively be used to increase range, payload, maneuvera- low-technology applications such as construction, bility and speed, or to reduce fuel consumption. which generally requires standardized shapes It has been estimated that a pound of weight such as tubes, bars, beams, etc. On the other saved on a commercial transport aircraft is worth hand, there is also a bottom-up process at work $100 to $300 over its service life, depending on in which savings in manufacturing costs permit the price of fuel, among other factors.15 This high unreinforced engineering plastics and short fiber- premium for weight saved is unique to this aero- reinforced PMCs to replace metals in applications space sector, and explains why it leads all others in which high strength and stiffness are not re- in advanced composite market growth rate. Ad- quired, such as use of SMC for automobile body ditional advantages of advanced composites are panels. their superior fatigue and corrosion resistance, and vibration-damping properties. Applications and markets for PMCs are dis- cussed according to end-user industry below. Military Aircraft Aerospace Advanced composites have become essential to the superior performance of a large number The aerospace industry is estimated to con- of fighter and attack aircraft (figure 3-4). Because sume about 50 percent of advanced composites the performance advantages of advanced com- production in the United States.11 Growth pro- posites in military aircraft more than compensate jections for aerospace usage of advanced com- for their high cost, this is likely to be the fastest posites have ranged from 8.5 percent per year12 growing market for advanced composites over 13 to 22 percent per year. Advanced Composites the next decade. Indications are that composites are used extensively today in small military air- may account for up to 40 percent of the struc- craft, military and commercial rotorcraft, and pro- lqCarl Zweben, “Polymer Matrix Composites, ” Frontiers in Ma- totype business aircraft. The next major aircraft teriak Technologies, M.A. Meyers and O.T. Inal (eds.) (The Nether- lands: Elsevier Science Publishers, 1985), ch. 12, p. 365. market opportunity for advanced composites is 15BOb Hammer, Boeing Commercial Aircraft Co., personal Com- in large military and commercial transport aircraft. munication, August 1986. The primary matrix materials used in aerospace applications are epoxies, and the most common Figure 3-4.—Composite Aircraft Structure (by percent) reinforcements are carbon/graphite, aramid (e.g., Du Pont’s Kevlar), and high-stiffness glass fibers. V-22 Rotor Craft However, high-temperature thermoplastics such as PEEK are considered by many to be the ma- trices of choice for future aerospace applications. implementation Adv Fighter & 40 Compared with metals, the principal advan- ~FighterA Attack A/C tages of advanced composites in aerospace ap- S-76 plications are their superior specific strength and 20 k stiffness, resulting in weight savings of 10 to 60 percent over metal designs, with 20 to 30 per- 1970 1980 1990 Year of first flight KEY O Business aircraft and rotorcraft I lstrategic Analysis, Inc., op. cit., March 1987. v Military rotorcraft ~lACCOr~irrg to ‘‘worldwide High Performance COrnpOSiteS, ” a A Fighter and attack aircraft ❑ market study conducted by Frost & Sullivan, New York, NY, as re- Large commercial and military aircraft O Bomber ported in World of Corrr~sites, a publication of the Society of Plas- tics Industries, winter 1986, p. 4. SOURCE: Richard N. Hadcock, Grumman Aircraft Systems Division, “Status and 1 IACCOrding to a market study by Charles H. Kline & CO., “Ad- Viability of Composite Materials in Structure of High Performance Air- craft,” a presentation to the National Research Council, Aeronautics vanced Polymer Composites, ” Fairfield, NJ, reported in Plastics Engi- and Space Engineering Board, Naval Postgraduate School, Monterey, neering, June 1985, p. 62. CA, Feb. 10, 1966. 84 “ Advanced Materials by Design Although overall growth of the business aircraft fleet through the early 1990s is expected to be only around 10 percent, two categories (turbo- prop and turbojets) are expected to grow sig- nificantly.20 These aircraft are also the best can- didates for composite fuselages. The estimated value (derived from cost and volume estimates) of composite fuselages, assuming all business air- craft manufacturers adopt this technology, is about $100 million per year.21 These fuselages could account for 1.2 million pounds of graph- ite/epoxy consumption annually. Large transport Photo credit: Hercules, Inc. or commercial aircraft fuselages will probably not be made from advanced composites until the A modern lightweight fighter incorporating 64 different components—more than 900 pounds of composite technology is demonstrated in business aircraft. structure per airplane. By the year 2000, PMCs could make up 65 per- cent of the structural weight of commercial trans- 22 tural weight of the Advanced Tactical Fighter port aircraft. Estimating a structural weight of (ATF), which is still in the design phase. One esti- 75,000 pounds per aircraft and production of 500 mate, which assumes only existing production aircraft per year, this application alone should ac- plus the ATF, projects a growth from about 0.3 count for 24 million pounds of advanced com- million pounds per year in 1985 to 2 million posites per year. Assuming a starting material pounds per year in 1995.16 value of $60 per pound, the market in the year 2000 is projected to be worth about $1.5 billion for the composite materials alone. A much more Commercial Aircraft conservative estimate, which assumes that no If aramid and glass fiber-reinforced composites new commercial aircraft will be built by 1995, are included, the volume of composites used in has placed the U.S. composite commercial air- commercial and business aircraft is about twice frame production at only 1 million to 2 million that used in military aircraft.17 In current com- pounds in that year.23 mercial transport aircraft, such as the Boeing 767, advanced composites make up about 3 percent Helicopters of the structural weight, and are used exclusively With the exception of the all-composite busi- in the secondary (not flight-critical) structure.18 ness aircraft prototypes, which are still awaiting However, two companies, Beechcraft and Avtek, certification, advanced composites have been are anticipating Federal Aviation Administration used more extensively in helicopters than in air- (FAA) certification of “all-composite aircraft pro- craft. Military applications have led the way, and totypes for business use in 1988 and 1990, respec- 19 the advantages of advanced composites are much tively. the same as in aircraft: weight reduction, parts consolidation, and resistance to fatigue and cor- rosion, lbRichard N. Hadcock, Grumman Aircraft Systems Division, “Status and Viability of Composite Materials in Structures of High Over the past 15 years, advanced composites Performance Aircraft, ” a presentation to the National Research Council, Aeronautics and Space Engineering Board, Naval Postgrad- have become the baseline materials for rotors, uate School, Monterey, CA, Feb. 10, 1986. blades, and tail assemblies. Sikorsky’s S-76 com- I Zlbid. 18Darrel R. Tenney, NASA Langley Research Center, “Advanced Composite Materials: Applications and Technology Needs,” pres- zOMaterials Modeling Associates, op. cit., footnote 6, 1985. entation to the Metal Properties Council, Inc., Miami, FL, Dec. 5, z’ Ibid. 1 1985. zzTenney, op. cit., footnote 8. lgAccordi ng t. information supplied by Beechcraft and Avtek. zJHadcock, CIp. Cit., footnote 16. . . Ch. 3—Polymer Matrix Composites c 85 mercial model, which is about 25 percent ad- vanced composite by weight (figure 3-4), was cer- tified in the late 1970s. Future military helicopters, such as the Army’s proposed LHX (with major airframe design teams at Bell/McDonnell Douglas and Boeing/Sikorsky), or the Navy’s tilt-rotor V- 22 Osprey (designed by Bell/Boeing) have speci- fications that require designers to consider ad- vanced composites. In these helicopters, com- posites are likely to comprise up to 80 percent of the structural weight (figure 3-4). Materials such as graphite/epoxy are likely to be used in the airframe, bulkheads, tail booms, and vertical fins, while glass/epoxy PMCs of lesser stiffness could be used in the rotor systems. As with aircraft, there could be a long-term trend away from epoxy resins and toward thermoplastic resins. Automotive Industry The automotive industry is widely viewed as Photo credit: Ford Motor Co. being the industry in which the greatest volume Compression molded composite rear floor pan of advanced composite materials could be used prototype for the Ford Escort. Ten steel components in the future. (See ch. 7 for a case study examin- were consolidated into a single molding, with ing the use of PMCs for automobile body struc- 15 percent weight savings. tures.) Because the industry is mature and highly The next major opportunity for PMCs in au- competitive, the principal motivation for intro- 25 tomobiles is in structural components. Two ducing PMCs is cost savings. structural components currently in service are the In contrast to the aircraft industry, there is no advanced composite drive shaft and leaf spring. clear-cut premium associated with a pound of Some 3,000 drive shafts, manufactured by fila- weight saved. Nevertheless, the automotive in- ment winding of graphite and E-glass fibers in a dustry continues to be interested in saving weight polyester resin, were used annually in the Ford as it pursues the conflicting goals of larger au- Econoline van.26 Meanwhile, glass FRP springs in tomobiles and higher fuel efficiency. Automakers the Corvette and several other models are in pro- are looking to the vehicle skin/frame systems to duction at the rate of approximately 600,000 per provide the next big leap in weight reduction. year. Leaf springs are regarded as a very promis- Other potential technical advantages of PMCs, ing application of PMCs, and they are expected such as corrosion resistance, appear to be sec- to show strong growth, especially in light trucks. ondary to the cost issue. prototype primary body structures have been con- structed with weight savings of 20 percent or By far the greatest volume of PMC material in more. use is sheet molding compound (WK), used in nonstructural parts such as exterior panels. The Engineering groups within the Big Three U.S. most visible automotive use of SMC in recent automobile producers are considering advanced years has been in the Pontiac Fiero, which has an all-PMC exterior.24 25P. Beardmore, “Composite Structures for Automobiles,” Comp- osite Structures, vol. 5, 1986, pp. 163-176. 26Although composite drive shafts are technically successful, Ford took them out of production in 1987 in favor of a new aluminum 24 The FierO wi II be cancel led at the end of 1988. design. 86 ● Advanced Materials by Design composite unibody vehicle designs for the late In robotic applications, increasing both the 1990s. 27 The automakers are exploring PMC speed and the endpoint accuracy of the robot are frames for a variety of reasons. PMC vehicles desired improvements. Stiffness is the key me- would enable designers to reduce the number chanical property in that the endpoint accuracy of parts required in assembly; some manufac- is limited by bending deflections in the beam- turers are looking into a one-piece advanced shaped robot members. With metal designs, stiff- composite body. By reducing the number of ness is obtained at the cost of higher mass, which parts, better consistency of parts can be achieved limits the robot’s response time. Consequently, at considerably reduced assembly costs. the ratio of the weight of the manipulator arm to that of the payload is rarely lower than 10:1.30 Advanced composites also offer substantial im- Because of their superior stiffness per unit weight, provements in specific mechanical properties, PMCs are a promising solution to this problem. with the possibility of reducing weight while in- At present, only one U.S. company has marketed creasing strength and stiffness. Finally, because 31 a robot incorporating PMCs, although there are they do not rust, PMCs offer greatly improved several Japanese models on the market and a corrosion resistance over steel or galvanized steel. number of other countries are funding research. Analysts have estimated that PMC automobiles could last 20 or more years, compared to the cur- Although the benefits of using PMCs in recip- rent average vehicle lifetime of 10 years .28 rocating equipment are clear, initial attempts to penetrate this market have been disappointing. The major technical barrier to use of PMCs in The market is a highly fragmented one, and the automotive industry is the lack of manufac- equipment manufacturers, who tend to be ori- turing technologies capable matching the high ented toward metals, have shown a reluctance production rates of metal-stamping technology to consider the use of a higher cost material (par- (see ch. 7). The fastest current technologies can ticularly when its use requires new processes and process material at the rate of tens of pounds per tooling) even when performance advantages are minute, but true economy will require rates of demonstrated. No attempt has been made to a hundred pounds per minute or more.29 Thus, quantitatively estimate future markets. PMC there is a gap of roughly an order of magnitude penetration is likely to be slow but steady. between current and economical rates. Naval Applications Reciprocating Equipment The light weight and corrosion resistance of PMC materials have considerable potential for PMCs makes them attractive for a number of use in many different kinds of high-speed indus- naval applications. Advanced composites are cur- trial machinery. Current applications include such rently in production in molded propeller assemblies components as centrifuge rotors, weaving ma- for the Mark 46 torpedo, at a cost savings of 65 chinery, hand-held tools, and robot arms. All of to 70 percent over the previous aluminum de- these applications take advantage of the low in- sign .32 The Navy is also evaluating PMCs for hatch ertial mass, but they also benefit to varying doors, bulkheads, and propeller shafts. PMC degrees from the tailorable an isotropic stiffness, components in the ship superstructure have the superior strength, low thermal expansion, and dual advantage of lowering the center of mass fatigue-life and vibration-damping characteristics (and therefore increasing the stability) and pro- of PMCs. 30B, s, Thompson and c.K. Sung, “The Design of Robots and in- telligent Manipulators Using Modern Composite Materials, ” Mech- anism and Machine Theory 20:471 -82, 1985. 31 G raco Robotics of Lavonia, Ml, manufactures a spray painting zTMaterials Modeling Associates, op. cit., footnote 6, 1985. robot with a hollow graphite/epoxy arm. However, this is being z81 bid. phased out in favor of a new aluminum design. Zgcharles Sega[, Omnia, in OTA workshop on ‘‘Future Applica- JZRonald L. pegg and Herbert Reyes, ‘‘Progress i n Naval Com- tions of Advanced Composites, ” Dec. 10, 1985. posites,” Advanced Materials and Processes, March 1987, p. 35. — Ch. 3—Polymer Matrix Composites w 87 Photo credit: The CUMAGNA Corp. Computer trace of fiber paths in a three-dimensional braided l-beam. This process yields a composite l-beam which is strong in all directions, but which weighs much less than steel. vialing better protection against shrapnel frag- Construction ments in combat. PMCs have also been in use for years as sonar domes on submarines, and ra- A potentially high-volume market for PMCs lies domes for surface ships. in construction applications, especially in con- struction of buildings, bridges, and housing. Future applications for PMCs on surface ships Additional applications include lampposts, smoke- include antenna masts and stacks (due to reduced stacks, and highway culverts. Construction equip- weight and radar cross section), and valves, pipes, ment, including cranes, booms, and outdoor and ducts (due to lower weight and corrosion re- drive systems, could also benefit from use of sistance). PMCs could also be used for an ad- PMCs. Because of the many inexpensive alterna- vanced technology submarine hull, providing tive building materials currently being used, the weight savings and thus speed advantages over cost of PMC materials will be the key to their use metal hulls currently in use. in this sector. 88 “ Advanced Materials by Design The chief advantage of using PMCs in construc- tion would be reduced overall systems costs for erecting the structure, including consolidation of fabrication operations, reduced transportation and construction costs due to lighter weight struc- tures, and reduced maintenance and lifetime costs due to improved corrosion resistance. 33 Bridges are likely to be the first large-scale con- struction application for PMCs in the United States. Because the largest load that must be sup- ported by the bridge is its own dead weight, use of lightweight advanced composites would allow the bridge to accommodate increased traffic or heavier trucks. Decking materials are likely to be relatively inexpensive vinylester or epoxy resins reinforced with continuous glass fibers. Cables would probably be reinforced with graphite or aramid fibers, because of the high stiffness and low creep requirements. The opportunities for use of PMCs in bridges are considerable: most highway bridges in the United States are over 35 years old, and most rail- road bridges are over 70 years old.34 Replacing or refurbishing even a small fraction of these with PMC materials would involve a substantial vol- ume of fiber and resin. However, significant tech- nical, economic, and institutional barriers exist to the implementation of this technology, such that construction opportunities should be viewed as long term. Nevertheless, the U.S. Department 37 of Transportation is currently evaluating PMCs for than assembled on site. In the future, factory use in bridge decking and stay cables.35 Fiberglass manufacture of housing promises to reduce hous- tendons are also being used in place of steel in ing costs while still maintaining options for dis- prestressed concrete bridge structures.36 Other tinctive designs. PMC manufacturing techniques countries that have active programs in this area such as pultrusion and transfer molding could be include China, Great Britain, West Germany, ls- used to fabricate integral wall structures contain- rael, and Switzerland. ing structural members and panels constructed in a single step. Components such as i-beams, The manufactured housing industry is an espe- angles, and channels can also be economically cially intriguing potential opportunity for PMC produced by these techniques. In spite of the op- materials. In 1984, almost half of all new hous- portunities, however, Japan and several countries ing units were partially manufactured; that is, in Europe are far ahead of the United States in large components were built in factories, rather housing construction technologies. 33HOWard smallowi~, “ReShaping the Future of Plastic Buildings, ” One important research need affecting the use Civil Engineering, May 1985, pp. 38-41. of PMCs in construction applications has to do JdJohn Scalzi, National Science Foundation, personal commun i- cation, August 1986. JSAccording to information provided by Craig A. Ballinger, Fed- eral Highway Administration, August 1986. JThomas E. Nutt-Powell, “The House That Machines Built, ” JbEngineering News Record t Aug. 29, 1985, p. 11. Technology Review, November 1985, p. 31. Ch. 3—Polymer Matrix Composites ● 89 with adhesion and joining. The joining of PMC fibers pressed with inexpensive resins or lami- materials to other materials for the purpose of nated structures involving FRP skin panels glued load transfer, or to themselves for the purpose to a foam or honeycomb core. of manufacturing components, requires advances in technology beyond present levels. This is a par- Medical Devices ticular obstacle when joining may be done by un- skilled labor. A second need for PMCs use in the PMC materials are currently being developed construction industry involves the availability of for medical prostheses and implants. The impact standardized shapes of standard PMC materials of PMCs on orthopedic devices is expected to be to be purchased much the way metal shapes are especially significant. Although medical devices currently sold for construction use. are not likely to provide a large volume market for PMCs, their social and economic value are An additional technical barrier is need for de- likely to be high. velopment of design techniques for integrated, multifunctional structures. Window frames made The total estimated world market for orthope- by joining together several pieces of wood can dic devices such as hips, knees, bone plates, and be replaced by molded plastic and PMC struc- intramedullary nails is currently about 6 million tures having many fewer pieces, lower assembly units with a total value of just over $500 miIlion.39 costs, and better service performance. The flexi- Estimates of the U.S. market for all biocompati- bility of the design and manufacture of PMC ma- ble materials by the year 2000 range up to $3 bil- terials could also be used to integrate a window lion per year.40 PMCs could capture a substan- frame into a larger wall section, again reducing tial portion of that, sharing the market with the number of parts and the cost of manufacture. ceramics and metals. This has already been done for certain experi- Metallic implant devices, such as the total hip mental bathroom structures in which lavatories, unit that has been used since the early 1960s, suf- shower rooms, and other structural components fer a variety of disadvantages: difficulty in fixa- have been integrated in a single molding.38 tion, allergic reactions to various metal ions, poor The principal barriers to the adoption of new matching of elastic stiffness, and mechanical (fa- materials technologies in the construction indus- tigue) failure. try in the United States are not so much techno- PMC materials have the potential to overcome logical as institutional and economic. Like the many of these difficulties. Not only can the prob- highway construction industry, the housing con- lem of metal ion release be eliminated, but PMC struction industry is highly fragmented. This materials can be fabricated with stiffness that is makes the rate of research and development in- tailored to the stiffness of the bone to which they vestment and adoption of new technology very are attached, so that the bone continues to bear low. The performance of housing materials is reg- load, and does not resorb (degenerate) due to ulated by thousands of different State and local absence of mechanical loading. This is a persist- building and fire safety codes, all written with ent problem with metal implants. conventional materials in mind. Further, engi- neers and contractors lack familiarity with the it is also possible to create implants from bio- PMC materials and processes. Finally, PMCs must degradable PMC systems that would provide ini- compete with a variety of low-cost housing ma- tial stability to a fracture but would gradually re- terials in current use. As a result, PMCs used in sorb over time as the natural tissue repairs itself. manufactured housing are not likely to be ad- In addition, PMCs can be designed to serve as vanced; rather, they are likely to consist of wood ~gl bid. ~~Larry L. Hench and ju ne Wi Ison, “Biocompatlbility of Sillcates 3~Ken neth L. Reifsnicfer, Materials Response Croup, Virglnla Poly- for Medical Use, ” Sr’/icon Blochemlstry, CIBA Foundation Sympo- technic Institute, “Engineering Research Needs of Polymer Com- sium No. 121 (Chichester, England: John Wiley & Sons, 1986), pp. posites, ” a contractor report prepared for OTA, December 1985. 231-246. 90 . Advanced Materials by Design a scaffold for the invasive growth of bone tissue To overcome the remaining technical barriers, as an alternative to cement fixation. This leads a cooperative effort of interdisciplinary teams is to a stronger and more durable joint. required. At a minimum, a team must include ex- pertise in design, engineering, manufacturing, Research in PMC orthopedic devices is cur- and orthopedic surgery. Significant strides in this rently being carried out on a relatively small scale field are being made in Japan, Great Britain, in the laboratories of orthopedic device manu- France, West Germany, Italy, Canada, and Aus- facturers. Further research is required to improve tralia, as well as in the United States.41 in situ strength and service life, stress analysis, and fabrication and quality control technologies. 41 Reif~nider, op. Cit., fC3C3tnC3te 38. FUTURE TRENDS IN POLYMER MATRIX COMPOSITES Novel Reinforcement Types sistance, and adhesive properties.43 Some of the more promising directions are discussed below. Rigid Rod Molecules PMCs can be reinforced with individual, rigid Oriented Molecular Structures rod-like molecules or with fibers generated from At present the anisotropic properties of most these molecules. One example is poly (phenyl- PMCs are determined by the directions of fiber benzobisthiazole), or PBT. Experimental fibers orientation. In the future, it may be possible to made from this material have specific strength orient the individual polymer molecules during and stiffness on a par with the most advanced fi- or after polymerization to produce a self- ber reinforcement, exceeding the properties of reinforced structure. The oriented polymers commercially available metals, including titanium, could serve the same reinforcing function as by more than a factor of 10.42 One particularly fibers do in today’s PMCs. In effect, today’s or- promising possibility is to dissolve the molecu- ganic fibers (e.g., Du Pent’s Kevlar or Allied’s lar rods in a flexible polymer and thus create a Spectra 900), which consist of oriented polymers PMC reinforced by individual molecules. Such and which have among the highest specific stiff- a homogeneous composition would mitigate the ness and strength of all fibers, provide a glimpse problem of matching the thermal expansion co- of the properties of tomorrow’s matrices. efficient between the reinforcement and the ma- trix, and it would virtually eliminate the trouble- Recently developed examples of oriented poly- some interface between them. The future of this mer structures are the liquid crystal polymers technology will depend on solving the problems (LCPs). They consist of rigid aromatic chains mod- of effectively dissolving the rods in the matrix and ified by thermoplastic polyesters (e.g., polyeth- of orienting them once dissolved. yleneterephthalate, or PET), or polyaramids. They have a self-reinforcing fibrous character that im- Novel Matrices parts strength and stiffness comparable to those of reinforced thermoplastic molding compounds, Because the matrix largely determines the envi- such as 30 percent glass-reinforced nylons.44 The ronmental durability and toughness, the greatest fiber orientations of current LCPs are hard to improvements in the performance of future PMCs control (current applications include microwave will come from new matrices, rather than new cookware and ovenware that require high-tem- fibers. Perhaps the most significant opportunities perature resistance but not high strength) and this lie in the area of molecular design; chemists will represents a challenge for the future. be able to design polymer molecules to have the desired flexibility, strength, high-temperature re- ojcharles P. West, Resin Research Laboratories, Inc., Personal communication, August 1986. qqReginald B. Stoops, qZThaddeus Helminiak, “Hi-Tech Polymers From Ordered “Ultimate Properties of Polymer Matrix Molecules, ” Chemical Week, Apr. 11, 1984. Materials, ” contractor report prepared for OTA, December 1985. Ch. 3—Polymer Matrix Composites 91 High-Temperature Matrices The maximum continuous service temperature of organic polymers in an oxidizing atmosphere is probably around 700° F,45 although brief ex- posures to higher temperatures can be tolerated. Currently, the most refractory matrices are poly- amides, which can be used at a maximum tem- perature of 600° F (316° C), although slow deg- radation occurs. 46 If stable, high-temperature matrices could be developed, they would find application in a variety of engine components and advanced aircraft structures. Thermotropic Thermoses These hybrid matrices are designed to exploit the processing advantages of thermoplastics and the dimensional stability and corrosion resistance of thermoses. The molecules are long, discrete chains that have the latent capacity to form cross- Iinks. Processing is identical to thermoplastics in that the discrete polymers are formed at high tem- peratures to the desired shape. Then, however, instead of cooling to produce a solid, the struc- Photo credit: National Aeronaut/es and Space Administration ture is given an extra kick, with additional heat or ultraviolet light, which initiates crosslinking be- Reference configuration for the NASA manned space station. Composites could be used in the tubular struts tween the polymer chains. Thus, the finished which make up the frame. structure has the dimensional stability character- istic of a thermoset.47 at speeds exceeding Mach 7, the lower surfaces Space Applications and leading edges would experience tempera- tures of 2,000 to 3,000° F (1 ,093 to 1,649° C). so Space Transportation Systems If advanced composites were available that could Over 10,000 pounds of advanced composites retain high strength and stiffness up to 800° F are used on the space shuttle. da Advanced com- (427° C), they could be used extensively for the posites are also being considered in designs for cooler skin structure and most of the substructure. a proposed National Aerospace Plane (NASP), al- though such an aircraft probably will not be avail- Space Station able until after the year 2000. The primary limi- Graphite/epoxy advanced composites and alu- tation on the use of advanced composites in this minum are both being considered for the tubu- 49 application would be high temperature. Flying lar struts in the space station reference design. The goal of reducing launch weight favors the use dspaul McMahan, Celanese Research Corp., in an OTA workshop, of advanced composites; however, their lower “Future Opportunities for the Use of Composite Materials,” Dec. thermal conductivity (compared with aluminum) 10, 1985. ~Aerospace America, May 1986, p. 22. could create problems in service. The most seri- qzjohn Riggs, Celanese Research Corp., in an OTA workshop, ous environmental problem faced by advanced “Future Opportunities for the Use of Composite Materials, ” Dec. composites is temperature swings between — 250° 10, 1985. 48Tenney, Op. Ck., footnote 18’ dgHadcock, op. cit., footnote 16. 50Ibid. 75-7920- 88 - 3 92 w Advanced Materials by Design F (– 1210 C) and +200° F (+93° C) caused by being evaluated for commercial production of lu- 54 periodic exposure to the Sun. This thermal cy- bricants, engineering nylons, and PMCS. For cling produces radial cracks in graphite/epoxy some materials, such as natural rubber, the tubes that can reduce the torsional stiffness by United States is totally dependent on foreign as much as 30 percent after only 500 cycles.51 sources. In the Critical Agricultural Materials Act To reduce the effects of thermal cycling, ad- of 1984 (Public Law 98-284), Congress mandated vanced composite tubes would be coated with that the Department of Agriculture establish an a reflecting, thermally conducting layer to equal- Office of Critical Materials to evaluate the poten- ize the temperature throughout the tube. The tial of industrial crops to replace key imported layer would also protect the PMC from atomic materials. Several demonstration projects of 2,000 oxygen (a major cause of material degradation acres or more were started in 1987. in low-Earth orbit), and solar ultraviolet radiation. With the possible exception of wood, it is un- likely that biologically produced materials will Military compete seriously with PMCs in the structural ap- Composites of all types, including ceramic, plications discussed in this report. Although nat- polymer, and metal matrix composites, are ideal ural polymers such as cellulose, collagen, and silk materials for use in space-based military systems, can have remarkably high strength, their low stiff- such as those envisioned for the Strategic Defense ness is likely to limit their use in many structures. Initiative. 52 Properties such as low density, high Nevertheless, their unique chemical and physi- specific stiffness, low coefficient of thermal ex- cal properties make them appropriate for certain pansion, and high temperature resistance are all specialty applications. For instance, collagen is necessary for structures that must maneuver rap- a biologically compatible material that is used to idly in space, maintain high dimensional stabil- generate artificial skin.55 ity, and withstand hostile attack. A program de- Biotechnology may offer a novel approach to voted to the development of new materials and the synthesis of biological polymers in the future. structures has been established within the Stra- 53 Genetically engineered bacteria and cells have tegic Defense Initiative Office. 56 been used to produce proteins related to silk. In the future, production rates could be acceler- Bioproduction ated by extracting the protein synthetic machin- Living cells can synthesize polymeric molecules ery from the cells and driving the process with an external energy source, such as a laser or elec- with long chains and complex chemistries that 57 cannot be economically reproduced in the lab- tric current. The flexibility inherent in such a oratory. For instance, crops and forests are an im- scheme would be enormous; by simply altering portant source of structural materials and chem- the genetic instructions, new polymers could be ical feedstocks. Several plants such as cram be and produced. rapeseed, and certain hardwood trees, are now 1 51 Tenney, op. cit., footnote 8. 54According to information supplied by the USDA’S Office of Crit- JZJerome Persh, “Materials and Structures, Science and Technol- ical Materials. ogy Requirements for the DOD Strategic Defense Initiative, ” Arrrer- 55 J. Burke, et al., “The Successful Use of Physiologically Accept- ican Ceramic Society Bulletin 64(4):555-559, 1985. able Artificial Skin in the Treatment of Extensive Burn In jury,” An- SJThe effo~ includes: lightweight structures; thermal and electri- na/s of Surgery, vol. 194, 1982, pp. 413-28. cal materials; optical materials and processes; tribological materi- 5bDennls Lan~, Syntro Corp., personal cornrnunlcdtlon, August als; and materials durability. In 1988, budgets for these materials 1986. programs were about $26 million, and are projected to reach $54 5zTerrence Barrett, National Aeronautics and space Adrn i n istra- million in 1989. tion, personal communication, August 1986. Ch. 3—Polymer Matrix Composites . 93 RESEARCH AND DEVELOPMENT PRIORITIES Federal R&D spending for PMCs in fiscal years complete and uniform cure, minimize thermal 1985 to 1987 is shown in table 3-3; roughly 70 stresses, control resin content, and ensure ac- to 80 percent in each year was spent by the De- curate fiber placement. This requires models that partment of Defense. The large drop in Federal can predict the influences of key process varia- expenditures from 1985 to 1986 does not reflect bles and techniques for monitoring these varia- a sharp cut in PMC R&D; rather, it can be at- bles so that pressure and temperature can be ad- tributed to the completion of large research pro- justed accordingly. Such models would also grams in 1985 and the transitioning of the tech- provide useful guidelines for tool design. At nology (particuIarly for carbon fiber PMCs) out present, though, modeling is in a very early stage of the basic and applied research categories of of development. the DoD budget (6. 1, 6.2, and 6.3A). Defense ap- The existence of low-cost fabrication processes plications continue to drive the development of will be critical to the use of new PMC systems, PMCs, which are used in an estimated $80 bil- such as low-cost, high-performance thermoplas- lion of weapons systems.58 tics reinforced with continuous fibers. For in- Reliable PMC structures can now be designed stance, methods for fabricating shapes with dou- that satisfy all of the engineering requirements of ble curvature are needed. Another important a given application. However, scientific under- problem is the impregnation and wetting of fi- standing of PMCs has lagged behind engineer- ber bundles by these relatively viscous plastics. ing practice. To design more efficiently and cost- The effects of processing on microstructure re- effectively, and to develop improved materials, quire further study. Similar knowledge is needed it will be necessary to understand and model sev- of the influence of residual thermal stresses, a par- eral important aspects of PMCs. Based on the op- ticular concern for resins processed at high tem- portunities outlined above, some research and peratures. Finally, as for thermoses, process development priorities for PMCs are suggested models are required. below, Impact Damage Very Important The resistance to impact damage of a PMC Processing Science structure has a critical effect on its reliability in service. Impact damage barely visible to the The primary goal of processing science is to be naked eye can cause a reduction in strength of able to control the fabrication process to ensure as much as 40 percent. 59 Impact resistance is S~Ken neth Foster, Assistant for Materials policy, Department of especially important in primary aircraft structures Defense, personal communication, August 1986. and other safety-critical components. Tougher thermoplastic matrix materials promise to im- prove the impact resistance of aircraft structures now made with epoxy matrices. Table 3-3.—Budgets for Polymer Matrix Composite R&D in Fiscal Years 1985 to 1987 (millions of dollars) The complexity of the impact damage process Agency FY 1985 FY 1986 FY 1987 makes modeling very difficult. However, it would Department of Defense (6.1, 6.2, 6,3A) $55.9 $29.2 $33.8 be very desirable to be able to relate the extent National Aeronautics and Space of damage to the properties of the matrix, fiber, Administration 23 8.7 5.0 and interphase, along with factors such as rein- National Science Foundation 1-2 1-2 3.0 National Bureau of standards 04 04 0.5 Department of Transportation . 0.4 0.2 Sqcarl zwehen, General Electrlc Co., “Assessment of the Science Total $80-81 $40-41 $42.5 Base for Composite Materials, ” a contractor report prepared for SOURCE OTA survey of agency representatives OTA, December 1985. 94 ● Advanced Materials by Design forcement form. This would facilitate the devel- geneous materials. Even for the simplest PMCs, opment of more reliable materials and structures. unidirectional laminates, there is an inadequate In addition, an understanding of impact damage understanding of the relationships between ax- mechanisms would aid in developing protocols ial and transverse loading (parallel and perpen- for repair of PMC structures, a field that still re- dicular to the fiber direction) and failure. In more lies largely on empirical methods. complex PMCs, containing several fiber orien- tations and various flaw populations, efforts to Delamination model strength have been largely empirical. It will be important in the future to have analytical There is a strong body of opinion that delami- models for the various failure modes of unidirec- nation is the most critical form of damage in PMC tional PMCs and laminates that relate strength structures (particularly those produced from pre- properties to basic constituent properties. pregs). As noted above, impact damage barely visible on the surface can cause dramatic reduc- Fatigue tions in strength through local delamination. Voids and pores between layers can also pose Fatigue of PMCs is an important design con- serious problems to the integrity of the PMC. sideration. Fatigue resistance is a major advan- Delamination may prove to be a problem of in- tage that PMCs enjoy over metals; however, the creasing severity in the future because of the traditional models for analyzing fatigue in metals trend toward higher working strains that tend to do not apply to PMCs. The risks associated with accentuate this mode of failure. fatigue failure are likely to increase because of the trend toward use of fibers with higher failure Analyses to date have concentrated on crack strains, plus the desire to use higher design growth and failure associated with compressive allowable for existing materials. loading, These need to be verified and refined. In addition, the effects of combined loading, resin Ideally, it would be desirable to be able to pre- fracture toughness, reinforcement form, and envi- dict PMC fatigue behavior based on constituent ronment need to be investigated. properties. A more realistic near-term objective is to understand fatigue mechanisms, and how Interphase they are related to the properties of fibers, ma- trix, interphase, loading, and environment of the The interphase has a critical influence on the PMC. Important topics that have not received PMC in that it determines how the reinforcement adequate attention are the fatigue properties of properties are translated into the properties of the the reinforcements and matrix resins, and com- composite structure. The characteristics of this pression fatigue of unidirectional PMCs. In view little-studied region merit thorough investigation. of the increasing interest in thermoplastics, fatigue The objective would be to develop a body of of these materials also deserves study. knowledge that would guide the development of fiber surface treatments, matrices, and fiber coat- Fracture ings that will optimize mechanical properties and provide resistance to environmental degradation. One of the most important modes of failure in metals is crack propagation. Arising at regions of high stress, such as holes, defects, or other dis- Important continuities, cracks tend to grow under cyclic ten- sile load. When cracks reach a critical size, they Strength propagate in an unstable manner, causing fail- The excellent strength properties of PMCs are ure of the part in which they are located. This, one of the major reasons for their use. However, in turn, may result in failure of the entire struc- as with many properties of PMCs, their heter- ture. In contrast, failure of PMCs often results ogeneity makes strength characteristics very com- from gradual weakening caused by the accumu- plex. This heterogeneity gives rise to failure modes lation of dispersed damages, rather than by that frequently have no counterpart in homo- propagation of a single crack. Ch. 3—Polymer Matrix Composites ● 95 In view of the significant differences in failure significant loss of strength compared to a uni- modes between metals and PMCs, use of linear directional laminate. However, multidirectional elastic fracture mechanics to describe fracture in reinforcement appears to confer increased frac- these complex materials is controversial. It is ture toughness on the PMC. open to question whether there are unique values Use of several types of fibers to reinforce PMCs of fracture toughness or critical stress intensity will be driven by the desire to obtain properties that describe the fracture characteristics of PMCs. that cannot be achieved with a single fiber, and To develop reliable design methods and im- to reduce cost. For instance, glass fibers, which proved materials in the future, it will be neces- are cheap but have a relatively low tensiIe stiff- sary to develop a body of fracture analysis that ness, can be mixed with more costly, high-stiff- is capable of accounting for the more complex ness graphite fibers to achieve a PMC that is both failure mechanisms. stiff and relatively cheap. Environmental Effects With both new reinforcement forms and hy- brid reinforcement, there is a great need for ana- The environments to which PMCs are sub- lytical methods to identify the configurations re- jected can have a significant effect on their prop- quired to produce desired properties. Without erties. Environments known to be especially such tools, it will be necessary to rely on human damaging are those of high temperature and intuition and time-consuming, costly empirical moisture under load, ultraviolet radiation, and approaches. some corrosive chemicals. The key need in the environmental area is to develop a thorough un- Desirable derstanding of degradation mechanisms for fibers, resins, and interphases in the environments of Creep Fracture greatest concern. This knowledge will lead to Materials subjected to sustained loading fail at more reliable use of existing materials and pro- stress levels lower than their static strengths. This vide the information required to develop new, phenomenon is called creep fracture. Topics that more degradation-resistant ones. require study include tensile and compressive loading of both unidirectional PMCs and lami- Reinforcement Forms and Hybrid PMCs nates, and the influence of temperature and envi- There are two main reasons for the interest in ronment. Because the time-dependent degrada- new reinforcement forms: improved through-the- tion of the matrix and interphase properties are thickness properties, and lower cost. A pervasive typically greater than those of the fiber reinforce- weakness of PMC laminates of all kinds is that ments, particular attention shouId be paid to the out-of-plane strength and stiffness, being de- transverse matrix cracking and delamination. pendent primarily on the matrix, are much in- ferior to the in-plane properties. This is because Viscoelastic and Creep Properties in conventional laminates there is no fiber rein- The occurrence of significant deformation re- forcement in the thickness direction. sulting from sustained loading can have an ad- New reinforcement forms under development verse effect on structural performance i n some include triaxial fabrics, muItilayer fabrics, two- applications, such as reciprocating equipment, dimensional braids, three-dimensional braids, bridges, and buildings. Consequently, creep be- and various kinds of knits. I n addition, laminates havior is an important material characteristic. This have been reinforced in the thickness direction subject could benefit from development of a data- by stitching. From an analytical standpoint, the base for creep properties of various fibers, ma- major drawback to fabrics, braids, and knits is trices, and PMCs, especially for compressive load- that they introduce fiber curvature that can cause ing, which has received relatively little attention. Chapter 4 Metal Matrix Composites Page ...... ***********n”*’” ...... 99 Current Applications and Market Opportunities ...... 99 Longer Term Applications...... ● ...... ● .. 99 Research and Development Priorities ...... 99 Introduction ● ● ● ● ● ● ● ● ● . ● . ● ● ● ● ● ● . ● ● ● ● ● ● ● ● ● . ● ● ● .-...... 100 Properties of Metal Matrix Composites ● ● ● ● . ● ● . . ● . . . ● ● ...... 100 ● ● ...... 100 . Discontinuous Reinforcement ...... ’. . . . Continuous Reinforcement ● ...... 102 MMC Properties Compared to Other Structural Materials ...... 102 Design,● Processing, and Testing ...... ,....., .*...... 106 . Design . . . ● . ● ● ● ...... ● ● * ● ● * ● ● ● . . .**...... *. ... ●☛✎✎✎✎✎ . . 107 Processing. ● . . * . . . ● ● ...... ● ● . ● ● ● . . . . ● ...... ,.. ● . . . 107 Costs. ● . . . ● ● .. ● , ● ...... ● ● ● ● ● ● ...... 110 . Testing . ● ● . . . . . ● ● . . . . ● ...... ● ● ● ● ● ● ...... 111 Health and Safety ...... ● ...... 111 Applications...... ● ...... 112 Current Applications ...... ,.,...... 112 Future Applications ...... *.*...... 113 Markets . ● ... ● ... ● ...... 115 Research and Development Priories ...... 115 Very Important...... ● ☛✎✎☛✎✎ ✎ ✎ ✎ ✎ ...... ● 115. . Important ...... ✎ ✎ ✎ ✎ ✎ ✎ ✎ ✎ ✎ ✎ ✎ ...... 116 Desirable ...... ✎ ✎ ✎ ✎ ✎ ✎ ✎ ✎ ✎ ✎ ✎ ...... 117 Tables Table No. 4-1. Costs of a Representative Sample of MMC Reinforcements...... 101 4-2. Structural Properties of Representative MMCs, Compared to Other Materials ...... 103 4-3. Strength and Stiffness of Some Fiber-Reinforced MMCs...... 104 4-4. Properties of 6061 Aluminum Reinforced With Silicon Carbide Particulate .105 4-5. MMC Manufacturing Methods .. . * ...... 108 4-6. Selected MMC Processing Techniques and Their Characteristics ...... 109 i Chapter 4 Metal Matrix Composites FINDINGS Metal matrix composites (MMCs) usually con- 300,000 such pistons are produced and sold in sist of a low-density metal, such as aluminum or Japan annually. This development is very impor- magnesium, reinforced with particulate or fibers tant because it demonstrates that MMCs are at of a ceramic material, such as silicon carbide or least not prohibitively expensive for a very cost graphite. Compared with unreinforced metals, sensitive application. Other commercial applica- MMCs offer higher specific strength and stiffness, tions include cutting tools and circuit-breaker higher operating temperature, and greater wear contacts. resistance, as well as the opportunity to tailor these properties for a particular application. Longer Term Applications However, MMCs also have some disadvantages compared with metals. Chief among these are the Metal matrix composites with high specific stiff- higher cost of fabrication for high-performance ness and strength could be used in applications MMCs, and lower ductility and toughness. Pres- in which saving weight is an important factor. In- ently, MMCs tend to cluster around two extreme cluded in this category are robots, high-speed ma- types. One consists of very high performance chinery, and high-speed rotating shafts for ships composites reinforced with expensive continu- or land vehicles. Good wear resistance, along ous fibers and requiring expensive processing with high specific strength, also favors MMC use methods. The other consists of relatively low-cost in automotive engine and brake parts. Tailorable and low-performance composites reinforced with coefficient of thermal expansion and thermal con- relatively inexpensive particulate or fibers. The ductivity make them good candidates for lasers, cost of the first type is too high for any but mili- precision machinery, and electronic packaging. tary or space applications, whereas the cost/ben- However, the current level of development ef- efit advantages of the second type over unrein- fort appears to be inadequate to bring about com- forced metal alloys remain in doubt. mercialization of any of these in the next 5 years, with the possible exception of diesel engine Current Applications and Market pistons. Opportunities Based on information now in the public do- main, the following military applications for Current markets for MMCs are primarily in mil- MMCs appear attractive: high-temperature fighter itary and aerospace applications. Experimental aircraft engines and structures; high-temperature MMC components have been developed for use missile structures; and spacecraft structures. Test- in aircraft, satellites, jet engines, missiles, and the ing of a National Aerospace Plane (NASP) pro- National Aeronautics and Space Administration totype is scheduled for the early to mid 1990s, (NASA) space shuttle. The first production appli- which might be too early to include MMCs. How- cation of a particulate-reinforced MMC in the ever, it may be possible to incorporate MMCs in United States is a set of covers for a missile guid- the structure or engines of the production vehicle. ance system. The most important commercial application to Research and Development Priorities date is the MMC diesel engine piston made by Toyota. This composite piston offers better wear MMCs are just beginning to be used in produc- resistance and high-temperature strength than the tion applications. In order to make present ma- cast iron piston it replaced. It is estimated that terials more commercially attractive, and to de- 99 100 . Advanced Materials by Design velop better materials, the following research and cost fiber reinforcements is a major need. development priorities should receive attention: Continued development work on existing materials is important to lower costs as well. ● Cheaper Processes: To develop low-cost, ● Coatings: Research in the area of reinforce- highly reliable manufacturing processes, re- ment/matrix interface coatings is necessary. search should concentrate on optimizing These coatings can prevent deleterious chem- and evaluating processes such as plasma ical reactions between matrix and reinforce- spraying, powder metallurgy processes, ment which weaken the composite, particu- modified casting techniques, liquid metal in- larly at high temperature, and optimize the filtration and diffusion bonding. interracial fiber/matrix bond. ● Cheaper Materials: Development of Iower INTRODUCTION Metal matrix composites (MMCs) generally in dramatic improvements in MMC properties, consist of lightweight metal alloys of aluminum, but costs remain high. Continuously and discon- magnesium, or titanium, reinforced with ceramic tinuously reinforced MMCs have very different particulate, whiskers, or fibers.1 The reinforce- applications, and will be treated separately ment is very important because it determines the throughout this chapter. mechanical properties, cost, and performance of Tailorability is a key advantage of all types of a given composite. composites, but is particularly so in the case of Composites reinforced with particulate (dis- MMCs. MMCs can be designed to fulfill require- continuous types of reinforcement) can have ments that no other materials, including other ad- costs comparable to unreinforced metals, with vanced materials, can achieve. There are a num- significantly better hardness, and somewhat bet- ber of niche applications in aerospace structures ter stiffness and strength. Continuous reinforce- and electronics that capitalize on this advantage. ment (long fiber or wire reinforcement) can result PROPERTIES OF METAL MATRIX COMPOSITES There are considerable differences in published Property data given in this chapter are therefore property data for MMCs. This is partly due to the given as ranges rather than as single values. fact that there are no industry standards for Some MMC properties cannot be measured as MMCs, as there are for metals. Reinforcements they would be for monolithic metals. For in- and composites are typically made by proprie- stance, toughness is an important but hard-to- tary processes, and, as a consequence, the prop- define material property. Standard fracture me- erties of materials having the same nominal com- chanics tests and analytical methods for metals position can be radically different. The issue is are based on the assumption of self-similar crack further clouded by the fact that many reinforce- extension; i.e., a crack will simply lengthen with- ments and MMCs are still in the developmental out changing shape. Composites, however, are stage, and are continually being refined. Numer- non homogeneous materials with complex inter- ous test methods are used throughout the indus- nal damage patterns. As a result, the applicabil- try, and it is widely recognized that this is a ma- ity of conventional fracture mechanics to MMCs jor source of differences in reported properties.2 is controversial, especially for fiber-reinforced ma- 1 As used i n this chapter, the terms 1‘al u m inu m, ‘‘magnesium, ” terials. and “titanium” denote alloys of these materials used as matrix metals. ~Carl Zweben, “Metal Matrix Composites, ” contractor report for OTA, January 1987. — Ch. 4—Metal Matrix Composites ● 101 Table 4-1 .—Costs of a Representative Sample of MMC Reinforcements Reinforcement Price ($/pound) Alumina-silica fiber...... 1 Silicon carbide particulate ...... 3 a Silicon carbide whisker ...... 95 Alumina fiber (FP) ...... 200 Boron fiber...... $262 Graphite fiber (P-100) ...... 950a Higher performance reinforcements (e.g., graphite and boron fibers) have sig- nificantly higher costs as well. aJoseph Dolowy, personal communication, DWA Composite Specialties, Inc., JuIy 1987. SOURCE: Carl Zweben, “Metal Matrix Composites, ” contractor report for OTA, January 1987. In terms of tailorability, a very important advan- tage in MMC applications, particulate reinforce- ment offers various desirable properties. Boron carbide and silicon carbide, for instance, are widely used, inexpensive, commercial abrasives that can offer good wear resistance as well as high specific stiffness. Titanium carbide offers a high melting point and chemical inertness which are desirable properties for processing and stability in use. Tungsten carbide has high strength and hardness at high temperature. In composites, a general rule is that mechani- cal properties such as strength and stiffness tend to increase as reinforcement length increases.4 Particulate can be considered to be the limit of short fibers. Particulate-reinforced composites are Photo credit: DWA Composite Specialties, Inc. isotropic, having the same mechanical proper- Micrograph (75x magnification) of 20 percent volume ties in all directions. fraction silicon carbide particulate-reinforced 2124 aluminum. In principle, whiskers should confer superior properties because of their higher aspect ratio Discontinuous Reinforcement (length divided by diameter). However, whiskers There are two types of discontinuous reinforce- are ‘brittle and tend to break up into shorter ment for MMCs: particulate and whiskers. The lengths during processing. This reduces their rein- most common types of particulate are alumina, forcement efficiency, and makes the much higher boron carbide, silicon carbide, titanium carbide, cost of whisker reinforcement hard to justify. De- and tungsten carbide. The most common type velopment of improved processing techniques - of whisker is silicon carbide, but whiskers of alu- could produce whisker-reinforced MMCs with mina and silicon nitride have also been produced. mechanical properties superior to those made Whiskers generally cost more than particulate, from particuiates. as seen in table 4-1. For instance, silicon carbide Another disadvantage of using whisker rein- whiskers cost $95 per pound, whereas silicon car- forcement is that whiskers tend to become ori- bide particulate costs $3 per pound. Cost pro- ented by some processes, such as rolling and ex- jections show that although this difference will trusion, producing composites with different decrease as production volumes increase, par- properties in different directions (anisotropy).5 3 ticulate will always have a cost advantage. 41 bid. 5See the discussion on an isotropy in ch. 3 on Polymer Matrix Com- 3Ibid posites. .- — 102 ● Advanced Materials by Design Anisotropy can be a desirable property, but it is when the composite is exposed to high temper- a disadvantage if it cannot be controlled precisely atures in processing or service. For example, bo- in the manufacture of the material. It is also more ron fiber can be coated with boron carbide and difficult to pack whiskers than particulate, and silicon carbide reaction barriers to prevent diffu- thus it is possible to obtain higher reinforce- sion and chemical reactions with the matrix that ment:matrix ratios (fiber volume fraction, v/o) decrease the strength of the composite. Alumina with particulate. Higher reinforcement percent- fibers can be given a surface coating of silica to ages lead to better mechanical properties such improve tensile strength. as higher strength. Coatings can also be used to tailor the bond strength between fiber and matrix. If adhesion Continuous Reinforcement between fiber and matrix is too good, cracks in In fiber reinforcement, by far the most com- the matrix propagate right through the fibers, and mon kind of continuous reinforcement, many the composite is brittle. By reducing the bond types of fibers are used; most of them are car- strength, coatings can enhance crack deflection bon or ceramic. Carbon types are referred to as at the interface, and lead to higher energy ab- graphite and are based on pitch or polyacryloni- sorption during fracture through fiber pullout trile (PAN) precursor. Ceramic types include alu- mechanisms. Sometimes a coating is needed to mina, silica, boron, alumina-silica, alumina-boria- promote wetting between the matrix and the fi- silica, zirconia, magnesia, mullite, boron nitride, ber, and thereby achieve a good bond. Graph- titanium diboride, silicon carbide, and boron car- ite can be coated with titanium diboride in or- bide. All of these fibers are brittle, flaw-sensitive der to promote wetting. materials. As such, they exhibit the phenomenon processing techniques, as well as coatings, can of size effect (see ch. 2); i.e., the strength of these be used to control deleterious fiber/matrix inter- fibers decreases as the length increases. actions. The application of pressure can be used Fiber/matrix interface coatings offer another to force intimate contact between fiber and ma- dimension of tailorability to MMCs. Coatings are trix and thus promote wetting; squeeze casting very important to the behavior of MMCs to pre- is one process that does this. vent undesirable reactions, improve the strength A less common type of continuous reinforce- of the fibers, and tailor the bond strength between ment is wire reinforcement. Wires are made of fiber and matrix. A reaction barrier is needed for such metals as titanium, tungsten, molybdenum, some fiber/matrix combinations, particularly beryllium, and stainless steel. Such wires offer some tailorability for certain niche applications; for example, tungsten wire offers good high-tem- perature creep resistance, which is an advantage . in fighter aircraft jet engines and other aerospace applications. MMC Properties Compared to Other Structural Materials Table 4-2 compares the most important mate- rial properties of MMCs with those of other struc- tural materials discussed in this assessment. Strength and Stiffness Photo credit: DWA Composite Specialties, Inc. The stiffnesses and strengths of particulate-rein- Cross-section of continuous graphite fiber-reinforced forced aluminum MMCs are significantly better aluminum composite: 52 percent volume fraction fiber, uniaxially reinforced. 300x magnification than those of the aluminum matrix. For exam- . Ch. 4—Metal Matrix Composites ● 103 pie, at a volume fraction of 40 percent silicon car- ing PMCs in structures subject to high transverse bide particulate reinforcement, the strength is stresses. about 65 percent greater than that of the 6061 6 High values of specific strength and specific aluminum matrix, and the stiffness is doubled. stiffness (strength and stiffness divided by den- Particulate-reinforced MMCs, which are isotropic sity) are desirable for high-strength, low-weight materials, have lower strength than the axial applications such as aircraft structures. Typically, strength (parallel to the direction of continuous particulate MMCs have somewhat better specific fiber reinforcement) of advanced polymer matrix strength and specific stiffness than the matrix composites (PMCs), see table 4-2. However, they metal, and fiber-reinforced MMCs have much have much better strength than the transverse better specific strength and specific stiffness than strength (perpendicular to the direction of con- the matrix metal. tinuous fiber reinforcement) of PMCs. The stiff- ness of particulate MMCs can be considered to Unfortunately, MMCs have a higher density be about the same as that of PMCs. than PMCs, making specific strength and specific stiffness lower than those for PMCs in the axial Unlike particulate-reinforced MMCs and mono- direction. Transverse specific strength and spe- lithic metals in general, fiber-reinforced MMCs cific stiffness of MMCs are still better than those can be highly an isotropic, having different strengths of PMCs. and stiffnesses in different directions. The high- est values of strength and stiffness are achieved High-Temperature Properties along the direction of fiber reinforcement. In this direction, strength and stiffness are much higher MMCs offer improved elevated-temperature than in the unreinforced metal, as shown in ta- strength and modulus over both PMCs and me- ble 4-2. In fact, the stiffness in the axial direction tals. Reinforcements make it possible to extend can be as high as six times that of the matrix ma- the useful temperature range of low density me- terial in a graphite fiber/aluminum matrix com- tals such as aluminum, which have limited high- posite: see table 4-3. However, in the transverse temperature capability (see table 4-2). MMCs typi- directions, strength values show no improvement cally have higher strength and stiffness than PMCs over the matrix metal. Transverse strengths and at 200 to 300° C (342 to 5720 F), although de- stiffnesses of continuous fiber-reinforced MMCs velopment of resins with higher temperature ca- compared to PMCs are very good, thereby giv- pabilities may be eroding this advantage. No ing MMCs an important advantage over the lead- other structural material, however, can compete with ceramics at very high temperature. bCarl Zweben, “Metal ,Matrlx Composites, ” contractor report fot Fiber-reinforced MMCs experience matrix/rein- OTA, January 1987. forcement interface reactions at high tempera- Table 4.2.—Structural Properties of Representative MMCs, Compared to Other Materials Matrix(l)* Particulate(2)* Fiber(3)* Property metala MMCa MMCa PMCb Ceramic b Strength (M Pa) (axial) ...... -290 290-480 620-1,240 820-1,680 140-3,900 Stiffness (G Pa) (axial)...... -70 80-140 130-450 61-224 97-400 Specific strength (axial)...... -100 100-170 250-390 630-670 51-670 Specific gravity ...... 2.5-2.8 -2.8 2.5-3.2 1.3-2.5 2.7-5.8 Transverse strength (MPa)...... -290 290-480 30-170 11-56 140-3,900 Transverse stiffness (GPa) ...... Same as axial Same as axial 34-173 3-12 Same as axial Maximum use temperature (“C) ...... 180 300 300 260 1,200-1,600 Plane strain fracture toughness (MPa-m½) ...... 18-35 12-35 — — 3-9 PMC IS used to denote a range of materials including graphite/epoxy, graphite/polylmlde, boron/polyimide, and S-glass/epoxy Ceramic is used to denote a range of materials including zirconia, silicon carbide, and silicon nitride “NOTE: (1) 6061 aluminum (2) 6061 aluminum reinforced with 0-400/0 volume fractions of SiC particulate (3) 6061 aluminum reinforced with 50°/0 volume fractions of fibers of graphite, boron. silicon carbide, or alumina SOURCES a Carl Zweben, “Metal Matrix Composites, ” b contractor report for OTA, January 1987 "Guide to Selecting Engineered Materials. ” Advanced Materials and Processes, vol. 2, No 1, June 1987 104 ● Advanced Materials by Design Table 4-3.—Strength and Stiffness of Some Fiber. Reinforced MMCs (Fiber V/O = 50%) Tensile Tensile strength strength Stiffness Stiffness Material (axial) (transverse) (axial) (transverse) Matrix material MPa MPa GPa GPa Aluminum 6061-T6 ...., 290 290 70 70 Titanium Ti-6AI-4V 1170 1170 114 114 Composite Graphite a/aluminum . . . 690 30 450 34 Boron/aluminum. . . . . 1240 140 205 140 Silicon carbideb/ aluminum . . . . . 1240 100 205 140 Silicon carbidec/ aluminum ...... 1040 70 130 99 Alumina d/aluminum . . . . . 620 170 205 140 Silicon carbide8/ titanium ...... 1720 340 260 173 Graphitea/copper ...... 512 31 464 49 Properly Improvements of MMCs over unreinforced metals can be significant For example, the axial stiffness of graphite fiber-reinforced aluminum is roughly 6 times greater than that of the unreinforced aluminum The axial tensile strength of silicon carbide fiber-reinforced aluminum IS about 4 times greater than that of the unreinforced aluminum aP-120 b AVCO monofilament c"Nicalon" d Fibe r "FP" ‘AVCO monofilament automobiles demonstrated an 85 percent improve- SOURCES: For all composites except graophit/copper: Carl Zweben, “Metal Matrix Composites, ” ment in wear resistance over the cast iron pis- contractor report for OTA, January 1987. For graphite/copper only: C Kaufmann, Ameri- 9 can Cyanamid, personal communication, Oct. 19, 1987. ton with nickel insert used previously. Fracture and Toughness tures. In addition, the transverse high-tempera- ture strength of fiber-reinforced MMCs is only as There is a wide variation in fracture toughness good as that of the matrix metal, since mechani- among MMCs, although it is generally lower than cal properties in the transverse direction are dom- that of the monolithic metal. Fracture toughness inated by the matrix and the fiber/matrix inter- can vary between 65 and 100 percent of the frac- face. For example, at 320 C (608° F), the axial ture toughness of the monolithic metal alloy.10 tensile strength of boron fiber-reinforced alumi- Lower toughness is a trade-off for higher strength num is about 1.1 gigapascals (GPa) compared to and stiffness. Particulate-reinforced MMCs have only 0.07 GPa for monolithic 6061 aluminum, a lower ultimate tensile strain than the unrein- whereas the transverse strength is 0.08 GPa, forced metals (see table 4-4) which may be im- about the same as that for the monolithic 6061.7 portant in some applications. This brittleness can complicate the design process and make joining Wear Resistance more difficult as well. Comparison to PMCs is dif- ficult, because the toughness of PMCs is very Wear resistance of MMCs is excellent compared temperature-dependent. to that of monolithic metals and PMCs, owing to the presence of the hard ceramic reinforcements. Thermal Properties For instance, in one test, the abrasive wear of 2024 aluminum under a 1 kilogram load was The introduction of silicon carbide particulate shown to be 6 times greater than the wear of the into aluminum results in materials having lower same alloy containing 20 percent volume frac- coefficients of thermal expansion, a desirable tion of silicon carbide whiskers.8 An alumina-silica property for some types of applications. By choos- fiber-reinforced aluminum piston used in Toyota ing an appropriate composition, the coefficient 7 Ibid. 9 lbid. 8 lbid. 10 lbid. Ch. 4—Metal Matrix Composites . 105 Table 4-4.—Properties of 6061 Aluminum Reinforced water damage than PMCs which can absorb With Silicon Carbide Particulate moisture, thereby reducing their high-tempera- ture performance. Second, some MMCs, such as Tensile Stiffness strength Tensile reinforced titanium, can stand high-temperature Reinforcement (G Pa) (M Pa) strain corrosive environments, unlike PMCs. 0% 10 290 16.O% 10 83 7.0 Nevertheless, some MMCs are subject to envi- 15 86 3&l 6.5 ronmental degradation not found in PMCs. For 20 90 430 6.0 instance, graphite fibers undergo a galvanic re- 25 103 — 3.5 30 117 470 2.0 action with aluminum. This can be a problem 35 124 — 1.0 when the graphite/aluminum interface is exposed 40 140 480 0.6 to air or moisture. In addition, PMCs are resis- Note the sharp rise in stiffness in the 400/0 composite (140 GPa) compared to the unreinforced aluminum (10 GPa). Ultimate tensile strength nearly doubles tant to attack by many chemicals (e.g., acids) that and tensile strain decreases nearly a full order of magnitude. corrode aluminum, steel, and magnesium. SOURCE: Carl Zweben, “Metal Matrix Composites,” contractor report for OTA, January 1987. cost of thermal expansion can be near zero in some A major disadvantage of MMCs compared to MMCs. MMCs also tend to be good heat conduc- most other structural materials is that they are tors. Using high thermal conductivity graphite generally more expensive. Both constituent ma- fibers, aluminum-matrix or copper-matrix MMCs terial costs and processing costs are higher. Costs can have very high thermal conductivity, com- of higher performance reinforcements (mostly pared with other types of composites. fibers) are high, and lower cost reinforcements (mostly particulate) may not yield dramatic im- Environmental Behavior provements in performance. Cost/benefit ratios In terms of environmental stability, MMCs have of most MMCs dictate that they be used only in two advantages over PMCs. First, they suffer less high-performance applications. However, both MICROWAVE CIRCUIT PACKAGING KOVAR METAL MATRIX COMPOSITE WEIGHT = 42 g WEIGHT = 15 g THERMAL 9.6 BTU THERMAL 74 BTU = = CONDUCTIVITY HR-FT-°F CONDUCTIVITY HR-FT-°F Photo credit: General Electric Co. Silicon carbide particle-reinforced aluminum microwave package 106 . Advanced Materials by Design the material and production costs may drop as more experience is gained in MMC production. Tailorability of Properties In some applications, MMCs offer unique com- binations of properties that cannot be found in other materials. Electronics packaging for aircraft requires a hard-to-achieve combination of low coefficient of thermal expansion, high thermal conductivity, and low density. Certain MMCs can meet these requirements, replacing beryllium, which is scarce and presents toxicity problems. Several other examples can be cited to illus- trate the unique advantages of MMCs in specialty applications. A large heat transfer coefficient is desirable for space-based radiators; this property is offered by graphite fiber-reinforced copper, alu- minum, and titanium (although this latter fiber/ matrix combination unfortunately has some in- Photo credit: Toyota Motor Corp. terface reaction problems). The higher transverse Aluminum diesel engine piston with local fiber strengths of MMCs compared to PMCs have led reinforcement in ring groove area to several MMC space applications, such as the space shuttle orbiter struts, made of boron fiber- reinforced aluminum. Use of local reinforcement to improve wear re- sistance makes possible the elimination of nickel One of the most important applications of and cast iron inserts. This reduces piston weight MMCs is the Toyota truck diesel engine piston, and increases thermal conductivity, improving produced at a rate of about 300,000 pistons per 11 engine performance and reducing vibration. Year. This consists of aluminum selectively rein- forced in the critical region of the top ring groove This approach minimizes cost and thereby makes with a ring-shaped ceramic fiber preform. (A pre- MMCs more competitive with cast iron. This de- form is an assemblage of reinforcements in the sign not only offers better wear resistance and shape of the final product that can be infiltrated better high-temperature strength but also elimi- with the matrix to form a composite.) nates one type of part failure associated with the design it replaced. It is considered by some to Two types of fibers are used: alumina and be a development of historic proportions because alumina-silica. Both are relatively low-cost ma- it demonstrates that MMCs can be reliably mass terials originally developed for furnace insulation. produced. It also shows that at least one type of aluminum matrix MMC can perform reliably in 11 Ibid. — a very severe environment. DESIGN, PROCESSING, AND TESTING In ceramics and polymer matrix composites billets or sheets and later machined to a final manufacturing, the material is formed to its final shape. Viable, inexpensive near-net-shape tech- shape as the microstructure of the material is niques for forming MMCs have not been success- formed. MMCs can be produced in this way, or, fully developed as yet, and there is still a debate as is traditionally done with metals, formed into about on the advantages of producing standard Ch. 4—Metal Matrix Composites . 107 MMC production processes can be divided into primary and secondary processing methods, though these categories are not as distinct as is the case with monolithic metals. Primary proc- esses (those processes used first to form the ma- terial) can be broken down into combining and consolidation operations. Secondary processes can be either shaping or joining operations. Ta- ble 4-5 shows the manufacturing methods dis- cussed here and notes which types of operations are included in each method. As with ceramics, net-shape methods are very important manufacturing processes. The machin- Photo credit: AVCO Corp. ing of MMCs is very difficult and costly in that Centrifugal casting of silicon carbide-reinforced MMCs are very abrasive, and diamond tools are aluminum. needed. In addition, it is desirable to reduce the amount of scrap left from the machining proc- ess because the materials themselves are very ex- shapes to be machined by the purchaser to final pensive. form, compared to the custom production of near-net-shape parts. Forming of net-shape MMC Continuous Reinforcement12 parts necessitates close integration of design and manufacture, where production of standard MMC The following discussion covers the primary structural shapes does not. and secondary processes involved in the manu- facture of MMCs with continuous reinforcement. Design Primary Processes.– Basic methods of combin- ing and consolidating MMCs include liquid metal The variability of metal matrix composite prop- infiltration, modified casting processes, and depo- erties is a handicap to designing with these ma- sition methods such as plasma spraying. Hot terials. There are currently no design aids such pressing consolidates and shapes MMCs. Diffu- as property databases, performance standards, sion bonding consolidates, shapes and joins and standard test methods. In addition, most MMCs. See table 4-6 for selected MMC process- designers are much more familiar with monolithic ing methods and their characteristics. metals. The lack of experience with MMCs in- creases the design and manufacturing costs asso- There is considerably more disagreement on ciated with the development of a new product. what is the most promising method for process- As with ceramic structures, brittleness is a new ing fiber-reinforced MMCs than there is for proc- and difficult concept to most designers. MMCs essing of particulate-reinforced MMCs. The Toyota are brittle materials, and new methods of design diesel engine piston has been heralded as an ex- will become important in the development of ample of the promise of modified casting tech- MMC applications. niques for keeping costs down. Critics charge that these types of casting techniques have not proven Processing adequate for manufacturing MMCs with desira- ble mechanical properties. (The Toyota piston Because MMC technology is hardly beyond the stage of R&D at present, costs for all methods of producing MMCs are still high. Manufacturing methods must ensure good bonding between ma- 12 As examples in the following discussion of processing, two com- mon types of particulate- and fiber-reinforced composites will be trix and reinforcement, and must not result in un- referred to as needed: silicon carbide particulate-reinforced alu- desirable matrix/fiber interracial reactions. minum, and boron fiber-reinforced alum inure. 108 ● Advanced Materials by Design Table 4-5.—MMC Manufacturing Methods Combines Consolidates Shapes Joins Primary methods: Casting ...... x x x Squeeze casting, compocasting, gravity casting, low-pressure casting Diffusion bonding ...... x x x Liquid infiltration ...... x x Gravity, inert gas pressure, vacuum infiltration Deposition ...... X x Chemical coating, plasma spraying, chemical vapor deposition, physical vapor deposition, electrochemical plating Powder processing ...... X x x Hot pressing, ball mill mixing, vacuum pressing, extrusion,— rolling Secondary methods: Shaping ...... x x Forging, extruding, rolling, bending, shearing, spinning, machining Machining ...... x Turning, boring, drilling, milling, sawing, grinding, routing, electrical discharge machining chemical milling, electrochemical milling Forming...... x x x Press brake, superplastic, creep forming Bonding...... x Adhesive, diffusion Fastening ...... x Soldering, brazing, welding ...... x SOURCE: Carl Zweben, “Metal Matrix Composites, ” contractor report for OTA, January 1987. uses fiber reinforcement mostly for wear resis- expensive than for monolithic structural metals. tance and less for more universally important As a rule, diamond tools are required because properties such as strength.) Some industry MMC carbide and other tools wear out too quickly. De- advocates suggest that processes such as diffu- spite this limitation, all of the basic mechanical sion bonding and plasma spraying are more prom- methods, such as drilling, sawing, milling, and ising for achieving high performance, and that turning have been proven to be effective with lower costs will come only with more produc- MMCs. Electrical discharge machining also has tion experience with these processes. been shown to be effective. secondary Processes.–Machining processes Mechanical fastening methods, such as rivet- for MMCs reinforced with ceramic materials, which ing and bolting have been found to work for are hard and abrasive, generally are much more continuously-reinforced MMCs. The same is true Ch. 4—Metal Matrix Composites ● 109 Table 4-6.—Selected MMC Processing Techniques and Their Characteristics Techniques Characteristics For fiber-reinforced MMCs: Liquid metal infiltration near-net-shape parts (low pressure) economical high porosity oxidation of matrix and fiber not reliable as yet Liquid metal infiltration (intert gas less porosity and oxidation than low pressure pressure, vacuum) techniques Low pressure casting near-net-shape parts low cost expensive preforms required three-dimensional preforms are difficult to make Squeeze casting good fiber wetting lower porosity expensive molds needed large capacity presses needed Plasma spraying potential for lower processing costs Diffusion bonding lower temperatures than hot pressing reduces fiber/matrix interactions not capable of net-shape parts except simple shapes slow, expensive fiber damage can occur Hot Pressing heats matrix above melt temperature, which can degrade reinforcement For particulate-reinforced MMCs: Powder metallurgy high volume fractions of particulate are possible (better properties) powders are expensive not for near-net-shape parts Liquid metal infiltration net-shape parts can use ingots rather than powders lower volume fraction of particulate (means lower mechanical properties) Squeeze casting may offer cost advantage; however molds and presses may be expensive SOURCE Carl Zweben, “Metal Matrix Composites, ” contractor report for OTA, January 1987 for adhesive bonding. Boron fiber-reinforced alu- forced MMCs are powder processing techniques. minum pieces can be metallurgically joined by There has not been much success at producing soldering, brazing, resistance welding and diffu- near-net-shape structures as yet. 13 (See discussion sion bonding. in chapter 2 on the desirabiIity of near-net-shape processing.) Other processes for discontinuously- Discontinuous Reinforcement reinforced MMCs are Iiquid metal infiltration and casting techniques (see table 4-6). The following discussion covers the primary and secondary processes involved in the manufac- At this time, there is no one MMC manufac- ture of MMCs with discontinuous reinforcement. turing method that holds great promise for reduc- Primary Processes.–The most common meth- ods for producing particulate- and whisker-rein- 110 . Advanced Materials by Design Photo credit: AVCO Specialty Materials Photo credit: AVCO Specialty Materials Centrifugal casting around braided tube of SiC Silicon carbide fiber-reinforced aluminum shaped by fibers and yarn. electrical discharge machining. A wide variety of joining methods can be used including mechanical fastening techniques, met- allurgical methods employed with monolithic metals, and adhesive bonding as used for PMCs. costs MMC costs are currently very high, and for them to come down, there must be some stand- ardization and a reliable compilation of materi- als properties (in a form such as a design data- base). This can be achieved only through greater production experience with MMC materials. Photo credit: AVCO Specialty Materials Some experts argue that entirely new materials Diffusion bonded SiC fiber-reinforced titanium: and processes must be found that are cheaper cross section of a hollow turbine blade. than the present ones. Opponents of this view hold that development of new processes and ma- ing costs, although there seems to be some agree- terials will delay a decrease in costs of existing ment that for particulate-reinforced MMCs, liquid materials, because it will take much longer to gain metal infiltration and powder metallurgy techniques the production experience necessary. are likely candidates for future development. Most present users buy preformed shapes, such Secondary Processes.–One of the major ad- as billets, plates, bars and tubes, and then ma- vantages of particulate- and whisker-reinforced chine these shapes to specification. MMCs are MMCs is that most of the conventional metal- not currently sold in standard sizes; users can or- working processes can be used with minor mod- der any size, manufactured to order. This lack ifications (see table 4-5), Methods demonstrated of standardization keeps prices for shapes high. include forging, extruding, rolling, bending, Some users produce their own MMCs for use in- shearing, and machining. Although they are ex- house. For example, Lockheed Georgia produces pensive, all conventional machining methods silicon carbide fiber-reinforced aluminum matrix have been found to work for these materials, in- composites for designing, manufacturing and test- cluding turning, milling, and grinding. ing fighter aircraft fins. Ch. 4—Metal Matrix Composites . 111 The cost of an MMC part depends on many composites are complex, heterogeneous mate- factors including shape, type of matrix and rein- rials that are susceptible to more kinds of flaws, forcement, reinforcement volume fraction, rein- including delamination, fiber misalignment, and forcement orientation, primary and secondary fiber fracture. fabrication methods, tooling costs, and number of parts in the production run. At present, there Failure in monolithic metals occurs primarily is little information available on production costs. by crack propagation. The analytical tool called The only items produced in any quantity are the linear elastic fracture mechanics (LEFM) is used Toyota engine pistons. Costs for this application to predict the stress levels at which cracks in are proprietary information, but the costs of these metals will propagate unstably, causing failure. MMCs are at least not prohibitive in a very cost- Failure modes in composites, especially those sensitive product. reinforced with fibers or whiskers, are far more complex, and there are no verified analytical Costs are very volume sensitive; high costs keep methods to predict failure stress levels associated volumes low, and low volumes mean high costs. with observed defects. As a consequence, em- Of course, some materials are inherently expen- pirical methods have to be used to evaluate how sive and will never be cheap enough for wide- critical a given flaw is in an MMC. spread commercial use, regardless of volume. Two basic methods have been established as With the exception of alumina-silica discontinu- reliable flaw-detection techniques for MMCs: ous reinforcement fibers, reinforcement prices radiography and ultrasonic C-scan. Radiography, are orders of magnitude higher than those of me- useful only for thin panels, detects fiber misalign- tals used in mass production items such as au- ment and fractures. C-scan identifies delamina- tomobiles. Unfortunately, the stiffness of alumina- tion and voids. There are no existing nondestruc- silica fibers is not substantially greater than that tive evaluation (N DE) methods for reinforcement of aluminum. The room-temperature strength of degradation in MMCs. aluminum reinforced with these fibers also shows little or no improvement over monolithic alumi- The costs of NDE methods for MMCs should num, although wear resistance and elevated- be no greater than for monolithic metals. How- temperature strength are enhanced. The signifi- ever, the reliability of manufacturing processes cance of this is that the fibers that provide major for these materials has not been established and improvements in material properties are quite ex- MMCs cannot be reliably or repeatably produced pensive, while use of low-cost alumina-silica as yet. Because fabrication processes are not de- fibers provides only modest gains in strength and pendable at present, it is generally necessary to stiffness. use NDE for MMCs in cases where testing would Testing not be employed at all, or as extensively, for monolithic metals, This additional cost factor Unlike monolithic metals, in which the main should decrease as experience and confidence types of flaws are cracks, porosity, and inclusions, are gained with MMCs. HEALTH AND SAFETY There is little documentation as yet of safe han- Health hazards associated with MMCs are sim- dling and machining practices for MMCs. Mate- ilar to those found in the production of ceram- rials handling practices are given by materials ics and PMCs. As with ceramics the most serious safety data sheets, and few yet exist for MMCs. However, there is one materials safety data sheet that applies to the MMC production process of lqRObefl BUffenbarger, I rlternational Assoclatlon of Machinists and plasma spray ing.14 Aerospace Workers, personal communication, March 23, 1987. 112 . Advanced Materials by Design health hazard is associated with the possible car- boria-silica. The effects of ceramic fibers on hu- cinogenic effects of ceramic fibers due to their mans are largely unknown. Until such data be- size and shape. MMC reinforcement fibers fall- come available, the indications discussed in chap- ing in this category include alumina, alumina- ter 2 for ceramics also apply to the manufacture silica, graphite, boron carbide, and alumina- of MMCs reinforced with these fibers. APPLICATIONS There are very few commercial applications of Current Applications MMCs at the present time. Industry observers be- lieve that the level of development effort in the Current MMC markets in the United States are United States is not large enough to lead to sig- primarily military. MMCs have potential for use nificant near-term commercial use of MMCs. in aircraft structures, aircraft engines, and naval However, the Toyota truck diesel engine piston weapons systems. Experimental MMC compo- has spurred the major U.S. automakers to under- nents were first developed for applications in air- take preliminary activity in MMCs. Although con- craft, jet engines, rockets, and the space shuttle. siderable interest in these materials is being gen- There has been little government funding of erated in the United States, it will be decades MMCs for commercial applications in the United before they are likely to have an appreciable im- States, and only a small number of specialized pact on production levels of competing materials. applications have been developed by private in- dustry. MMCs are not competing solely with mono- lithic metals; they are also competing with the Military/Space whole range of advanced materials, including The high stiffness and compression strength and PMCs, ceramics, and other new metal alloys. It low density of boron fiber-reinforced aluminum is not yet clear whether, compared to PMCs, ce- led to its use in production space shuttle orbiter ramics, and monolithic metals, MMCs will have struts. Its high cost has prevented wider use. big enough performance advantages to warrant use in a wide variety of applications. In fact, The National Aeronautics and Space Adminis- MMCs may be limited to niche applications in tration (NASA) Hubble Space Telescope uses two which the combinations of properties required antenna masts made of aluminum reinforced with cannot be satisfied by other structural materials. P-100 pitch-based graphite fibers. This material was selected because of its high specific stiffness The properties that make MMCs attractive are 16 and low coefficient of thermal expansion. This high strength and stiffness, good wear resistance, material replaced a dimensionally stable telescope and tailorable coefficient of thermal expansion mount and an aluminum waveguide, resulting in and thermal conductivity. Furthermore, develop- a 70 percent weight savings. 17 ment of high-temperature MMCs has been cited as a way to help reduce U.S. dependence on crit- Two companies are producing silicon carbide ical and strategic materials, such as manganese particulate-reinforced aluminum instrument cov- and cobalt. ’ 5 The following sections describe the ers for a missile guidance system. This is the first current and future applications for which these production application of particulate-reinforced properties are of value. MMCsin the United States. 161bid. I Twilllam C, Riley, Research Opportu nites, Inc., personal com- IJzweben, op. cit., January 1987 munication, October 27, 1987. Ch. 4—Metal Matrix Composites ● 113 AIRFOIL CROSS SECTION X75 X100 Photo credit: NASA Lewis Research Center Tungsten wire-reinforced super alloy gas turbine engine blade Commercial The Toyota piston has stimulated a consider- able interest in MMCs for pistons and other au- Photo credit: Advanced Composite Materials tomotive parts on a worldwide basis. Other com- Missile guidance system covers of silicon carbide ponents now being evaluated by automakers particle-reinforced aluminum. world-wide include connecting rods, cam fol- lowers, cylinder liners, brake parts, and drive shafts. Military/Space Experimental MMC bearings have been tested Based on information in the public domain, the on railroad cars in the United Kingdom. An ex- following applications appear likely to be devel- perimental material for electronic applications has oped in the United States: high-temperature been developed in Japan, consisting of copper fighter aircraft engines and structures, high-tem- reinforced with graphite fiber, Another electrical perature missile structures, spacecraft structures, use of MMCs is in circuit breakers. Graphite- high-speed mechanical systems, and electronic reinforced copper used as a “compliant layer” packaging. minimizes thermal stresses in an experimental Development of applications such as hyper- magnetohydrodynamic (MHD) generator ceramic sonic aircraft, which will require efficient high- channel in Japan. An aluminum tennis racket temperature structural materials, will undoubt- selectively reinforced with boron fiber was sold edly lead to increasing interest in MMCs. commercially in the United States for a brief time during the 1970s, Commercial Future Applications Commercial applications in the next 5 years are likely to be limited to diesel engine pistons, and Future applications include those which could perhaps sporting goods such as golf clubs, tennis be possible in the next 5 to 15 years. rackets, skis, and fishing poles. There are a num- .—— . 114 . Advanced Materials by Design ber of potential applications that are technically possible but for which the current level of devel- opment effort is inadequate to bring about com- mercialization in the next 5 years; these include: brake components, push rods, rocker arms, ma- chinery and robot components, computer equip- ment, prosthetics, and electronic packaging. High Specific Stiffness and Strength.–MMC materials with high specific stiffness and strength are likely to have special merit in applications in which weight will be a critical factor. Included in this category are land-based vehicles, aircraft, ships, machinery in which parts experience high accelerations and decelerations, high-speed shafts and rotating devices subject to strong centrifu- gal forces. The high value of weight in aircraft makes use of MMCs a strong possibility for structural appli- cations, as well as for engine and other mechan- nents, use of materials with high specific prop- ical system components. Mechanical properties erties - MMCs - will be a way of achieving future of MMCs could be important for a number of performance goals. medical applications, including replacement joints, bone splices, prosthetics, and wheelchairs. For high-speed rotating shafts, such as automo- bile and truck drive shafts, a major design con- There are numerous industrial machinery com- sideration is that the rotational speed at which ponents that could benefit from the superior spe- the shaft starts to vibrate unstably, called the crit- cific strength and stiffness of MMCs. For exam- ical speed, must be higher than the operating ple, high-speed packaging machines typically speed. As critical speed depends on the ratio of have reciprocating parts. Some types of high- stiffness to density, the high specific stiffness of speed machine tools have been developed to the MMCs makes them attractive candidates for this point where the limiting factor is the mass of the application. assemblies holding the cutting or grinding tools, which experience rapid accelerations and de- Attractive Thermal Properties. -There are a celerations. Further productivity improvements number of potential future applications for which will require materials with higher specific me- the unique combinations of physical properties chanical properties. Computer peripheral equip- of MMCs will be advantageous. For example, the ment, such as printers, tape drives, and magnetic special needs of electronic components present disk devices commonly have components that particularly attractive opportunities. must move rapidly. MMCs are well suited for Electronic devices use many ceramic and ce- such parts. ramic-like materials, that are brittle and have low The excellent mechanical properties of MMCs coefficients of thermal expansion (CTEs). Exam- make them prime candidates for future applica- ples are ceramic substrates such as alumina and tion in robots, in which the weight and inertia beryllia, and semiconductors such as silicon and of the components have a major effect on per- gallium arsenide. These components frequently formance and load capacity. Centrifugal forces are housed in small, metallic packages. MMCs are a major design consideration in high-speed can help prevent fracture of the components or rotating equipment, such as centrifuges, gener- failure of the solder or adhesive used to mount ators, and turbines. As these forces are directly these components, since the CTE of the package proportional to the mass of the rotating compo- can be tailored to match that of the device. Ch. 4—Metal Matrix Composites ● 115 Another desirable feature of packaging mate- Markets rials is high thermal conductivity to dissipate heat generated in the system, since the reliability of Market projections for MMCs vary widely. One electronic chips decreases as operating temper- market forecast by C. H. Kline is that MMCs will play no significant role in the current advanced ature increases. Two of the more common me- 18 tals now used in packaging are molybdenum and composite markets until after 1995. A second Kovar, a nickel-iron alloy. The thermal conduc- forecast (Technomic Consultants) is that U.S. non- tivity of Kovar is quite low, only about 5 percent military uses of MMCs will reach $100 million per year by 1994, and world-wide commercial uses of that of copper, and it cannot be used in appli- 19 cations in which large amounts of heat must be will reach $2 billion per year. dissipated. Molybdenum, which is more expen- There does seem to be agreement though, that sive and difficuIt to machine, is normally used in in the United States, MMC materials are likely to such cases. MMCs (e. g., with a high thermal con- be used primarily in military and space applica- ductivity copper matrix) could be used instead tions, and, to a much smaller degree, in electronic of these two materials. Examples of potential fu- and automotive applications. Because MMC ma- ture applications include heat sinks, power semi- terials are currently used mainly for research pur- conductor electrodes, and microwave carriers. poses, the markets for them are now only a few 20 The low CTE that can be achieved with some thousand pounds per year. Materials costs should MMCs makes them attractive for use in precision decrease with time, as production volumes in- machinery that undergoes significant temperature crease. However, the actual downward trend has change. For example, machines that assemble been slower than most predictions, and the cost/ precision devices are commonly aligned when performance benefits of MMCs have yet to be cold. After the machines warm up, thermal ex- demonstrated over alternative materials in large pansion frequently causes them to go out of align- volume applications. ment. This results in defective parts and down time required for realignment. Laser devices, —.. — which require extremely stable cavity lengths, are lgjacques shou~ens, Metal Matrix Composites Information Anal- ysis Center (MMCIAC), personal communication, March 27, 1987. another potential application for which low CTE lglbid. is an advantage. ZOI bid. RESEARCH AND DEVELOPMENT PRIORITIES Federal funding of MMC research and devel- The following section describes R&D priorities opment (R&D) comes mainly from the military. for MMCs in three broad categories of descend- Combined totals for the three services plus the ing priority. These categories reflect a consensus Defense Advanced Research Projects Agency as determined by OTA of research that needs to (DARPA) for 6.1,6.2, and 6.3A money were $29.7 be done in order to promote the development million for fiscal year 1987.21 There are a num- of these materials. ber of classified projects, and projects in other categories of funds, that also involve MMCs. Al- though the Department of Defense is the major Very Important government funding source, NASA also funds Cheaper Processes MMC research. NASA plans to provide $8.6 mil- lion for MMCs in fiscal year 1988, up from $5.6 First in importance is the need for low-cost, million in fiscal year 1987.22 highly-reliable manufacturing processes. Several industry experts advocate emphasis on modified ~ 1 Jerome” Persh, Department of Defense, personal comm u nlca- casting processes; others suggest diffusion bond- tlon, August 1987. ~~Brlan Qulgley, NatlOndl Aeronautics and Space Administration, ing and liquid metal infiltration as likely candi- personal communication, December 1987. dates for production of fiber-reinforced MMCs. 116 ● Advanced Materials by Design There is some agreement that plasma spraying Important is also a promising method. For particulate-rein- forced MMCs, powder metallurgy and liquid in- Environmental Behavior filtration techniques are considered most prom- It is critical to understand how reinforcements ising. To develop near-term applications, research and matrices interact, particularly at high tem- should concentrate on optimizing and evaluat- peratures, both during fabrication and in service. ing these processes, including development of A thorough understanding of material behavior low-cost preforms. is necessary to ensure reliable use and to provide guidelines for development of materials with im- proved properties. To date, study of the behavior Cheaper Materials of MMCs in deleterious environments has been Development of high-strength fiber reinforce- much more limited than for PMCs. Research is ments of significantly lower cost is a major need, needed in the areas of stress/temperature/defor- as there are no high-performance, low-cost fibers mation relations, strength, mechanical and ther- available at present. There are two schools of mal fatigue, impact, fracture, creep rupture, and thought as to the best approach to reducing costs. wear. Some analysts believe that the range of useful- ness can be expanded by the development of Fracture new fibers with better all-purpose design prop- The subject of fracture behavior in MMCs erties, such as higher strength, higher tempera- deserves special attention. The applicability of ture, and lower cost; they also see new matrix traditional analytical techniques is controversial alloys as important to facilitate processing and to because MMCs are strongly heterogeneous ma- optimize MMC performance. However, some terials. It seems reasonable that these traditional critics charge that this search for all-purpose fibers techniques should be valid at least for particulate- and better matrices is likely to be unrewarding reinforced MMCs, because they do not appear and that increased production experience with to have the complex internal failure modes asso- present fibers and matrices is the best route to ciated with fiber-reinforced MMCs. In view of the lower costs, particularly for potential near-term lack of agreement on how to characterize frac- applicat ions. ture behavior of MMCs, though, it will be nec- essary to rely on empirical methods until a clearer Interphase picture emerges. Control over the fiber/matrix interphase in Nondestructive Evaluation MMCs is critical to both the cost and perform- ance of these materials. For example, new fiber Reliable NDE techniques must be developed coatings are needed to permit a single fiber to for MMCs. They should include techniques for be used with a variety of matrices. This would detecting flaws and analytical methods to evalu- be cheaper than developing a new fiber for each ate the significance of these flaws. In MMCs as matrix. in PMCs, there is the possibility of many kinds of flaws, including delamination, fiber misalign- At high temperatures, fiber/matrix interactions ment, and fracture. There are no N DE procedures can seriously degrade MMC strength. Research presently available for measuring the extent of in the area of coatings is desirable, not only to undesirable reinforcement/matrix interaction and prevent these deleterious reactions but also to resultant property degradation. promote the proper degree of wetting to form a good fiber/matrix bond. Coatings add to the ma- Machining terial and processing costs of MMCs, so that re- search into cheaper coatings and processes is es- The machining of MMCs is currently a very ex- sential. pensive process that requires diamond tools be- .- Ch. 4—Metal Matrix Composites ● 117 cause of the materials’ very hard and abrasive ce- fabricating MMCs. What are needed are design ramic reinforcements. As machining is a major methods that take into account plasticity effects cost factor, development of improved methods and provide for development of efficient, selec- tailored to the unique properties of MMCs would tively reinforced structures and mechanical com- help to make these materials more competitive. ponents. Research on modeling of processing be- havior is necessary, together with the eventual Desirable development of databases of properties and proc- ess parameters. Modeling Analytical modeling methods would be of value in helping to develop and optimize processes for Chapter 5 Factors Affecting the Use of Advanced Materials CONTENTS Page Finding s...... 121 Introduction...... 122 Integrated Design . . . . ● ****** ● ...... ● .*.*.. .*....*. .. 122 Systems Approach to Costs ...... 123 Education and Training...... , . ., . ...,..., ..,,...124 Multidisciplinary Approach ...... 125 Standards ....,...... 126 Standard Test Methods ...... 126 U.S.Standardization Efforts ...... ,..127 lnternational Standardization Efforts...... ,.....127 Automation ...... ● *. ,,,,. .,, ...... ,,. ● 128 , Computer-Aided Design Systems ....; ...... ,.128 Modeling ...... ,128 Computerized Processing Equipment...... 128 Robotics and Material Handling...... ,...... 129 Sensors and Process Monitoring Equipment ...... ,...... 129 Statistical Process Control ...... 129 Computer-Aided Design and Manufacturing...... ,....131 Expert Systems ...... ,...... ● . . . . ., * .,*.*...... 131 Considerations for ...... ,,..,..,..131 Advanced Structural Material Design...... ,...... ● *.*,** . . . . . 132 Advanced Structural Materials Production ...... 132 . Tables Table No. Page 5-1. Polymer Matrix Composite Design Parameters...... ,.122 5-2, Hypothetical Multidisciplinary Design Team for a Ceramic Component ...125 S-3. Reasons for Automating, and Appropriate Types of Automation ...... ,..133 — Chapter 5 Factors Affecting the Use of Advanced Materials FINDINGS Because of the intimate relationship between skilled engineers who have strong backgrounds advanced materials and structures produced from in these advanced materials. Retraining will be them, the design and manufacture of these new required for engineers already in the work force, materials must be treated as an integrated proc- and training in manufacturing with these mate- ess. These materials make it possible to form parts rials will be needed for production workers. and systems in larger, more combined operations than are possible with traditional metals technol- Standards ogy. one operation can form both the part and the material, thereby eliminating costly assem- Several types of standards will facilitate inte- bly operations. The need for such an integrated, grated design with advanced materials: quality or unified, approach will affect all aspects of man- control standards applied at each stage of the ufacturing. manufacturing process, product specification standards, and standardized test methods for ma- terials qualification. Numerous groups in the costs United States are working on domestic materi- Although the high per-pound cost is currently als standards, although progress has been slow. a barrier to the increased use of advanced struc- There is also a large domestic effort on the part tural materials, low cost could become a selling of the Japanese. Several international organiza- point for these materials in the future if systems tions are also attempting to develop international costs are considered. Advanced structural mate- standards for advanced materials. rials offer the opportunity to consolidate parts and reduce manufacturing and assembly costs. In Automation general, use of advanced materials will only be cost-effective if the manufacturer can offset higher Those forms of automation that aid the integra- raw materials costs with savings in assembly and tion of design and manufacturing will be of great maintenance costs. use in speeding up the acceptance of the new materials. These might include design databases, automated processing equipment and sensors for Multidisciplinary Approach process information feedback. Automation can help reduce material and process cost, ensure The integrated nature of advanced materials part quality, and eliminate the long manufactur- manufacturing will require close cooperation be- ing times inherent in some processes. tween research scientists, designers and produc- tion engineers. Effective commercialization will Technical challenges for the automation of ad- require teams that bring together expertise from vanced materials production are generally simi- many professional disciplines. lar to those for traditional metals production; however, such problems as the lack of design Education and Training data and strict quality control requirements may be more serious for advanced composite or ce- Cooperation and blending across different dis- ramic part production. Automation will proceed ciplines in industry will require interdepartmen- slowly, given the newness of the materials and tal educational opportunities for students in uni- the time needed to develop experience with, and versities. At the same time there is a need for confidence in, their use. 121 122 . Advanced Materials by Design INTRODUCTION The future of advanced materials involves more ent from the sequential manufacturing processes than purely technical changes. Other factors that associated with conventional materials. With me- will affect the development and commercializa- tals, the materials and processes are determined tion of these materials are: an integrated approach by the specifications; with advanced materials, to design and manufacturing, a systems approach the materials and manufacturing processes are to cost, interdisciplinary research and production, designed with the aid of the specifications. education and training, standards development, The principle of integration will have a strong and automation of design and manufacturing influence on the future use of advanced materi- processes. als. This development will depend on more uni- Because advanced ceramics and composites fied approaches to problem solving, requiring a are tailored to suit their applications, these ma- broader view on a wide range of issues. An in- terials cannot be considered apart from the struc- tegrated approach will be imperative, not just in tures made from them. Both material and struc- finding solutions to technical challenges, but also ture are manufactured together in an integrated in dealing with various institutional and economic fabrication process. This is fundamentally differ- issues. INTEGRATED DESIGN When designing a structure to be made of metal, Table 5-1.—Polymer Matrix Composite the design team specifies the metal to be used Design Parameters and has a rough idea of its final properties. This Tensile strength x,y team then can simply hand the design over to Tensile stiffnesses x,y the production team. The production team, in 3. Elongation at break x,y separate operations and without further contact 4. Flexural strength 5. Flexural stiffnesses with the designers, treats the metal to achieve the 6. Compressive strength x,y microstructure and mechanical properties that 7. Compressive stiffnesses x,y 8. Shear strength (short beam shear test and/or off- the designers envisioned, shapes the structure in axis tensile test) a rough fashion, and finishes it to have the pre- 9. Shear stiffnesses x,y cise shape desired. 10. Interlaminar strength (Gc) 11. Impact strength With advanced composites and ceramics, these 12. Compression strength after impact 13. Coefficient of thermal expansion x,y steps are collapsed into a single processing step; 14. Hydroscopic expansion (moisture coefficient x,y) thus a design team working with these materials 15. Poisson’s ratios x,y cannot be separated from the manufacturers of 16. Fiber volume content 17. Void content the part. Design of the material, structure, and 18. Density manufacturing process is called integrated design. x,y: In two directions, parallel and perpendicular to the long direction of the rein- forcement fiber. Integrated design requires a large amount of NOTE: These design parameters are a few of the large number of design parameters which give rise to the plethora of variables which must be con- data. Some of the kinds of materials property in- trolled during manufacturing. formation a designer might want are shown in SOURCE: Materials Modeling Associates, “Properties, Costs, and Applications of Polymeric Composites,” contractor report for OTA, December 1985. table 5-1. Mechanical properties of ceramic and composite structures, as well as of the constitu- ent materials, will be needed for a wide variety There is currently a great deal of effort under- of materials. Processing parameter data and cost way by many different groups to determine what data will also be important in material and proc- might comprise a materials design database for ess choice. PMCs. (Ceramic and metal matrix composite Ch. 5—Factors Affecting the Use of Advanced Materials s 123 [MMC] technologies are less evolved and may not reducing tendencies to overdesign and through be ready at this time for database development.) shortening design time. Ideally this data should be available for a wide Several attempts are being made to establish range of fibers and matrices. A comparison of the databases for advanced materials. The National costs of different materials would also be a desira- Bureau of Standards is currently attempting to de- ble feature of such a materials database. velop a protocol for an electronic database for To direct the manufacture of a part, or to be ceramic materials. In the private sector, one ef- able to design a part with forethought on how fort underway to create a centralized database it could be manufactured, processing variables is the National Materials Properties Data Net- databases would also be necessary. These data- work, which plans to provide its subscribers with bases would include variables such as curing the capability to search electronically a large times of resins and heat treatment curves for ob- number of data sources that have been evaluated taining various microstructure, and, most nota- by experts.1 bly, processing costs. A processing database would be of greatest benefit in deriving proper- ties of a composite or ceramic structure as a whole. Having this knowledge could allow cus- I Materials and Processing Report, Renee Ford, Ed., MIT Press, tom tailoring of parts, and may trim costs through Cambridge, MA, February, 1987. SYSTEMS APPROACH TO COSTS It is often stated that the three biggest barriers mature. For instance, the cost of a pound of to the increased use of advanced materials are standard high-strength carbon fiber used to be cost, cost, and cost. In a narrow sense, this ob- $300 but is now less than $20, and new processes servation is correct. If advanced materials are con- based on synthesis from petroleum pitch prom- sidered on a dollar-per-pound basis as replacements ise to reduce the cost even furthers If high- for steel or aluminum in existing designs, they strength carbon fibers costing only $3 to $5 per cannot compete. This has often been the percep- pound were to become available, major new op- tion of potential user industries, which tend to portunities would open up for composites in au- be oriented toward metals processing. However, tomotive, construction, and corrosion-resistant per-pound costs and part-for-part replacement applications. costs are rarely valid bases for comparison be- Advanced ceramics and composites should tween conventional and advanced materials. really be considered structures rather than ma- A more fruitful approach is to analyze the over- terials. Viewed in this light, the importance of a all systems costs of a shift from conventional ma- design process capable of producing highly in- terials to advanced materials, including integrated tegrated and multifunctional structures becomes design, fabrication, installation, and Iifecycle clear. Polymer matrix composites (PMCs) provide costs. 2 On a systems cost basis, the advanced ma- a good example. In fact, the greatest potential terials can compete economically in a broad economic advantage of using such materials, be- range of applications. Moreover, the high per- yond their superior performance, is the reduc- pound cost is largely a result of the immaturity tion in the manufacturing cost achieved by reduc- of the available fabrication technologies and the ing the number of parts and operations required low production volumes. Large decreases in ma- in fabrication. For example, a typical automobile terials costs can be expected as the technologies body has about 250 to 350 structural parts. Using an integrated composite design, this total could 2 “How Should Management Assess Today’s Advanced Manufac- turing Options, ” Industry Week, May 26, 1986, pp. 45-88. 3/rOn Age, June 20, 1986, P. J6 124 ● Advanced Materials by Design be reduced to between 2 and 10 parts, with ma- percent of it due to the introduction of lightweight jor savings in tooling and manufacturing costs.4 materials such as high-strength steel, plastics, and aluminum. 8 Increases in fuel prices would en- Fuel Costs courage some further interest in advanced com- posites for automotive applications. (For further Fuel costs also represent an important factor discussion of the impact of energy costs on use that can affect the competitiveness of advanced of composites in automobiles, see chs. 6 and 7.) ceramics and composites compared with conven- tional structural materials. The cost of the energy In aircraft, one of the major benefits of using required to manufacture ceramic and compos- PMCs is lower Iifecycle costs derived from bet- ite components is only a negligible fraction of ter fuel efficiency, lower maintenance costs and longer service life. This has already been dem- overall production costs. However, the high po- tential for energy savings when the component onstrated by the fact that there was a significant increase in the use of PMCs in aircraft when oil is in service is a major reason for using advanced 9 ceramics and composites. 5 prices were greater than $30 per barrel. It is also evident however, that Iifecycle costs and capi- penetration of ceramics into such applications tal, materials, and labor costs (notably the high as heat exchangers, industrial furnaces, industrial labor costs of hand lay-up) are design trade-offs cogeneration, fluidized bed combusters, and gas which determine the choice of materials. When turbine engines depends on energy costs. Ce- oil prices drop as low as $12 per barrel (as they ramic heat exchanger systems have potential for did in the fall of 1986), the relatively high cost greater than 60 percent fuel savings.6 Ceramics of composite materials makes them unattractive used in advanced turbines could result in 30 to to the aircraft manufacturer.10 60 percent fuel savings.7 There are predictions that low oil prices will Weight reduction, through intensive use of continue through the year 2000, and that jet fuel PMCs in automobiles, may be translated into prices will not even increase as quickly as crude improved fuel economy and performance, and oil prices.11 This does not necessarily mean that thereby lower vehicle operating cost. The trend gains made in use of composites in aircraft will toward fuel-efficient automobiles after the oil cri- be reversed. Rather, the persistent low energy sis of 1973-74 resulted in a substantial decrease costs are likely to reduce the incentives to in- in the average weight of an automobile, some 25 crease the use of composites in structures now made of aluminum. 4P. Beardmore et al., Ford Motor Co., “Impact of New Materials on Basic Manufacturing Industries—Case Study: Composite Automo- ‘Steven R. Izatt, “Impacts of New Structural Materials on Basic bile Structure, ” contractor report for OTA, March 1987. Metals Industries,” contractor report for OTA, April 1987. 5 David W. Richerson, “Design, Processing, Development and 9A.S. Brown, “Pace of Structural Materials Slows for Commer- Manufacturing Requirements of Ceramics and Ceramic Matrix Com- cial Transports, ” Aerospace America, American Institute of Aer- posites,” contractor report for OTA, December 1985. onautics and Astronautics, June 1987, pp. 18-21, 28. 6 S.M. Johnson and D.J. Rowcliffe, SRI International Report to EPRI. 10 Ibid. “Ceramics for Electric Power-Generating System s,” January 1986 11 p.D. HOltberg, T.J. Woods, and A. B. Ash by, “Baseline projec- 7Richerson, op. cit., December 1985. tion Data Book, ” Gas Research Institute, Washington, DC, 1986. EDUCATION AND TRAINING The expanding opportunities for advanced ce- or composite materials. There is also a shortage ramics and composites will require more scien- of properly trained faculty members to teach the tists and engineers with broad backgrounds in courses. However, considerable progress is be- these fields. At present, only a few U.S. univer- ing made in the number of students graduating sities offer comprehensive curricula in ceramic with degrees in advanced materials fields. In the Ch. 5—Factors Affecting the Use of Advanced Materials . 125 1984-85 academic year, a total of 77 M.S. degrees, aerospace industry. Continuing education is espe- and 34 Ph.D.s were awarded in ceramics in the cially important in relatively low-technology in- United States. One year later the totals were 139 dustries such as construction, which purchase, and 78, respectively. About 40 percent of the rather than produce, the materials they use. Some Ph.D.s were foreign students. No estimates were universities and professional societies are now available on how many of the foreign students offering seminars and short courses to fill this gap; subsequently returned to their home countries.12 such educational resources should be publicized The job market for graduates with advanced and made more widely available, degrees in ceramic or composite engineering is Beyond the training of professionals, there is good, and can be expected to expand in the fu- a need for the creation of awareness of advanced ture. Stronger relationships between industry and materials technologies among technical editors, university laboratories are now providing greater managers, planners, corporate executives, tech- educational and job opportunities for students, nical media personnel and the general public. In and this trend is expected to continue. recent years, there has been a marked increase There is a great need for continuing education in the number of newspaper and magazine arti- and training opportunities in industry for designers cles about the remarkable properties of advanced and engineers who are unfamiliar with the new ceramics and composites, as well as in the num- materials. In the field of PMCs, for instance, most ber of technical journals associated with these of the design expertise is concentrated in the materials. The success of composite sports equip- ment, including skis and tennis rackets, shows lzBusiness Communications Co., InC., “Strategies of Advanced Materials Suppliers and Users, ” contractor report for OTA, Jan. 28, that new materials can have a high-tech appeal 1987. to the public, even if they are relatively expensive. MULTIDISCIPLINARY APPROACH Commercialization of advanced materials re- Table 5.2.—Hypothetical Multidisciplinary Design quires a team effort. In producing a typical ce- Team for a Ceramic Component ramic component, the team could consist of one Specialist Contribution or more professionals from each of several techni- Systems engineer ...... Defines performance cal disciplines, as illustrated in table 5-2. Disciplines Designer ...... Develops structural concepts that overlap materials science and engineering Stress analyst ...... Determines stress for local environments and difficult are: solid state physics; chemistry; mechanical, shapes electrical, and industrial engineering; civil and Metallurgist ...... Correlates design with metallic biomedical engineering; mathematics; and aero- properties and environments Ceramist ...... Identifies proper composition, space, automotive, and chemical engineering. reactions, and behavior for Materials research lends itself naturally to col- design laborative institutional arrangements in which the Characterization analyst. . . Utilizes electron microscopy, X-ray, fracture analysis, etc. rigid disciplinary boundaries between different to characterize material fields are relaxed. Ceramic manufacturer . . . . Defines production feasibility SOURCE: J.J. Mecholsky, “Engineering ResearchNeeds of Advanced Ceramics Similarly, interjector cooperation in materials and Ceramic Matrix Composites, ” contractor report for OTA, Decem- research could speed the development of advanced ber 1985. materials. New mechanisms for collaborative work among university, industry, and government als development and utilization’, (The role of gov- laboratory scientists and engineers are having a ernment/university/industry collaborative R&D is salutary effect on the pace of advanced materi- explored in greater detail in ch. 10.) 126 . Advanced Materials by Design STANDARDS There are many problems inherent in setting gine applications. These materials have a broad standards in rapidly moving technologies.13 range of potential uses, but designers cannot Standards development is a consensus process compare them or use them without a reliable that can take years to complete, and it is likely database on standard compositions having speci- to be all the slower in this case because of the fied properties. While there is a danger in prema- complex and unfamiliar behavior of advanced ce- turely narrowing the possibilities, these experts ramics and composites. As these technologies say, there is also a danger in not developing the mature, though, such difficulties will generally be- materials already available. Opponents of this come more tractable. view argue that, since large commercial markets are still far in the future, there is no need to set- The extensive data requirements of integrated tle for present materials and processes. On the design can be simplified by material standards to reduce the volumes of data that are processed, contrary, they say, the focus should be on new and by data transfer standards to permit the effi- materials and processes which can “leapfrog” the present state-of-the-art. This classic dilemma is cient handling of data. Standards are essential for the generation of design data, and for reliability characteristic of any rapidly evolving technology. specifications for advanced materials sold domes- tically or abroad. Areas that could benefit from Standard Test Methods the formulation and application of standards in- The need for standard test methods has long clude: quality control, product specifications, been identified as an important priority. For and, most importantly, materials testing. homogeneous materials such as metals, testing The two keys to competitiveness in any area methods are fairly straightforward. In composites, of manufacturing are quality assurance at low however, the macroscopic mechanical behavior cost. Quality control standards applied at each is a complex summation of the behavior of the stage of the manufacturing process help to en- microconstituents. Consequently, there has been sure high product quality and low rejection rates. great difficulty in achieving a consensus on what For instance, there is a need for standards applied properties are actually being measured in a given to ceramic powders and green bodies (unsintered test, let alone what test is most appropriate for ceramic shapes) to minimize the flaws in the fi- a given property. Currently there are numerous nal sintered product. Product specification stand- test methods and private databases in use through- ards, largely determined by the requirements of out the industry. This has resulted in consider- the buyer, provide the buyer with assurance that able property variability in papers and reports. the product will meet his needs. The variability problem is particularly severe for testing of toughness, bending, shear, and com- As a way to accelerate the commercialization pression properties. of advanced materials, some experts advocate choosing one or two materials in a given cate- Standardized test methods would not only fa- gory and concentrating on producing uniform, cilitate consistent reporting of materials proper- high-quality components from these. In ceram- ties in the research literature, but they could also ics, for instance, silicon carbide, silicon nitride, drastically reduce the costs of the repetitive test- and zirconia would be possible candidates, be- ing presently necessary to qualify new materials cause they have already received a large amount for use in various applications.14 Due to liability of research funding over the years for heat en- concerns, a new material must be qualified by extensive testing for an individual application be- fore a user company will incorporate it into a 13 J. David Roessner, “Technology Policy in the United States: system. Structures and Limitations,” Technovation, vol. 5, 1987, p. 237, provides a brief case study of problems in setting standards in the early stages of development of numerically controlled machine tools. I qThis is discussed for polymer matrix composites in ch. 11. Ch. 5—Factors Affecting the Use of Advanced Materials . 127 At present, each defense prime contractor com- as the lead service, has recently initiated a new pany qualifies its material for each separate de- program for standardization of composites tech- fense or aerospace application according to its nology (CMPS).16 CMPS is attempting to promote own individual tests and procedures. Data on ma- the integration of diverse standards for compos- terial properties are often developed under gov- ites by gathering standardized test methods (e.g., ernment contract (costing $100,000 to $10 mil- from ASTM) into Military Handbook 17(MIL-17) lion and taking up to 2 years), but companies are and by developing separate test methods where reluctant to share the results. Even when data are necessary. 17 A Joint Army-Navy-NASA-Air Force reported in the literature, often the type of test (JANNAF) Composite Motor Case Subcommittee used and the statistical reliability of the results are is developing standard test methods for filament not reported with the data. Although the lack of wound composites used for rocket motor cases.18 standards probably does not inhibit the expert As part of CMPS, the Army Materials Labora- designer of composite aerospace structures, the tory in Watertown, MA, has established coordi- availability of standards could encourage the use nation with a variety of organizations, including of composites in industries such as construction, ASTM, the Composites Group of the Society of where designers have no familiarity with the ma- Manufacturing Engineers (COGSME), the Society terials. of Automotive Engineers (SAE), the Society for the Advancement of Material and Process Engineer- U.S. Standardization Efforts ing (SAMPE), American Society for Metals (ASM) The American Society for the Testing of Mate- International, the Society of Plastics Engineers rials (ASTM), provides the United States with an (SPE), and the Society of the Plastics Industry (SPI). excellent and internationally respected mecha- nism for setting materials standards. ASTM has International Standardization Efforts recently established an Advanced Ceramics Com- mittee (C-28), which is now staffing subcommit- International organizations that are pursuing tees in the fields of properties, performance, de- advanced materials standards include the Ver- sign and evaluation, characterization, processing, sailles Project on Advanced Materials and Stand- and terminology. The ASTM Committee on High ards (VAMAS), and the International Energy Agency Modulus Fibers and Their Composites (D-30) and (IEA). VAMAS is now formally independent, hav- the Committee on Plastics (D-20) are the principal ing begun as an outgrowth of the periodic summit sources of standardized test methods for PMCs. meetings of the heads of government of Canada, Advanced materials trade associations such as the France, the United Kingdom, West Germany, United States Advanced Ceramics Association Italy, Japan, the United States, and the European (USACA) and the Suppliers of Advanced Com- Community. Subdivided into 13 technical work- posite Materials Association (SACMA) have also ing areas, VAMAS is attempting to improve the been working with ASTM and government agen- reproducibility of test results among laboratories cies to develop standards. by round robin testing procedures designed to identify the most important control variables. U.S. On the users’ side, the Aircraft Industries Asso- liaison with VAMAS is primarily through the Na- ciation has initiated Composite Materials Charac- tional Bureau of Standards (NBS). terization, Inc. (CMC), a consortium of aerospace companies involved in fabricating composites. CMC is conducting limited materials screening tests on composite materials for its members.15 Consistent with its growing interest in compos- ites, the Department of Defense, with the Army 16u .s. @pa~rnent of Defense, Standardization program plan, Composites Technology Program Area (CMPS), Mar. 13, 1987. 17A draft of Ml L 17 was being evaluated at this Writing. 15Advanced Composites, July/August 1987, p. 45 18 U.S. Department of Defense, op. cit., footnote 16. 128 “ Advanced Materials by Design The IEA is developing standards for character- coordinated through the Department of Energy. izing ceramic powders and materials. The prin- Currently, U.S. participation in these international cipal participants are the United States, Sweden, standards-related activities tends to be limited, and West Germany. U.S. liaison with the IEA is with funds being set aside from other budgets. AUTOMATION The term automation is used here to encom- options and trade-offs associated with various pass the wide range of new design and process- production strategies, including processing costs. ing technologies for advanced materials. Auto- mation of design and early development work Computerized Mathematical Modeling involves standardized materials and processing databases; computer-aided design (CAD) systems; To expand the capabilities of a CAD system, and computerized mathematical/ modeling of de- the designer would need accurate models of how sign and processing of the material. Automation the material and the part would behave in the of production processes can involve any combi- operating environment. Computerized mathe- nation of the following technologies: computer- matical models will be necessary to describe the ized processing equipment that can be used in relationships among materials properties, mate- a stand-alone fashion or in coordination with rial microstructure, environmental conditions, other technologies; robotic, instead of human, static and dynamic forces, manufacturing varia- handling of material; sensors and process moni- bles, and other aspects of design such as life toring equipment; statistical process control for prediction and repairability considerations. Math- better part quality; computer-aided manufacture ematical models may also aid in decreasing the (CAM) and “expert” systems software for coordi- amount of stored data needed. It may also prove nation of design and manufacture. possible to develop, during the design of a given component, temporary mathematical models, Computer-Aided Design Systems specific to that component. This wouId facilitate quick redesign of the component during the de- CAD systems currently focus on three-dimen- sign or prototype development phases.21 sional graphics manipulation, and many of them also have the capability for stress analysis of a Computerized Processing Equipment structure. CAD systems for mechanical drawings currently cannot recognize parts of a drawing as Computer control of all aspects of processing significant features; e.g., the collection of lines and manufacturing will be an important factor in that a designer sees as a hole is seen by the CAD increasing and maintaining the reliability and system as simply a collection of Iines.19 20 A com- reproducibility of parts made of advanced ma- prehensive CAD system that would facilitate the terials. What is required initially is processing process of choosing suitable materials, reinforce- equipment similar to today’s computer numeri- ment geometry, and method of fabrication is still cally controlled (CNC) machine tools for machin- far in the future. Such a system would require ing metal. Automated processing equipment is both materials databases on fiber and resin prop- being designed in-house by some aerospace man- erties and processing databases that would per- ufacturers and manufacturers of machine tools, mit modeling of the manufacturing steps neces- Currently, production equipment (computer sary to fabricate the part. The principal advantage controlled or otherwise), designed specifically for of such a system would be to define clearly the advanced materials is at a prototype stage. An ex- lgHerb Brody, “CAD Meets CAM, ” High Technology, May 1987, ample is automated tape-laying machinery for pp. 12-18. ZOMore sophisticated CAD systems exist for drawing electronic 21 Norman Kuchar, General Electric Co., personal Commu nica- circuits. tion, Apr. 15, 1987. Ch. 5—Factors Affecting the Use of Advanced Materials “ 129 PMCs. The tape-laying machines now available of composites.24 For this reason, applications for are modified milling machines similar to those robots in advanced material production are likely used for metalworking. There is a great deal of to be limited to the carrying of nondestructive interest in developing new programmable auto- evaluation sensors (see below) and a small amount mated tape-laying equipment, with computer- of part handling. Robots are currently used for aided determination of the tape-laying path.22 assembly operations such as welding. It may be that robots will be used in composite joining Another promising technology for automating operations, such as the application of adhesives. PMC production is the filament winding machine. Recent development work in flexible filament winding machines indicates that it may be pos- Sensors and Process Monitoring sible to generate complex, noncylindrical parts.23 Equipment Other processes for producing composite parts To monitor advanced materials processing on- that are good candidates for computerized proc- line (during the process), sensors are needed. This essing are: fast pultrusion processes, impregna- information must be sent to the computer and tion of prepregs, and three-dimensional fabrics analyzed, so that errors can be detected and any and preforms. needed corrections can be made while the part is still being formed. This procedure permits near- Ceramic processing techniques that could ben- instant correction of costly mistakes in process- efit from this sort of automation are shaping and ing. This is accomplished through the use of sen- densification methods, machining techniques, sors and monitoring equipment that can detect and particularly techniques for near-net-shape abnormal conditions without interfering with nor- processing, such as hot isostatic pressing and cast- mal processes. Sensors are used not only to de- ing techniques. tect major processing problems but also for the Microprocessors can monitor and control cy- fine-tuning of quality control. cle times and temperatures for such processes as There are many types of sensors: laser and hot isostatic pressing for ceramics and fast-curing other visual sensors, vibration-sensing monitors spray-up processes for PMCs. Equipment under that can operate in many frequency ranges, force computer control will eventually be used in part and power monitors, acoustic and heat-sensing finishing operations and assembly as well as par-t probes, electrical property probes (e.g., capaci- forming. tance- or inductance-based) and a host of other types. There are also many types of sensors that Robotics and Materials Handling can be used for part inspection once a part has Robots function as would a human hand and been completed; these include such techniques arm in manipuIating parts and materials. Robots as nondestructive evaluation (using acoustic and can also be used to hold and operate tools, such other vibrational methods, radiography, holog- as welding equipment or drills. Processes such raphy, thermal wave imaging, and magnetic res- as hand lay-up of composites currently require onance among other methods) and use of laser- a great deal of human handling of material, but based high-precision dimensional measuring ma- it is not necessarily cost-effective to replace a hu- chines. man with a robot directly in advanced material production. Processes such as filament winding Statistical Process Control and resin transfer molding are more likely to re- Quality control, in a general sense, means stay- place hand lay-up cost-effectively for certain types ing within predetermined tolerances or specifica- tions when manufacturing a batch of parts. Each - batch of parts has a statistical distribution of part 22 Roger Seifried, Cincinnati Milacron CO., personal communica tion, June 1, 1987. ZIDick McLane, Boeing Airplane Co., personal Communication, ZAT’irnOthy Cutowski, Massachusetts Institute of Technology, Per- Apr. 29, 1987. sonal communication, Apr. 15, 1987. 130 . Advanced Materials by Design qualities, all of which must fall within a certain also that the large majority of the parts in the tolerance range. Statistical process control en- batch are of the most desirable quality. compasses quality-control practices that ensure Statistical process control is mainly mathemati- that the statistical part quality distribution falls cal in nature and relies heavily on the sensor tech- within the tolerance range, and that this distri- 25 nologies described above for information inputs. bution is centered within the tolerance range. To apply the information gained from statistical This procedure ensures not only that part qual- process control techniques most effectively, feed- ity of all the parts in the batch is acceptable, but back into the manufacturing system must occur during the process of forming the batch. The in- formation fed back into the process is used to make the minor processing corrections that can 25 Kelth Beauregard, Perception Inc., “Use of Machine Vision TO significantly increase the reliability of the proc- Stay Within Statistical Process Control Limits of Dimensions, ” Cut- ting Tool Materials and Applications Clinic, Detroit, Ml, Society of ess, enhance the overall quality of each batch, Manufacturing Engineers, Mar. 11-13, 1986. and reduce the rejection rates of the final parts. Ch. 5—Factors Affecting the Use of Advanced Materials ● 131 Computer-Aided Design tem is essentially a type of artificial intelligence and Manufacturing and requires an extremely complex program that can make educated guesses when confronted CAD/CAM technology lies further in the future with a lack of hard knowledge. Such a system is than most of the automation technologies de- an assemblage of interactive software plus data- scribed here. The CAD systems described above bases that offer all of the working knowledge could help the designer choose a material and gleaned by experts in a particular field. A designer pick the least costly, most sensible process for inexperienced with composites or ceramics might manufacturing, as well as model the behavior of be able to use the system to learn how to design the part in service. A fully integrated CAD/CAM with the unfamiliar material. The benefits of an system would then send instructions to the cor- expert system for materials design are clear. These rect set of machines to process the material. It materials could become more accessible with the wouId also need to include instructions for proc- advent of such an expert system, and all design- ess variables, raw materials inventory, manufac- ers, whatever their level of experience, would ture or supply of tooling, production time sched- have an enhanced base on which to draw. uling, and other shop-floor considerations. Expert Systems Expert systems technology, like the CAD/CAM technology, lies far in the future. An expert sys- CONSIDERATIONS FOR IMPLEMENTING AUTOMATION Full automation implies an integration of all those forms of automation that could fill the facets of design, development, materials inven- needs of that company in a timely and cost- tory, production, quality assurance, product in- effective fashion. ventory, and marketing. Clearly such a degree Many industry experts feel that technologies of automation is far in the future for advanced such as advanced ceramics and composites are materials and will only occur when the dollar too new to warrant a large investment in auto- volume of advanced materials products is high mation. Automation is seen as an inflexible proc- enough to warrant the significant capital invest- ess requiring fixed, well-characterized process- ment needed for this type of production. Al- ing techniques. In the view of these experts, it though this degree of technical complexity is not will be many years before enough experience has yet available, all of these technologies are in- been gained with these materials to consider dividually of continuing interest to advanced ma- automation cost-effective. It will be useful to con- terials manufacturers. sider here what automation technologies offer for composites and ceramics manufacture and what It is important to note that this type of com- challenges face the automation of advanced ma- plete automation need not occur at once. in fact, terial production. for reasons of capital cost alone, it is wise not to implement a high degree of automation quickly. Automation offers three advantages: speed, Fortunately, some of these technologies can be reliability/reproducibility, and cost, However, verified and put in place well before others are these benefits cannot be realized simultaneously; available. It is necessary for each industry or com- trade-offs are required. A system that offers so- pany to decide what benefits of automation are phisticated controls and sensors for producing most important and to choose to incorporate parts to tight specifications may not be a system 132 ● Advanced Materials by Design that has enough speed (or low enough costs) to In addition, unexpected machining behavior use in high-volume applications. The capital in- may occur depending on factors that cannot be vestment required may not be low enough to known in advance, such as the rigidity, age, and make advanced materials attractive enough to brand of machine tool used. Thus, individual cor- use even in high-volume applications. Another rections must be made after the original param- trade-off is between flexibility and speed/cost. eters are chosen and tested. Robots or materials processing equipment that There are similarly a large number of variables can perform a wide range of tasks will not be as for the design of a metal part. At present, most inexpensive and operationally quick as equip- of the country’s design and production engineers ment dedicated to one particular task. working with metals use handbooks of incom- Currently, there are several major roadblocks plete tables to make best guesses as to design and to automation in the advanced materials field. process parameters. These data have been de- One is the inability to link machine tools, con- rived experimentally in an uncoordinated fash- trollers, and robots made by different manufac- ion over a period of decades. The situation for turers, or even by the same manufacturer at dif- composites databases is even more complicated ferent points in time. This problem of interfacing because of the larger number of component ma- nonstandard and dissimilar machines has been terials and materials interactions that must be under consideration by a number of organiza- taken into account. tions, most notably the Automated Manufactur- ing Research Facility (AMRF)26 at the National Bu- Advanced Structural Materials Design reau of Standards (NBS) and the Manufacturing 27 Most of the problems described above are Automation Protocol (MAP) system developed present whether the material is metal, ceramic, by General Motors. Some advanced materials ad- vocates have cited data transfer standards as or a composite. However automation is a much some of the most important standards needed for more problematic undertaking with advanced ce- ramics or composites than with metals. One ma- increased use of advanced materials. jor problem is the complexity of design. Another difficulty in automation is the wealth At this stage, design databases, both for mate- of information needed in electronic form which rials properties and the processes used in manu- presents difficulties in data collection and in- facturing parts, are still incomplete for available creased probability of errors during data access. To illustrate the formidable problems facing the and familiar metals that have been in use for some decades. With newer materials this is even more development of electronic databases of ceramic and composite properties, consider the state of of a problem because there is little material ex- metal machining databases. There are currently perience or history available from any source. thousands of metals and metal alloys, and thou- Some experts believe that the use of mathemati- sands of types of microstructure that can occur cal modeling of manufacturing processes will in each metal or alloy. Machining conditions can eventually allow the designer to construct a part- specific database as a new part is being designed. change with: microstructure of the metal; the This preliminary database could be updated as type of machining process; the type, size and the design moved to the prototype and produc- condition of tool; the depth, length, width, and speeds of cut; and the type and amount of lubri- tion phases and more knowledge of the mate- cant. Each of these parameters must be selected rial is gained. for each operation that must be performed on One esoteric problem in automating design a metal part. processes involves engineering knowledge of an intuitive or experiential nature. This human knowledge is difficult to translate into informa- zG’’Automated Manufacturing Research Facility,” National Bureau tion that can be transferred or used electronically. of Standards, December 1986. Zzcatherine A. Behringer, “Steering a Course With MAP,” Man- Examples: The ability to tell the temperature of ufacturing Engineering, September 1986, pp. 49-53. a molten metal by its color, or to ascertain the Ch. 5—Factors Affecting the Use of Advanced Materials ● 133 service life left to a cutting tool by the sound it expensive changes at once. Even though one of makes during the cut. To translate this kind of the main advantages of these new engineered know-how into electronic data, extremely ac- materials is the integration of design and manu- curate, sensitive, durable, and reliable sensors are facturing, it will not be possible to develop all required. This is particularly important consider- these technologies at once into a single, unified ing the flaw sensitivity of such a material as a ce- factory system. ramic, because a large number of parts can be As companies begin to automate, they will use ruined for a slight margin of error in the sensor. different combinations of automation technol- These materials cannot be reworked, and high ogies, depending on the priorities of the user in- scrap rates are a major factor contributing to the dustry. Table 5-3 illustrates how the reasons for high cost of ceramic parts. automating might differ among manufacturers. In the near term, automation based on the use Advanced Structural Materials of robotics to reduce labor costs may not be cost- Production effective if labor costs are a small pat-t of overall cost, or if part volumes are Iow.28 The automo- Several problems are likely to hamper the de- bile industry would desire to automate to save velopment of automated techniques for produc- materials and manufacturing process costs. tion of advanced materials that do not arise in the production of parts made from metal. Al- In the aircraft industry, techniques such as auto- though new structural materials offer the advan- mated tape laying to save the labor costs of hand tage of combining what would be several metal lay-up could be important. Where long design parts into a single structure, when an error oc- times mean a significant cost, such as in aircraft curs in production, cost-efficiency may be seri- design, automation is desirable in the form of ously threatened. Advanced materials cost more, mathematical modeling, expert systems for de- the structure cannot be reworked, and the whole signers, and systems for prototype production, composite or ceramic structure is lost where only such as mold design software. 29 Since the relia- a single metal part might have been with a metal bility and reproducibility of ceramic parts are of design. This is another reason why automated primary importance, automated processing tech- production of these advanced materials will re- quire extremely reliable and accurate sensors. 28S. Krolewski and T. Gutowski, “Effect of the Automation of Ad- Another problem is the large capital investment vanced Composite Fabrication Process on Part Cost, SAA4PE” Quar- tedy, October 1986. involved in automation. Full automation of de- zgNorman Kuchar, General Electric Co., personal Communica- sign through production requires many new and tion, Apr. 15, 1987. Table 5-3.—Reasons for Automating, and Appropriate Types of Automation Reason Types of automation Industry example Save labor costs: Robotics Automotive paint spraying, New processing technologies (i.e., filament joining winding, tape laying) Speed up production: New processing technologies: Auto body High-speed resin transfer molding, automated tape laying Increase part quality: Process controls, sensor technologies Ceramic auto engine parts Composite aircraft structures Shorten design times: Expert sytems Composite aircraft structures CAD Mathematical modeling Databases NOTE: Different manufacturing challenges require different types of automation solutions. SOURCE: Office of Technology Assessment, 1988. 134 ● Advanced Materials by Design niques and sensor technology would be used to the quality of sensors and a higher level of so- automate the manufacture of ceramics. The plas- phistication in equipment for forming advanced tics industry is turning to robots for several rea- materials. As we have seen and will see again in sons, among them the ability to integrate plastic the following chapters, processes such as auto- part manufacturing with “downstream” assem- mated tape laying of PMCs and near-net-shape bly operations, and flexibility to meet changing processes for ceramics will need precision form- production requirements.30 ing and monitoring equipment to begin to offer the needed reliability and cost savings. The one form of automation nearly all indus- tries require immediately involves better materi- Automation techniques that foster integrated als processing technologies possessing some de- design through promoting close cooperation be- gree of automation. This means an increase in tween designer and manufacturing engineer should be of highest priority. These would include ex- tensive design databases, automated processing 30 Robert V. Wilder, “Processors Take a Second, Harder Look at equipment and sensors for process information Robots, ” Modern Plastics, August 1987, p. 48. feedback. Chapter 6 Impacts of Materials Substitution on the Basic Metals Industries CONTENTS Page Findings ...... ● *,...... 137 Introduction...... 137 Historical Supply and Demand Factors for Steel and Aluminum ...... 138 supply...... ,. .**...... 138 Demand ...... * ● ...*...... 138 Interrelationships of Factors Affecting Supply and Demand ...... 139 The Relative Importance ofthe End Uses of Steel and Aluminum . ....,...... 139 Potential for Substitution in the Aircraft industry...... 141 Potential for Substitution in the Automobile Industry + ...... 144 Potential for Substitution in the Construction Industry ...... 147 High-Strength Concrete as a Substitute for Steel ...... 147 PMCs and Unreinforced Plastics as substitutes for Steel and Aluminum .. ...148 Potential for Substitution in the Container Industry. ., ...... 148 Development of New Industries and Changes in Existing Industries ...... 150 PMCs and Unreinforced Plastics industries ...... , ...... 150 Adhesives and Coating Industries...... 151 Weaving industry...... 151 Recycling Industry ...... 151 Figures Figure No. Page 6-1. Relationship Between Property Improvement and Weight Savings for Various Materials...... 143 6-2. Projected Savings in Aircraft Structural Weight Based on Selected Advanced Materials...... 143 6-3. Breakdown of Structural Materials Use in Two Alternative Designs of Commercial Transport Aircraft ...... 143 Tables . Table No. Page 6-1. U.S. Personal Consumption Expenditures for 1978 and 1983...... 139 6-2. Industries Using the Largest Amount of Steel, 1977 ...... 140 6-3. Industries Using the Largest Amount of Aluminum, 1977...... 140 64. Current and Proposed Use of Advanced Materials in Aerospace Structures ...... 142 6-5. Current and Proposed Use of Advanced Materials in Automobiles ...... 145 6-6. Cost Comparison of Using Normal and High-Strength Concrete for a 79-Story Building ...... 147 Chapter 6 Impacts of Materials Substitution on the Basic Metals Industries FINDINGS The U.S. steel and aluminum industries are cur- strength, low-alloy (HSLA) steels, aluminum-lith- rently undergoing a substantial restructuring proc- ium alloys (A1-Li), and rapidly solidified metal al- ess caused by large increases in world supply and loys. This makes the pace of substitution difficult decreases in per capita demand. Overall, mate- to predict. rials substitution has been only a minor factor An analysis of the end uses of these metals in- affecting the demand for these metals in the past dicates that substitution is likely to be most im- decade. However, the importance of substitution portant in four markets: aircraft, automobiles, con- by alternative materials is likely to be significantly struction, and containers. However, OTA finds greater in the next 10 to 20 years. that by far the greatest volume of metals will be The materials likely to have the greatest impact displaced by relatively low-performance materi- on the aluminum and steel industries are unrein- als, such as unreinforced plastics, sheet-molding forced plastics, polymer matrix composites (PMCs), compounds, and high-strength concrete, rather metal matrix composites (MMCs), and high-strength than by so-called advanced materials. concrete. Ceramics and ceramic matrix compos- As new materials are increasingly adopted, a ites (CMCs) are not expected to have a signifi- variety of secondary industries, such as adhesives, cant impact on steel or aluminum use in the next coatings, and weaving industries can be expected 20 years. to grow. The recyclability of the new materials The threat of substitution has stimulated im- could become a major factor affecting their use. provements in metals technology, e.g., high- INTRODUCTION With the development of new materials such This chapter outlines the effects of materials sub- as structural plastics and composites, engineers stitution on the U.S. aluminum and steel indus- now have many more options available for de- tries.1 An analysis of the major markets for these signing products. These new materials can offer two metals suggests that the most significant pos- performance advantages over such traditional ma- sibilities for substitution will be in aircraft, automo- terials as aluminum, steel, and concrete. How will biles, construction, and containers. In the follow- these new materials affect the traditional manu- ing section, materials substitution is considered facturing industries? What new industries will de- in the context of the many factors affecting sup- velop to support the use of these materials? The ply and demand within the basic metals industries. answers to these questions are important to an understanding of the factors that will influence ‘This chapter draws heavily on “Impacts of New Structural Ma- terials on Basic Metals Industries, ” by Steven R. lzatt, a contractor the evolution of U.S. manufacturing industries in report prepared for the Office of Technology Assessment, April the 1990s and beyond. 1987. 137 138 . Advanced Materials by Design HISTORICAL SUPPLY AND DEMAND FACTORS FOR STEEL AND ALUMINUM supply the large U.S. aluminum producers are diver- sifying into other materials, particularly ad- The supply of steel and aluminum worldwide vanced materials, for their future business. has grown substantially in recent years. Major fac- This factor tends to reduce U.S. primary over- tors that have affected the supply of steel and alu- capacity. minum in the United States are: the present U.S. ● Scrap recovery: Recycling of aluminum has overcapacity for steel and aluminum; the world- played a large part in its competitiveness. wide overcapacity for steel and aluminum; gov- However, large amounts of recovered alu- ernment ownership of foreign production facil- minum scrap also displace primary aluminum ities; volatile and depressed prices for steel and in several applications, aluminum; imports of steel and aluminum, the ● Shift to fabrication: There has been a shift growth of steel mini-mills in the United States; to supplying fabricated shapes rather than restructuring of the steel and aluminum indus- producing large units of steel (e.g., billets) tries; domestic scrap recovery of aluminum; and to be shaped by the purchaser. This has lit- a shift to fabricated shapes in aluminum. tle effect on total supply, but tends to favor ● Overcapacity: The main factor affecting the industry restructuring toward mini-mills and supply of steel and aluminum in the United away from integrated steel manufacturers. States is the current domestic and worldwide overcapacity. Demand ● Foreign government ownership: Abroad, The per capita demand for steel and aluminum many foreign governments own the national has been continuously decreasing in the United production of steel and aluminum. These States since its peak in the early 1970s.2 The fac- governments thereby control commodity tors that have tended to decrease demand are: price, and this can lead to overproduction. shifting consumption patterns, market saturation, ● Steel and aluminum prices: Prices are de- more efficient use of materials, and materials sub- pressed for these commodities; often they stitution. are highly variable. This can be as damaging as continuous low prices, since fluctuating ● Consumer preferences: Over the past 10 prices prevent long-term planning. years, there has been a shift in consumer ● Imports: Large volumes of foreign steel and spending away from durable goods to serv- aluminum are imported that are of good qual- ices (table 6-1 ). This switch in spending ity and of lower cost than can be found in preference is reflected in the decrease in the the United States. manufacturing sector’s contribution to the ● Mini-mills: These smaller, more efficient steel national income since the late 1960s (down mills are servicing some of the markets pre- to 22 percent in 1983 from 30 percent in viously held by the larger integrated steel 19653), and thus the decrease in per capita mills. This is very significant in product lines consumption of steel and aluminum. such as bar, rod, and wire, in which increased ● Market saturation: Analysts have observed supply from mini-mills has caused overca- that as a country matures past the rapid pacity in the integrated steel mills. growth phase of its industrial development, ● Restructuring: Both the aluminum and steel the majority of the primary industrial infra- industries have been undergoing restructur- structure has been built. This results in a de- ing; for instance, the U.S. steel industry is evolving with the growth of mini-mills. Within 2 Bureau of Economic Analysis, U.S. Department Of Commerce, individual steel and aluminum companies, World Almanac and Book of Facts, 1985, p. 152. restructuring is also taking place; for instance, 3 lbid. Ch. 6—Impacts of Materials Substitution on the Basic Metals Industries ● 139 Table 6-1 .—U.S. Personal Consumption Expenditures copper in high voltage transmission lines, and for 1978 and 1983 (billions of dollars) steel in beverage cans. 1978 1983 Expenditures [% of total Expenditures 1% of total Interrelationships of Factors Affecting Durable goods: Supply and Demand Motor vehicles & parts $ 95.7 7.1 $ 129.3 6.0 Domestic raw steel overcapacity is significantly Other ., . . 104.5 7.8 150.5 7.0 increased by several factors that are outside of Total durable the control of the steel industry and act to increase goods . 200,2 14.9 279.8 13.0 Nondurable goods. 528.2 39.2 801.7 37.2 supply. For instance, the factor of foreign gov- Services 618.0 45.9 1,074.4 49.8 ernment ownership of steel mills encourages for- Total personal consumption eign overproduction by mills not acting in re- expenditures $1,346.4 100.0 $2,155.9 100.0 sponse to market forces. Between 1978 and 1983, personal consumption of services increased by nearly 4 percent, while consumption of durable and nondurable goods decreased by The problem of domestic overcapacity is also about 2 percent. SOURCE: U.S. Department of Commerce, Bureau of Economic Analysis, The affected by worldwide overcapacity (this provides World Almanac and Book of Facts, 1985, p. 165. an increased incentive for importers to import to the United States). Industry restructuring (i.e., crease in the ratio of materials consumption growth of mini-mills, plant closings and bank- to per capita gross national product (GNP). ruptcy filings, joint venture and acquisition activity In the United States, this ratio peaked for steel in new materials) has occurred as a response to around 1950 and for aluminum in the mid- domestic and worldwide overcapacity. 4 1970s, and is now declining. Materials substitution and efficient use of ma- ● Efficient use of materials: The use of a mate- terials are strongly interrelated factors. The threat rial becomes more efficient when a higher of materials substitution has encouraged produc- performance per pound of material is achieved. ers to apply new technologies aimed at reducing Producers have devoted significant R&D re- the amount of material (and hence lowering the sources to develop steel and aluminum prod- cost) required to meet consumer needs. In the ucts and process technologies that require steel industry, this interrelationship is seen in the less steel or aluminum to satisfy a particular case of HSLA steel and coated steels that have market need. been developed in response to the threat by light- ● Materials substitution: When a new material weight materials such as unreinforced plastics, can offer a cost or performance advantage PMCs, and aluminum. over the current material in an established application, the new material will begin to Materials substitution significantly affects the displace the old in that application. For in- trend toward more efficient use of aluminum. For stance, aluminum showed rapid growth in instance, the increasing use of PMCs in aircraft the post World War II era as it replaced such applications has motivated the aluminum indus- traditional materials as wood in construction, try to provide lighter weight aluminum alloys and MMCs. To develop these advanced materials, the aluminum industry has undergone some restruc- 4E$ D. Lar~~n, M..j. Ross, and R*H. Williams, “Beyond the Era turing in the form of joint ventures and acqui- of Materials,” Scientific American, 254(6):37, June 1986. sitions. THE RELATIVE IMPORTANCE OF THE END USES OF STEEL AND ALUMINUM To understand the impacts of substitution on Tables 6-2 and 6-3 present industries classified the steel and aluminum industries, it is necessary in the most recent (1 977) complete U.S. input- to know the major markets for these materials. output tables, ranked in the order of highest use 75-792 0 - 88 - 4 140 ● Advanced Materials by Design Table 6-2.—industries Using the Largest Amount of Steel, 1977° (in miiiions of doiiars at producers’ prices) Use of Potential for substituting Industry classification steel Percent alternative materials 1. Motor vehicles and equipment ...... 9,471 15 High 2. Heating, plumbing, and fabricated structural metal products...... 5,700 9 Medium 3. Screw machine products and stampings ...... 5,318 8 Low 4. New construction ...... 4,567 7 Medium 5. Other fabricated metal products ...... 3,791 6 Medium 6. Construction and mining machinery ...... 2,880 5 Low 7. Metal containers ...... 2,556 4 High 8. General industrial machinery and equipment ...... 2,036 3 Low 9. 0ther transportation equipment ...... 1,993 3 Low 10. Farm and garden machinery ...... 1,432 2 Low c Total ...... 39,744 62% a lncludes all categories listed under the Primary Iron and Steel Manufacturing Classification in the 1977 Input-0utput Table:blast furnaces and steel mills, electrometal- Iurgical products, steel wire and related products, cold finishing of steel shapes, steel pipes and tubes, iron and steel foundries, iron and steel forgings, metal heat treating, and primary metal products, not elsewhere classified. bIncludes all categories listed under these Industry Classifications. CThere are 85 Industry classifications in the Input-output tables. The remaining 38 percent of the total U.S. steel output is consumed by the 75 industries not listed here. SOURCE: U.S. Department of Commerce, Bureau of Economic Analysis, The Detailed Input-Output Structure of the U.S. Economy, 1977, Volume 1: The Use and Make of Commodities by Industries, 1977, Washington, DC, 1984, pp. V-227. Table 6-3.—Industries Using the Largest Amount of Aluminum, 1977a (in millions of dollars at producers’ prices) Use of Potential for substituting Industry classification aluminum Percent alternative materials 1, Heating, plumbing, and fabricated structural metal products...... 1,950 11 Medium 2. Motor vehicles and equipment ...... 1,276 7 Medium 3. Metal containers ...... 1,166 7 High 4. Other fabricated metal products ...... 675 4 Medium 5. Aircraft and parts ...... 488 3 High 6. Screw machine parts and stampings ...... 465 3 Low 7. Service industry machines ...... 447 3 Low 8. Electric industrial equipment and apparatus ...... 338 2 Low 9. Other transportation equipment ...... 291 2 Medium 10. Engines and turbines ...... 289 2 Medium Total ...... 7,385 44%C alncludes the following categories under the primary Nonferrous Metals Manufacturing Classification in the 1977 Input-output Table: primary aluminum, aluminum rolling and drawing, and aluminum castings. bIncludes all categories listed under these Industry Classifications. CThere are 85 industry classifications in the Input-Output tables. The remaining 56 percent of the total U.S. aluminum output iS consumed by the 75 industries not listed here. SOURCE: U.S. Department of Commerce, Bureau of Economic Analysis, The Detailed Input-Output Structure of the U.S. Economy, 1977, Volume 1: The Use and Make of Commodities by Industries, 1977, Washington, DC, 1984, pp. V-227. of steel and aluminum to lowest. Each of these tainers, both of which are covered in this industries has been further evaluated as to the assessment. possibility for alternative materials substituting for Of the three largest steel-consuming industries steel or aluminum. The industries that were both with a medium potential of substitution, construc- major consumers of steel or aluminum and that tion is the only one covered in this chapter. The held a high potential for substitution were other two, screw machine products, stampings, evaluated. and other fabricated metal products, are not ana- Table 6-2 shows that of the top 10 industries lyzed here because these sectors cover such a that use steel, 5 are judged to have a high or diversity of types of products, each of limited dol- medium potential for substituting alternative ma- lar value on its own, that it is difficult to conduct terials. 5 The two industries of high potential are a reliable, in-depth analysis. motor vehicles and equipment, and metal con- Table 6-3 shows that of the top 10 industries 5 Izattt, op. cit., footnote 1, 1987. that use aluminum, seven have a high or medium Ch. 6—Impacts of Materials Substitution on the Basic Metals Industries . 141 potential for substituting alternative materials.6 turbines) the great diversity of products again pre- Three of these seven, which are treated in this cludes a reliable analysis. chapter, are aircraft and parts, motor vehicles and Thus, the four end uses judged to be of great- equipment, and metal containers. In the four in- est potential for substitution of new materials for dustries of medium possibility not analyzed here traditional metals are: aircraft, motor vehicles, (heating, plumbing, and fabricated structural construction, and containers. I n the category of metal products; other fabricated metal products; motor vehicles, the analysis is entirely of the au- other transportation equipment; and engines and tomobile industry. The analysis of the market for ——- containers includes not only beverage containers 6 Ibid. but food packaging as well. POTENTIAL FOR SUBSTITUTION IN THE AIRCRAFT INDUSTRY About 3 percent of the total aluminum output tion of aircraft. Missing this cyclic “window” and one percent of the total steel output (by dol- means that the material cannot be considered for Iar value) of the United States is consumed by use until a new generation of aircraft is developed. the aircraft industry. Even though the aircraft in- Each of the materials that are candidate substi- dustry is a minor market for pounds of aluminum tutes for aluminum is at a different point in de- shipped (approximately 5 percent of the trans- velopment. portation segment), it is an important one in terms Table 6-4 describes the possible use of advanced of the value of the aluminum shipped, as well as structural materials in aircraft applications. PMCs in terms of the U.S. balance of trade. The aircraft and MMCs have been or could be used in many market is performance-sensitive and is therefore Navy, Army, Air Force, National Aeronautics and willing to pay a premium for materials that in- Space Administration (NASA) or civilian commer- crease performance. This market acts as a devel- cial helicopters, aircraft, and space structures. To opment market for advanced materials that have date, the motivation for this substitution has a high initial cost. mainly been the opportunity to achieve weight Currently, aluminum accounts for 80 percent savings. As the properties of these materials im- of the structural weight of commercial aircraft.7 prove, their level of performance, and hence sub- In military aircraft, the percentage has varied from stitution, should also increase. More important, 65 percent in the 1960s (F-4) to 50 percent in the as more experience is gained with these materi- 1970s (F-15) and to 55 percent in the 1980s als, their associated costs could decrease, pro- (AV-8B).8 viding the major motivation for their use, espe- cially in commercial aircraft. Although PMCs, and less developed materials such as A1-Li alloys, MMCs, and rapidly solidified Reducing aircraft weight increases fuel effi- aluminum alloys, are all possible future con- ciency, which results in lower life-cycle costs. Sig- tenders for aircraft, it may be some time before nificant reductions in weight and increases in they actually displace traditional aircraft materi- strength are desired to meet fuel efficiency needs. als. The planning cycles of aircraft have a signifi- Industry experts have projected that substantial cant effect on materials substitution. A new ma- weight savings could be achieved along with prop- terial must be fully developed and qualified in erty improvements; for instance, a 30-percent time to be considered for use in the next genera- weight savings could be obtained with a 200- percent increase in fatigue strength by using 7Standard and Poor’s Industry Surveys, Metals-Nonferrous, Basic PMCs, and a 20-percent weight savings could ac- Analysis, July 10, 1986, pp. M76-M77. 8B.A. Wilcox, “influence of Advanced Materials on the Domes- crue with an 80-percent improvement in stiffness tic Minerals Industry, ” Materials and Society, 10(2):209, 1986. using MMCs (see figure 6-1). 142 ● Advanced Materials by Design Table 6-4.—Current and Proposed Use of Advanced Materials in Aerospace Structures System Structure Material Aircraft: Boeing 747 30°/0 of exposed surface area, 10/0 of structural weight, secondary fiberglass/epoxy structures Boeing 767 rudders, elevators, spoilers, ailerons ducting, stowage bins, parti- graphite/epoxy tions, lavatories, escape system parts, leading- and tailing-edge Kevlar/epoxy panels, cowl components, landing gear doors, fairings graphite-Kevlar/epoxy hybrid F-15 secondary structure, empennage parts graphite, boron/epoxy F-18 I0% by weight of total structure; primary structure, wing applica- graphite/epoxy tions, sandwich panel skins Beech Starship I 90% of aircraft; primary and secondary structures graphite/epoxy ATF 40% of total structure; fuselage substructure, inlet structure, in- graphite/polyimide or tegral tankage, bulkheads, fins graphite/bismaleimide or silicon carbide/aluminum Avtek 400 all primary and secondary structures Kevlar/epoxy Helicopters: AH-64 Apache secondary structures, primary structures, i.e., fuselage, rotor blades Kevlar/epoxy AV-8BV/STOL 26% of total weight; forward fuselage horizontal stabilizer, eleva- graphite/epoxy tors, rudder, overwing fairings, wing box skins and substructure, ailerons, flaps Boeing Vertol 234 center section of aft rotor assembly graphite-fiberglass/epoxy hybrid LHX, JVX airframes (results in acquisition and operational cost savings, graphite/epoxy, Kevlar/epoxy, weight savings, increased damage tolerance, etc.) fiberglass/epoxy, fiberglass/ polyimide Space shuttle fuselage, frame support struts, payload bay doors, purging ducts graphite-fiberglass/epoxy system, filament wound pressure vessels, nose cap, wing lead- hybrid, graphite/epoxy, ing edges, structural parts (increasing allowable temperature) Kevlar/epoxy, carbon/carbon, graphite/polyimide SOURCE: Steven R. Izatt. “lmpacts of New Structural Materials on Basic Metals Industries,” a contractor report prepared for the Office of Technology Assessment, April 1987. A note of caution is appropriate here on the and infiltrated with a resin system typically sells strong influence of fuel prices: If fuel prices do for approximately $40 per pound. The final cost not increase during the next 10 years, PMCs of the finished aircraft structure can be in the range could look less attractive compared to aluminum. of $100 to $400 per pound.10 Aircraft designers currently estimate that a pound Another important cost consideration in com- of weight saved is worth $100 over the life of the paring PMCs with metals is the significantly re- aircraft. Fuel prices as of August 1986 were about duced number of parts made possible by using 55 cents per gallon. It has been estimated that PMCs. For instance, in the Bell Helicopter Tex- it would take at least a factor of 2 increase in these tron, Inc./Boeing Vertol prototype PMC helicop- fuel prices to make PMCs look attractive to air- 9 ter body, the V-22 Osprey, there is a reduction craft buyers. in the number of airframe parts from 11,000 (alu- The important cost factors in considering ad- minum) to 1,530 (PMC). The number of fasteners vanced composites substitution for aluminum are is reduced from 86,000 to 7,000. The weight re- life-cycle costs, as noted above, and production duction is from 4,687 Ibs to 3,281 Ibs.11 costs. The major improvement in future costs Figure 6-2 shows the potential savings in air- should come from improved fabrication meth- craft structural weight forecast for the next quarter- ods. The contribution of the base material costs century. PMCs have the potential to give the to overall structure costs is relatively small. For largest weight reduction (30 to 40 percent) using instance, lower stiffness (30 Msi) PAN-based advanced fibers with modified epoxies and ther- graphite fibers generally sell for approximately $20 per pound. Prepreg tape made from these fibers 10 D. R. Tenney and H.B. Dexter, “Advances in Composites Tech- nology,” Materials and Society, 9(2):188, 1985. 9Bob Hammer, Boeing Aircraft Co., personal communication, 11 P. N. Lagasse, “The Role of Reinforcing Fibers in Composites, ” September 1987. Rubber World, May 1985, pp. 27-28. Ch. 6—Impacts of Materials Substitution on the Basic Metals Industries “ 143 Figure 6-1 .—Relationship Between Property moplastic matrices. A1-Li and powder metallurgy Improvement and Weight Savings for (P/M) alloys are expected to be introduced over Various Materials the next 5 to 10 years and offer a 10- to 15-percent I I 1 I r I 1 weight savings. Fatigue, PMCs I 30 The open question is whether aluminum (and its new alloys and composites) or PMCs, will be the material of choice in the next generation of commercial transport aircraft. Figure 6-3 shows Stiffness I 20 . MMCs two possible options (extensive use of new alu- minum technologies or extensive use of PMCs) Density for a hypothetical commercial transport built in Al-Li Powder metallurgy the 1990s. Due to recent improvements in resins, fibers, and processing technology for PMCs, and 10 to higher-than-projected costs for aluminum al- loys, the extensive PMC scenario currently looks very promising. However, the actual outcome is likely to lie in between these two scenarios. v 0 The use of A1-Li alloys or rapidly solidified tech- 20 40 60 80 100 200 300 nologies wouId cause the total amount of alumi- inure used in aircraft applications to decline, since Property improvement (percent) Compared with conventional materials, using advanced they are stronger per unit weight and/or less dense materials offers improvements in mechanical properties as than traditional aluminum alloys. Whichever sce- well as weight savings. nario (i. e., extensive use of PMCs or extensive SOURCE: P.R. Bridenbaugh, W.S. Cebulak, F.R. Billman, and G.H. Hildeman, “Par- use of new aluminum technologies as described ticulate Metallurgy in Rapid Solidification,” Light Metal Age, October in figure 6-3) occurs, the use of traditional alum i- 1985, p. 18. Figure 6-3.— Breakdown of Structural Materials Use in Two Alternative Designs of Commercial Transport Aircraft Figure 6.2.—Projected Savings in Aircraft Structural Boeing 767 1990-2000 Transport Baseline-Design Weight Based on Selected Advanced Materials 1% Misc. 40 “ 30 “ 11% Adv. ’aluminum 20 “ 10 “ 14% Steel aluminum / 12% Steel 1970 1980 1990 2000 2010 8% Titanium In the option featuring extensive use of advanced aluminum, 7150—Wrought aluminum alloy with zinc. the proportion of aluminum drops by 26 percent due to im- 2324—Wrought aluminum alloy with copper. proved structural efficiency. In the option featuring exten- sive use of advanced composites, the proportion of aluminum Advanced PMCs offer the greatest weight savings drops by 69 percent. Steel use remains virtually unchanged. SOURCE: D.R. Tenney and H.B. Dexter, “Advances in Composites Technology,” SOURCE: D.R Tenney and H.B. Dexter, “Advances in Composites Technology,” Materials and Society 9(2):186, 1985. Materia/s and Society 9(2):194, 1985. 144 ● Advanced Materials by Design num could decrease by between 26 and 69 per- in aircraft use of aluminum could mean a 1 to cent. Since aircraft and aircraft parts account for 2 percent decrease in the dollar value of total U.S. slightly less than 3 percent of total aluminum out- aluminum use by the year 2000. Note that steel put in the United States (table 6-3), this decrease use remains roughly constant in either scenario. POTENTIAL FOR SUBSTITUTION IN THE AUTOMOBILE INDUSTRY In evaluating substitution in the automobile in- market segmentation could mean that an increas- dustry, it is very important to understand that the ing number of models will be made in smaller automotive market is a commodity market that production volumes and model design could is extremely cost-sensitive, compared to the high change more frequently. performance-oriented aircraft market. Thus, it is The current trend toward market segmentation more difficult for new, high-performance (high- (more automotive models) could increase the cost) materials to penetrate the automotive mar- likelihood of substitution, since sheet molding ket, unless a significant cost savings can be compound (SMC) fabrication is competitive with realized. that of steel in low production volumes. The SMC During the past 20 years, three trends have had composite-skinned Fiero, for instance, is assem- major effects on the materials content of automo- bled at the rate of only 100,000 cars per year biles in the United States. From 1967 to 1976, gov- while the annual production rate for the steel- ernment standards encouraged automakers to bodied J-body cars (Cavalier, 2000 Sunbird, Firen- add structural weight to make autos safer. In 1975 za, Skyhawk, Cimarron) is 600,000. Most auto- the passage of the Energy Policy and Conserva- mobiles, because of the cost/benefit advantages tion Act (Public Law 94-1 63) required yearly in- for large production runs, still have steel body creases in the average fuel efficiency of each man- panels. ufacturer’s fleet of vehicles. This trend toward Major materials used in automobiles are mild fuel-efficient cars resulted in a substantial decrease steel, cast iron, HSLA steel, aluminum, unrein- in the average weight of an automobile. The ma- forced plastics, and so-called lower technology jority of this decrease can be attributed to down- PMCs. These latter two are now just beginning sizing and most of the remainder to use of high- to have a presence in the automotive market. The strength steels, and to a lesser extent, unreinforced ability to mold unreinforced plastics, and rein- plastics and aluminum as substitutes for mild steel forced plastics such as sheet molding compound, and iron.12 into aerodynamic shapes more easily than steel makes them strong contenders for increased sub- The most recent trend affecting the U.S. au- stitution. Stimulated by this threat, new types of tomobile industry has been the increase in inter- steel products—HSLA and coated steels—have national and domestic competition that has de- become available, providing the potential for con- veloped since about 1983. The industry has tinued dominance of steel in automotive appli- become increasingly cost- and quality-conscious cations. The trend toward the increased use of as U.S. consumers have turned increasingly to precoated steels has also reduced the potential imported vehicles. To compete in the low-growth substitution of current unreinforced plastics for automotive market, one of the strategies that au- steel sheets. tomakers have used to keep market share is to Table 6-5 lists examples of where lighter weight appeal to a broad range of consumers in differ- materials such as unreinforced plastics, fiberglass ent market niches. For this reason, the number and graphite-reinforced composites, aluminum, of major automotive nameplates is projected to and HSLA steel are substituting for iron and steel increase from 68 in 1984 to 77 in 1989.13 This in automobiles. These programs are a mixture of approved projects and projects that have been 121zaH op. cit., footnote 1, 1987. 13L. L&nard, “Aljtomotive Materials War Heats Up, ” Materials proposed. Most are secondary-structural or non- Engineering, October 1985, p. 29. structural applications such as fenders, door parts, Ch. 6—impacts of Materials Substitution on the Basic Metals Industries . 145 Table 6-5.—Current and Proposed Use of Advanced Materials in Automobiles Material/current use Material/proposed use Plastics: Plastics: b ● Ford Merkur XR4Ti: rear double spoiler (injection molded ● Buick LaSabre (1987): front fenders polycarbonate/acrylonitrile-butadiene-styren(PC/ABS)), ● Chrysler’s P-body cars (1987): bumper fasciasb b instrument panel and glove compartment, door handles, ● Buick Reatta (1987): front fenders b radiator grille, light frames, rear package tray and center ● Chrysler’s imported Q-coupes (1987): bumper fascias console a . Ford Ranger pickup (1988): plastic leaf springsb b ● Chrysler T-Vans (commercial version): plastic back but- ● Ford Tempo and Topaz (1988): alI plastic bumpers b terfly doors Plastics and composites: ● Ford Aerostar van (commercial version): plastic back but- ● b GM composite bodied cars (GM80 Program): Camaro and terfly doors Firebird replacement cars (1991 was target date, but has ● GM Fiero: roof, decklid (SMC); fascias, fenders and doors b d been cancelled) e (reaction-injection-molded urethane) ● Pontiac Fiero: space frame ● Ford Aerostar van: fuel tank, lamps, front and rear g ● Chrysler Genesis Program (1990s): composite chassis g bumpers’ ● Ford Alpha Program (1990s): composite chassis g Composites: ● GM-100 Program (1990s): composite chassis —Fiberglass c Aluminum: ● Chevrolet Corvette: body and transverse rear spring ● e Ford F-trucks and Econoline van (1987): aluminum drive ● GM Eank cars: leaf springs h i shafts ● Ford Aerostar hood, rear Iiftgate ● b GM 3200 series V-6 engine (1989 Camaro and Firebird): ● Chrysler Dakota pickup: leaf springs cylinder block, head, two inlet manifolds, oil pan, water — Fiberglass/graphite i c pump, and pistons ● Ford Econoline van: rear wheel drive shaft ● Audi (date unspecific@ entire body—formed jointly with Aluminum: Alcoa l h ● Chevrolet Corvette: driveshaft ● Chrysler Voyager, Caravan, and Daytona (1987): case for m ● Ford Aerostar van: driveshaft, one-piece wheels, rear axle manual transaxies carrier, oil pan, and enginemount bracketsi ● Chrysler LeBaron (1987): bumper reinforcements . Ford Ranger pickup.- one-piece aluminum wheeli ● GM Genll 2.8 L V-6 (1987): front cover, rocker cover, ● Chrysler 2.5 L balance-shaft engines: carriers for the generator mounting bracket and belt tensioner, cylinder balance shaftsk heads, and intake manifoldk - i ● Chevrolet Corvette. cylinder heads on 5.7 L V-8 ● GM Genll 2.0 L 4 cylinder(1987): front cover, rocker cover, . Dodge Dakota pickup.- intake manifold on 3.9 L V-6 elbow on remote air cleaner assembly, air cleaner hous- engine ing, and cylinder headsk ● Lincoln Town Car: inner and outer hood panels and hinge ● AMC 4.0 L. 6-cylinderJeep engine (1987): engine covers, reinforcements” rocker coversk ● Stainless steel: Ford 4.9 L inline 6 cylinder for light trucks (1987): intake plenum and branch manifold individual runnersk ● 0ldsmobile Toronado: exhaust system from manifold to ● tailpipe i Chrysler Turbo II 4 cylinder for Dodge Daytona Shelby (1987): intercooler and dual toned intake manifoldk ● Cadillac: exhaust manifolds i ● Chrysler 3.O L V-6 (import, 1987): cylinder heads, rocker ● Ford Taurus/Sable: exhaust pipes and supports arms, and three-piece intake manifolds High-strength steel: ● Oldsmobile Buick LaSabre and Trofero (T-Type), Ponti- ● Current or potential use: 35-45 ksi—outer and inner body ac Bonneville, Chevrolet Celebrity and Cavalier Z24 components such as door, hood, fender, deck, quarter, (1987): wheels k floor, pan, and dash panel; 50-60 ksi—rocker panel (side ● Ford Econoline van (1987): driveshaft k sill), front and rear rails, wheel, frame, control arm, brack- ● Cadillac Allante (1987): stamped body panels—six inner et, bumper and reinforcement, seat track, and cross and outer hood, deck lid and removable roof panelsk member; 70-80 ksi—door beam, bumper reinforcement, ● Ford 4-wheel-drive Tempo and Topaz (1987): transfer j and bracket casek Stainless steel: ● Chrysler front-wheel-drive car/van lines: exhaust systems m SOURCES: aDesign News, Dec. 2, 1985, p. 30. h American Metal Market, Jan. 26, 1986, p. 5. bAmerican Metal Market, Aug. 21, 1986, p. 8. iMaterials Engineering, October 1985, pp. 28-35. j CPopular Science, July 1985, pp. 50-53. Chemtech, September 1985, p. 556. dChemical Business, June 1988, pp. 10-13. kAmerican Metal Market, Aug. 14, 1986, p. 1. l elron Age, Dec. 20, 1985. Light Metal Age, December 1985, pp. 16-17. fAmerican Metal Market/Metal Working News, May 19, 1986, p. 1. mAmerjcan Metal Market/Metal Working News, July 21, 1986 gAutomotive News, 1985, p, 1. nMetal Progress, May 1986, p. 44. 146 ● Advanced Materials by Design grilles, and interior panels. Structural applications, Substitution of lightweight materials in automo- using glass and graphite fiber-reinforced matrices, biles is at a plateau; most of the easier substitu- include leaf springs and drive shafts. tions have been made, and only those requiring For the automakers, using unreinforced plas- substantial improvements in the technology of alternative materials remain.19 When the newer tics and fiberglass composites trims tooling costs unreinforced plastics and PMCs are improved to (tooling for a steel hood requires 52 weeks; for 14 the point where they can be used in more de- a fiberglass composite hood, 39 weeks ) and al- manding applications and can be produced eco- lows them to respond quickly to market and com- nomically, materials substitution can occur at a petitive changes because of the cost advantages faster rate. of unreinforced plastics and fiberglass compos- ites at low production volumes. Using these ma- Early estimates by automakers suggested that terials also provides increased part durability and the usage of lightweight materials would increase decreases the number of necessary parts (e.g., significantly by 1991.2021 Such a change in usage the space frame used in the Fiero has 300 struc- would depend heavily on: 1 ) the concurrent de- tural steel parts; by using PMCs, this total could velopment of lightweight materials technologies be reduced to 30, and 4,000 welds could be elim- and competitive costs, 2) maintenance of the cur- inated).15 rent automotive industry trend toward increased New coating technologies, mostly of zincrome- competitiveness, and 3) the acceptance of new tal, have improved the corrosion resistance of steel materials by car buyers, automakers, and sup- and helped to keep it competitive with noncor- pliers to the automotive industry. roding reinforced plastics. One company has de- However, automakers now feel that these early veloped an alumina-ceramic coating derived from estimates may have been too optimistic by about aerospace products (blades, vanes, and other gas five years. A plausible scenario might be that com- turbine engine hardware) that can be used to pro- posites could displace 3 percent of automotive tect automobile fasteners from corrosion.16 HSLA steel use by the late 1990s.22 this would mean steels offer weight savings over traditional carbon a decrease in total steel use in the United States steels due to their higher strength. The use of of only 0.4 percent by dollar value. HSLA steels in automobiles has increased from Because aluminum is a lightweight material, 5 percent in 1975 to 14 percent in 1985 and is there is not as much driving force for substitu- expected to rise above 20 percent by early in the 17 tion by PMCs. However, if PMCs offer other ad- 1990s. Aluminum is generally not considered vantages over aluminum, such as lower cost or cost-competitive with either HSLA or mild steel, greater ease of manufacturing, PMCs may begin but it is almost cost-competitive with cast iron. to substitute for aluminum in automobiles. A recent joint venture by an aluminum company and an auto manufacturer produced a prototype aluminum car body that weighed 46.8 percent less than a comparable steel prototype and per- formed as well as a comparable steel body.18 191zatt, op. cit., footnote 1, 1987. “’’Fiber-Glass Composites Aim at Autos’ Structural Parts, ” /ron ZOH ,E. Chandler, “Material Trends at Mazda Motor Corp., ” Metal Age, Dec. 20, 1985, p. 16. Progress, May 1986, pp. 52-58. I Slbid. 21A. Wrigley, “Alloys and New Materials – Auto Industry in Ma- lbD. F. Baxter, “Developments in Coated Steels,” Meta/ Progress, terials Flux: Alloys Outlook Still Optimistic, ” American Meta/ Mar- May 1986, pp. 31-34. ket, Feb. 24, 1986, pp. 7, 10. 38 1 TLar~on et al., op. cit., footnote 4, p. ” Zzch. 7 presents a scenario of 500,000 PMC automobiles per year 1 8’’ Aluminum Car Bodies in the Future, ” Light Meta/ Age, De- in production by the late 1990s. This would cause a drop in au- cember 1985, pp. 16-17. tomotive steel use of 250,000 tons or about 3 percent. Ch. 6—impacts of Materials Substitution on the Basic Metals Industries c 147 POTENTIAL FOR SUBSTITUTION IN THE CONSTRUCTION INDUSTRY New construction represents the fourth largest An example presented in table 6-6 shows that U.S. market for steel (about 7 percent of total steel total cost of 33 steel-reinforced concrete columns output as shown in table 6-2). New construction for a 79-story building would be about $3.8 mil- consumes less than 1 percent of the total U.S. lion for high-strength concrete, compared to ap- aluminum output. proximately $7.7 million for normal-strength concrete. High= Strength Concrete as a The major uses for high-strength concrete have Substitute for Steel been for columns of high rise structures and pre- cast, prestressed bridge girders, although there The development and increasing use of high- have also been some special applications in dams, strength concrete represents a market challenge grandstand roofs, piles for marine foundations, to both steel structural shapes and steel rein- decks of dock structures, industrial manufactur- forcing bars. Because of the high compressive 24 ing applications, and bank vaults. strengths of high-strength concrete (defined to be in the range of 84 to 110 megapascals (MPa)) this Significant improvements in the properties of material can be used in structural applications that high-strength concrete can occur over the next would otherwise use structural steel members. 20 years. Research is underway on fibers for a High-strength concrete has comparatively low new generation of fiber-reinforced high-strength tensile strength, low stiffness, and low toughness, 24 lbid,, pp. 403-404. although its toughness is higher than that of lower strength concrete. In addition, it requires less rein- forcement than ordinary concrete, thus reduc- ing the need for reinforcing bars. Table 6-6.—Cost Comparison of Using Normal and High-Strength Concrete for a 79-Story Building High-strength concrete, which has been under development for several years, has now entered Compressive strength a high-growth phase. Use of high-strength con- High a Normal b (up to 12,000 psi) (4,000 psi) crete could increase at a much more rapid rate Materials (84 MPa) (28 MPa) over the next 5 to 10 years as those various high- Cost per 25 x 25 ft. panel strength concretes under laboratory testing are Concrete ...... $45,035 $88,836 used in actual construction. Forms...... 35,729 54,606 Longitudinal steel ...... 34,449 87,161 The major driving force for using high-strength Spirals ...... 1,441 1,930 concrete is its relatively greater ratio of strength Total ...... $116,654 $232,533 Total cost for 33 columns . . $3,849,582 $7,673,589 to unit cost which makes it the most economical a With the high.strerlgth concrete, column dimensions were kept constant and means of carrying compressive forces. Because were calculated so that the lowest story columns can be made with a 12,000 psi (84 MPa) concrete and 1 percent longitudinal steel. The dimensions of the compressive strength is also higher per unit weight column and the percentage of the longitudinal steel was maintained constant and volume, less massive structural members can for all 79 stories. The top 29 floors were designed with 4,000 psi (28 MPa), the next 31 floors with 9,000 psi (63 MPa), while the bottom 19 floors were designed be used compared to lower strength concrete. with 12,000 psi (84 MPa). b For normal strength concrete, all floors had concrete with a Compressive Cost studies have been conducted that show the strength of 4,000 psi (28 MPa). However, to maintain a 1 percent ratio of the longitudinal steel, the dimensions of the designed circular columns were in- advantage of using high-strength concrete with creased from 1,400 mm at the top to 2,950 mm for the bottom story, 23 a minimum of steel reinforcement. SOURCE: S.P. Shah, P. Zia, and D. Johnston, “Economic Consideration for Using High Strength Concrete in High Rise Buildings, ” a study prepared for Z3KI Committee 363, “State of the Art Report on High Strength Elborg Technology Co., December 1983 As presented in: S.P. Shah and S.H. Ahmad, “Structural Properties of High Strength Concrete and Concrete,” ACI 363 R-84, ACI Journal, July-August 1984, pp. Its Implications for Precast Prestressed Concrete,” Prestressed Con- 366-367. crete Institute Journal 30(6):109-110, November-December 1985. 148 c Advanced Materials by Design concretes. As this technical improvement occurs, highly fragmented nature of the construction in- construction markets originally dominated by dustry tends to retard their widespread adoption. steel could become potential markets for the new However, in the Iongterm, PMCs may find limited concrete. Assuming from the example in table use in specialized applications such as nonmetal- 6-6 that 60 percent less steel (by dollar value) is lic, nonmagnetic structures, bridges, and manu- needed to reinforce high-strength concrete build- factured housing (see ch. 3). ing columns, and that this figure could be used Unlike PMCs, unreinforced plastics have the as an estimate for the decrease due to substitu- potential to displace significant amounts of metal tion in total construction use of steel (7 percent (mainly aluminum) in the construction industry. by dollar value), this would mean a decline in Sales of unreinforced plastics to the construction total steel use by a dollar value of about 4 percent market rose from 2,354 million metric tons in 1974 to 4,212 metric tons in 1984, an increase of nearly PMCs and Unreinforced Plastics as 80 percent. Sales are expected to grow an addi- Substitutes for Steel and Aluminum tional 25 percent by 1990, to 5,265 million met- ric tons.25 These figures highlight the overall trend PMCs are highly unlikely to substitute for steel in the construction market toward using unrein- or aluminum in the construction industry to a sig- forced plastics. Unreinforced plastics compete nificant degree in the foreseeable future. The cost directly with aluminum in those applications that of PMCs is prohibitive compared to other con- require little load bearing capability such as win- struction materials. Steel, cement, and concrete dow frames, doors, and screens. sell for dollars per ton, whereas PMCs that have matured in their processing technology (e.g., fiber- glass/epoxy) sell for dollars per pound. As with z5j.A. schlegel, Barrier Plastics: The Impact of Emerging Technol- high-strength concrete, the general lack of famili- ogy, AMA Management Briefing, American Management Associa- arity with the properties of PMCs as well as the tion, 1985, p. 43. POTENTIAL FOR SUBSTITUTION IN THE CONTAINER INDUSTRY Containers and packaging constitute the third the mature phase of their technology develop- largest market segment for aluminum (see table ment. In contrast, unreinforced plastics for the 6-3) and the seventh largest market segment for soft drink market are still relatively new technol- steel (see table 6-2). The large majority of rigid ogies. To compete in the soft drink market, plas- containers are used for the primary packaging of tic containers are required to have barrier prop- beer, food, and soft drinks. Total rigid container erties to protect the container contents against shipments increased at an average annual rate permeation of gases (e.g., oxygen, carbon dioxide, of 1.4 percent during the 1974-84 period; this rep- and water vapor), degradation due to light (espe- resents 19.6 billion containers.26 However, be- cially ultraviolet light), aroma/odor changes, and cause the food and beverage segments of the con- effects of organic chemicals and hydrocarbons. tainer market have reached maturity, the growth Aluminum, steel, and glass provide an “ultimate for any one material must come at the expense barrier” against these possibilities. of another. There are a number of driving forces for the The container market represents a competition adoption of unreinforced plastics in those mar- among several materials: aluminum, steel, unrein- kets currently served by metal containers. These forced plastics, and glass. With respect to bever- include potential for processing savings; shipment age containers, both aluminum and steel are in and storage savings (aseptic products made of plastic can be shipped and stored without refrig- ZGU.S. Department of Commerce, 1985 U. S. /ndustria/ Out/ook, eration); consumer preference for convenience January, 1985, Washington, DC, p. 6-1. packaging that allows a container to be used eas- Ch. 6—Impacts of Materials Substitution on the Basic Metals Industries “ 149 ily, e.g., taken from freezer to microwave (or con- ventional oven) and thence to the table. The fact that some barrier plastics can be recycled may also be a driving force for adopting unreinforced plastics for containers and packaging. It is esti- mated that 100 million pounds, or about 19 per- cent of the total annual polyethyleneterephtha- late (PET) production of 535 million pounds was recycled in 1984.27 Over the short term (2 to 5 years), aluminum couId face a continually increasing competitive threat from unreinforced plastics in the single- serve soft drink market. Unreinforced plastics would not substitute directly for aluminum in the short term, but they could continue to displace glass in half-liter sizes and hence offer consumers a choice of the plastic container as an alternative to the 12-ounce can. These competitive forces do not constitute substitution of unreinforced plas- tics for aluminum; rather, this situation would hold the demand for cans under what it normally would have been, thereby decreasing the over- all growth of the market for aluminum. Photo courtesy of Processed Plastics Co. In the longer term (5 to 10 years), the recycla- Plastalloy bench made of 100°/0 recycled plastic. bility of unreinforced plastics versus aluminum will be an important consideration, as will the rela- ket could increase to about 10 to 15 percent over tive weight of the two materials since weight the next 15 years.28 affects processing, shipping, and storage costs. Although the current plastic material, PET, is The current trend toward alternative containers recyclable (the recycled product goes into con- could continue to become very significant in the verting textile fiber-fill, strapping, plastic lumber, 3-to lo-year time frame, and unreinforced plas- and polyols for other polymer manufacture), this tics could be the dominant materials for food cans. is not the material that would substitute directly The substitution of unreinforced plastics for alu- for the aluminum beverage can. The plastic or minum in beverage containers could begin in a plastic composite can (i.e., a can made of com- significant way in the 3- to 10-year time frame bined layers of plastic with special barrier prop- and become a potentially serious competitor to erties) could be made of more than one type of aluminum in the 5- to 15-year time frame. plastic and hence could make recycling much Assuming that in 15 years unreinforced plas- more difficult. tics will capture half of all container markets for Since the technology for aluminum food cans aluminum (currently 7 percent by dollar value of is still in a beginning stage, there could be signifi- all aluminum use), total U.S. aluminum use could cant advances over the next 10 to 20 years that decrease by 3 to 4 percent by dollar value. Total could increase the aluminum can’s competitive container use of steel is currently 4 percent of position. Aluminum’s share of the food can mar- the total steel output by dollar value, and use of steel is likely to decrease significantly as both alu- minum and unreinforced plastics substitute for 17 I x)6 Beverage incjustry Annual Manual, produced by Naga- steel in containers. zines for Industry, Harcourt, Brace, )ovanovich Publications, Sep- tember 1986, p. 62. 28 Alcoa 1985 Annual report. 150 ● Advanced Materials by Design DEVELOPMENT OF NEW INDUSTRIES AND CHANGES IN EXISTING INDUSTRIES Substitution has the potential to become a sig- In addition to diversifying into nonmetals busi- nificant force over the next 20 years as new ma- nesses, the aluminum industry is pursuing oppor- terials technologies are commercialized. This tunities in Al-Li alloys, MMCs, and rapidly solidi- assessment, however, is contingent on the abil- fied technology. Currently, for instance, four ity of these materials to overcome key technical aluminum firms either have or are anticipating and economic barriers that are identified in this having plants to produce Al-Li alloys. Because Al- report. Li alloys are sold to the same markets as tradi- tional aluminum, aluminum firms have a strong To the present time, there have been two ef- marketing advantage over new firms. The wide- fects of materials substitution on the steel and alu- spread use of Al-Li alloys could also cause sig- minum industries: an increase in R&D aimed spe- nificant modifications to the end users of these cifically at efforts to develop new materials; and new alloys. inter- and intra-industry joint ventures aimed at new product development in traditional as well Because lithium is poisonous even at very low as advanced materials. concentrations, special precautions must be taken to segregate Al-Li scrap from other aluminum lntra-industry cooperative efforts in the steel in- scrap that would be recycled by usual methods. dustry have centered on developing a new di- Because of the special precautions that must be rect sheet casting process and on electrogalvaniz- taken, specialized machine shops and recycling ing (EG) lines. These efforts are being undertaken centers could be required. jointly (primarily due to a lack of individual com- pany resources) as responses to a recognized ma- Alcoa is developing its aramid-reinforced alu- terials substitution threat. The installation of EG minum MMC (ARALL) to be used on commercial lines is in direct response to more stringent auto- aircraft and Dural Aluminum Composites Corp. maker requirements concerning corrosion and (a wholly owned subsidiary of Alcan Aluminum) surface quality, and represent the steelmaker’ brought 2 to 3 million pounds of capacity for sili- strategy to ward off competition from other me- con carbide-reinforced aluminum MMC on line tals and unreinforced plastics.29 The commitment in February 1988.31 to this strategy can be seen by the fact that five Significant substitution of advanced materials new lines came on stream in 1986 representing for aluminum and steel in the various markets a $500 million investment, and that there are 13 mentioned above could occur in roughly 10 to coatings for automotive sheet steel now being 30 30 years after substitution has begun, based on produced. past experience in these or similar industries. As There have been several joint ventures between these materials begin to substitute for aluminum aluminum user and supplier industries including and steel, new industries will be formed. one to develop and make high-performance plas- tic containers for the U.S. food industry, and one PMCs and Unreinforced Plastics with a foreign automaker for the development Industries of a prototype aluminum auto body and frame. These efforts are direct responses by the alumi- The PMC and unreinforced plastics industries num industry to the materials substitution threat have already established definite market seg- and the potential for aluminum to substitute for ments. Significant growth in sales of PMCs is ex- steel in automobiles. pected. Charles H. Kline& Co. estimates that the Zgwrigley, op. cit., footnote 21 ~ 1986. JOT. Cirisafulli, “Industry Striving for Better Steels to Battle Com- 31 ~JAlcan~5 Dural (Jnit to Expand Aluminum COnlpOsite CaPac- petition in Auto Market, ” American Metal Market, Mar. 11, 1986, ity, ” Petiormance Materja/s (Washington, DC: McGraw-Hill, jan. p. 3. 11, 1988), p. 2. Ch. 6—Irnpacts of Materials Substitution on the Basic Metals Industries ● 157 demand for PMCs in automobiles could rise from approximately 700,000 pounds in 1984 to 1.4 mil- lion pounds in 1995, and the demand for PMCs in aircraft/aerospace applications could increase from approximately 8.6 million pounds in 1984 to nearly 75 million pounds in 1995.32 This study projects that sales of PMCs will reach approxi- mately $5.5 billion by the year 2000.33 Overall, about 3 percent of total U.S. resin production is used in some type of composite. 34 Adhesives and Coating Industries increased growth in PMC materials could also increase the demand for specialty adhesives and Photo courtesy of AVCO Specialty Materials coatings, C. H. Kline & Co. forecasts that demand Flexible interweaving of, SiC-reinforced Al to be used for specialty adhesives and coatings for PMCs in investment casting process. could grow from $35 million in 1985 to $110 mil- lion in 1995, an average rate of growth of 12.1 percent per year.35 Liquid, paste, and film adhe- sives together accounted for 85 percent of the total dollar value of adhesives markets in 1985. The current adhesives and coatings industry structure is fairly concentrated, with American Cyanamid, Ashland, 3M, and Morton-Thiokol to- gether controlling about 60 percent of the mar- ket. However, the industry may become less con- centrated over the long term as other suppliers strive to increase their presence. Photo courtesy of Polymer Products, Inc Weaving Industry Integrated benches and table made from PMCs using three-dimensional braided fibers 100°/0 recycled plastics. or woven fabrics offer a significant advantage over unidirectional tape or two-dimensional prepreg, 10 to 20 years because of expected increases in i n that there is less tendency for the PMC struc- the use of braided preforms for PMCs and MMCs, ture to delaminate under loading. Although the especially in the aircraft industry. number of companies now producing these braided structures is small, their numbers could Recycling Industry ‘ grow as the demand for braided PMCs increases. This industry could grow quickly over the next Disposal of unreinforced plastics and PMCs cur- rently pose large problems; several States now have legislation pending to ban nondegradable 3$, Brown, c. H. Eckert, and C. H. KI i ne, ‘‘Advanced Polymer plastic products such as six-pack rings, fast food Composites: Five Keys to Success, ” presented to the Suppliers of packaging, and egg cartons. 36 However, no via- Advanced Composite Materials Association (SACMA), in Anaheim, CA, Mar. 21, 1985, ble technologies currently exist for degradable 33 Ibid plastics food packaging. 37 More and more, com- jqNOrman Fishman, SRI International, personal Communication, May 1988, 36 Robert Leaversuch, “Industry Weighs Need to Make Polymers “’’Adhesives, Coatings Makers Banking on Composites Growth, ” Degradable, ” Modern Plastics, August 1987, p. 53. Chemical Marketing Reporter, July 21, 1986, pp. 7, 26, 371 bid. 152 ● Advanced Materials by Design panics are beginning to look toward recyclable by steel could have adverse effects on the recy- plastics. The fact that thermoses such as epoxies cling industry, especially in the case of automo- are not recyclable may make them obsolete, biles, in that scrap steel is reused in electric according to some industry experts .38 Reinforced furnaces. or layered plastics may prove to be a major prob- The third change could be the emergence of lem to recycling efforts, sufficient to inhibit their specialty recycling facilities that can handle poi- use, according to some recycling industry repre- 39 sonous materials (e.g., aluminum alloys contain- sentatives. ing lithium) or difficult-to-recycle materials (e.g., Three changes could occur in the recycling in- unreinforced plastics, MMCs, or PMCs). There dustry. First, since recycling of aluminum cans currently exists no satisfactory commercial proc- has become a significant activity over the past 15 ess to recycle these materials. However, recycling years, the aluminum recycling industry could be processes are now under development, and it is seriously affected as the use of aluminum in bever- possible that commercially viable processes could age cans decreases. It is possible, however, that be put into use as the growth of these materials the recyclability of aluminum could give the metal industries proceeds. a significant advantage over competing materi- In summary, the substitution of new materials als that cannot be easily recycled, e.g., unrein- for aluminum and steel in major market segments forced plastics and PMCs. could create significant new industries and modifi- The second change could occur in the steel cations to existing industries over the next two recycling industry. The increasing use of non- decades. Secondary industries such as the adhe- recyclable materials in uses traditionally served sives, coatings, weaving, and recycling industries could also be affected as new materials are in- creasingly adopted. The recyclability of the new ~BRobe~ Leaversuch, “Practicality is the Key in New Strategies for Recycling,” A40dern P/asfics, August 1987, p. 67. materials could become a major factor affecting Jglbid. their use. Chapter 7 Case Study: Polymer Matrix Composites in Automobiles CONTENTS . Page Figure No. Page Findings..,...... 155 7-10. Relationship Between Performance and Introduction ...... 00 156 Fabrication for Composites ...... 166 Background ...... 157 7-11. Sheet Molding Compound Material Polymer Matrix Composite Materials ...... l60 Preparation and Component Performance Criteria ...... 161 Fabrication ...... 166 Fatigue ...... 161 7-12 Typical SMC Production Aerostar Energy Absorption ...... 162 Tailgate ...... 166 Stiffness and Dam ping...... 164 7-13 Typical SMC Production Aerostar Potential ManufacturingTechiques .. ..,....165 Hood...... 167 ...... 165 7-14 Typical SMC Truck Cab...... 167 High-Speed Resin Transfer Molding...... 169 7-15 Prototype Escort Composite Rear Floor Filament Winding...... 171 Pan ...... 168 Impact on Production Methods ...... 173 7-16 Thermoplastic Compression Molding . . . . 169 Manufacturing Approach ...... 173 7-17 High-Speed Resin Transfer Molding . . . . . 170 Assembly Operation Impact ...... 176 7-18 Squeeze Molding and Resin Transfer Labor impact ...... 177 Molding ...... 171 Impact on Support Industries...... 178 7-19. Filament Winding Process ...... 172 Material Suppliers, Molders and Fabricators .178 7-20. Typical Assembly of (a) Steel Underbody Steel Industry ...,...... * 179 and (b) Underbody, Bodyside Assemblies Repair Service Requirements ...... 180 Etc. into the Completed Steel Body PMC Vehicle/Component Recycling ...... l80 Shell ...... 174 Potential Effects of Governmental Regulations .181 7-21. Typical Assembly of Composite Bodyside Health Safeguards ...... 181 Panel by Adhesive Bonding of lnner and Recyclability ...... 181 Outer SMC Molded Panels ...... 175 Crash Regulations ...... 182 7-22. Typical One-Piece Composite Bodyside Fuel Economy Standards ...... 182 Panel With Foam Core Molded by Technology Development Areas ...... 182 HSRTM ...... 175 Compression Molding ...... 182 7-23. Typical Body Construction Assembly for High-Speed Resin Transfer Molding...... 182 Composite Body Shell ...... 176 Fiber Technology ...... + ...... 183 7-24 Typical Body Construction Assembly Joining ● ....** ● *...... **...... 183 Using Two Major Composite Moldings . . 177 Requirements ...... 183 7-25 Effect of Composite Use on Steel Use in ...... 183 Automobiles ...... 179 Summary ...... 183 Tables Table No. Page Figures 7-l, Major Weight Savings of GrFRP Over Figure No. Page Steel in Ford ’’Graphite LTD’’ Vehicle 7-1. Steel Body Shell Structure ...... 157 Prototype ...... 159 7-2. Ford GrFRP Vehicle ...... 158 7-2. Crash Energy Absorption Associated With 7-3. Ford GrFRP Vehicle With the Composite Fracture of Composites Compared Components Shown...... 159 With Steel ...... 159 7-4. Typical Fatigue Curves for (Unidirectional 7-3. Typical Stiffness of Selected GIFRP ...... 161 Composites ...... 165 7.5. Typical Fatigue Curve for SMC...... 162 7-4. Typical Body Construction System: Steel 74. Tensile Stress-Strain Curves for Steel and Panels ...... 174 Aluminum ...... 162 7-5. Compression Molded Structural Panels ..175 7-7, Tensile Stress-Strain Curves for Graphite 7-6. Preform Fabrication Sequence ...... 175 Fiber Composite, Kevlar Fiber Composite, 7-7. Foam Core Fabrication Sequence ...... 175 and Glass Fiber Composite ...... 163 7-8. HSRTM Molded Structural Panels...... 176 7-8. Energy Dissipation Mechanism in 7-9. Body Construction Assembly Sequence ..176 Ceramics ...... 163 7-10. Effect of Composites on Body 7-9. Different Collapse Mechanisms in Metal Complexity ...... 177 and Composite Tubes ...... 164 7-11. Automotive Steel Usage ...... 179 Chapter 7 Case Study: Polymer Matrix Composites in Automobiles FINDINGS The increased use of advanced structural ma- filament winding, At this time, no method can terials may have significant impacts on basic man- satisfy all of the requirements for production; ufacturing industries. The automotive industry however, resin transfer molding seems the most provides an excellent example, since it is widely promising. viewed as being the industry in which the great- Clearly, the large-scale adoption of PMC con- est volume of advanced composite materials, par- struction for automobile structures would have ticularly polymer matrix composites (PMCs), will a major impact on fabrication, assembly, and the be used in the future. Motivations for using PMCs supply network. The industry infrastructure of include weight reduction for better fuel efficiency, today would completely change; e.g., the multi- improved ride quality, and corrosion resistance. tude of metal-forming presses would be replaced Extensive use of composites in automobile body by a much smaller number of molding units, mul- structures would have important impacts on tiple welding machines would be replaced by a methods of fabrication, satellite industry restruc- limited number of adhesive bonding fixtures, and turing, and creation of new industries such as the assembly sequence would be modified to recycling. reflect the tremendous reduction in parts. This The application of advanced materials to au- complete revamping of the stamping and body tomotive structures will require: 1 ) clear evidence construction faciIities wouId clearly entail a rev- of the performance capabilities of the PMC struc- olution (albeit at an evolutionary pace) in the in- tures, including long-term effects; 2) the devel- dustry. However, there would probably not be opment of high-speed, reliable manufacturing a significant impact on the size of the overall la- and assembly processes with associated quality bor force or the skill levels required. control; and 3) evidence of economic incentives Extensive use of PMCs by the automotive in- (which will be sensitively dependent on the man- dustry would necessitate the development of ufacturing processes). completely new supply industries geared to pro- The three performance criteria applicable to a viding inexpensive structures. It is anticipated that new material for use in automotive structural ap- such developments would take place through plications are fatigue (durability), energy absorp- two mechanisms. First, current automotive sup- tion (in a crash), and ride quality in terms of noise, pliers, particularly those with plastics expertise, vibration, and harshness (generally related to ma- would unquestionably expand and/or diversify terial stiffness). There is emerging evidence from into PMCs to maintain and possibly increase their both fundamental research data and field experi- current level of business. Second, the currently ence that glass fiber-reinforced PMCs can be de- fragmented PMCs industry, together with raw ma- signed to fulfill these criteria. terial suppliers, would generate new integrated companies with the required supply capability. At present, the successful application of PMCs In addition, completely new industries would to automobile body structures is more dependent have to be developed, e.g., a comprehensive net- on quick, low-cost processing methods and ma- work of PMC repair facilities, and a recycling in- terials than it is on performance characteristics. dustry based on new technologies, There are several good candidate methods of pro- duction, including high-speed resin transfer mold- Economic justifications for using PMCs in au- ing, reaction molding, compression molding, and tomotive are not currently available. The eco- 155 156 ● Advanced Materials by Design nomics will not become clear until the manufac- annual U.S. auto production would have to con- turing developments and associated experience vert to large-scale PMC usage before a major im- are in hand. Economics, customer perception, pact is felt by such related industries as the steel and functional improvements will dictate the industry, tool and die manufacturers, and chem- eventual extent of usage. Present economic in- ical manufacturers. For example, it would take dicators suggest that PMCs would initially be used production of 500,000 largely-PMC vehicles per only for low-volume vehicles, and thus the most year to cause a 3 percent decrease in automo- likely scenario would be limited usage of these tive steel use. The corresponding effect on these materials. It is clear that a significant fraction of industries, therefore, would be minor. INTRODUCTION The use of PMC materials in the United States ● corrosion resistance; and in automotive applications has gradually evolved ● lower cost of vehicle ownership. over the past two decades. With new materials However, there are areas where major uncer- and processing techniques being continuously tainties exist that will require extensive research developed within the U.S. plastics and automo- and development prior to resolution. For example: tive industries, there is potential for a more rapid expansion of these types of applications in the ● high-speed, high-quality manufacturing proc- future. PMC applications, both for components esses with acceptable economics; and for major modular assemblies, appear to be ● satisfaction of all functional requirements, a potential major growth area that could have a particularly crash integrity and long-term significant impact on the U.S. automotive industry durability; and associated supply industries if the required ● repairability; developments result in cost-effective manufactur- ● recyclability; and ing processes. ● customer acceptance. Extensive research and development (R&D) ef- The purpose of this case study is to present forts currently underway are aimed at realizing scenarios showing the potential impact of PMCs eight potential benefits of PMC structures for the on the U.S. automotive industry, its supplier base, U.S. automotive industry: and customers. These scenarios depict the effects likely to be generated by implementation of the ● weight reduction, which may be translated types of materials and process techniques that into improved fuel economy and performance; could find acceptance in the manufacturing in- ● improved overall vehicle quality and consis- dustries during the late 1990s, provided devel- tency in manufacturing; opment and cost issues are favorably resolved, ● part consolidation resulting in lower vehicle and manufacturing costs; To project the potential of PMCs for automo- ● improved ride performance (reduced noise, tive applications, it is necessary to provide a rea- vibration, and harshness); sonably extensive summary of the current state ● vehicle style differentiation with acceptable of these materials from the U.S. automotive in- or reduced cost; dustry’s perspective. In particular, the specific ● lower investment costs for plants, facilities, types of PMCs showing the most promise for struc- and tooling—depends on cost/volume rela- tural applications are described, as well as the tionships; most viable fabrication processes. The particu- lar properties of greatest relevance to automo- ‘This chapter is based on a contractor report prepared for the tive applications are presented, together with an Office of Technology Assessment, by P, Beardmore, C.F. johnson, agenda for gaining the knowledge required be- and G.G. Strosberg, Ford Motor Co., entitled “Impact of New Ma- terials on Basic Manufacturing Industries—Case Study: Composite fore high confidence can be placed in the struc- Automobile Structure, ” 1987. tural application of the materials. Ch. 7—Case Study: Polymer Matrix Composites in Automobiles w 157 This case study illustrates the potential of PMCs does not include the hood, decklid, and doors, by examining the case of a highly integrated PMC has been chosen as representative of the type of body shell, as depicted in figure 7-1. Basically, assembly that might be produced in moderate this body shell is the major load-bearing struc- volumes as PMC materials begin to penetrate the ture of the automobile. This basic structure, which U.S. automobile industry. Figure 7-1.—Steel Body Shell Structure w SOURCE P Beardmore, C.F. Johnson, and G.G. Strosberg, Ford Motor Co., “im- pact of New Materials on Basic Manufacturing Industries, A Case Study’ Composite Automobile Structure,” contractor report for OTA, 1987 BACKGROUND The economic constraints in a mass-production The next major step for PMCs in the automo- industry such as the automotive industry are quite tive business is extension of usage into truly struc- different from the aerospace or even the specialty- tural applications such as the primary body struc- vehicle industry. This is particularly true in the ture, and chassis/suspension systems. These are potential application of high-performance PMC the structures that have to sustain the major road- materials, which to date have primarily been de- Ioads and crash loads. In addition, they must de- veloped and applied in the aerospace industry. liver an acceptable level of vehicle dynamics such At present, virtually all uses of plastics and PMCs that the passengers enjoy a comfortable ride. in high-volume vehicles are restricted to decora- These functional requirements must be totally tive or semistructural applications. satisfied for any new material to find extensive Sheet molding compound (SMC) materials are application in body structures, and it is no small the highest performance composites in general challenge to PMCs to meet these criteria effec- automotive use for bodies today. However, the tively. These criteria must also be satisfied in a most widely used SMC materials contain about cost-effective manner. Appropriate PMC fabrica- 25 percent chopped glass fibers by weight and tion procedures must be applied or developed cannot really be classified as high-performance that satisfy high production rates but still main- composites. Typically, SMC materials are used for tain the critical control of fiber placement and grille-opening panels on many auto lines and clo- distribution. sure panels (hoods, decklids, doors) on a few se- PMC body structures have been used in a va- lect models. riety of specialty vehicles for the past three dec- 158 “ Advanced Materials by Design ades; Lotus cars are a particularly well-known ex- tween an FRP vehicle and an identical steel ve- ample. The PMC reinforcement used in these hicle to derive baseline characteristics. Perhaps specialty vehicles is invariably glass fiber, typically the best comparison would be between the pro- in a polyester resin. A variety of production meth- totype “Graphite LTD” built by Ford, and a pro- ods have been used but perhaps the only thing duction steel vehicle.3 The vehicle was fabricated they have in common is that all the processes are by hand lay-up of graphite fiber prepreg. slow, primarily because of the very low produc- This graphite fiber-reinforced plastic (GrFRP) tion rate of vehicles (typically, up to a maximum 2 auto is shown in figure 7-2, and an exploded sche- of 5,000 per year). Thus, there has been no in- matic showing its composite parts is presented centive to accelerate the development of these in figure 7-3. The weight savings for the various processes for mass production. The other com- structures are given in table 7-1. While these mon factor among these specialty vehicles is the weight savings (of the order of 55 to 65 percent) general use of some type of steel backbone or might be considered optimal because of the use chassis, which is designed to absorb most of the of low density graphite fibers, other more cost- road loads and crash impact energy. Thus, while effective fibers are stiff enough to be able to the composite body can be considered somewhat achieve a major portion of these weight savings structural, the major structural loads are not im- (with redesign).4 Although the GrFRP vehicle posed on the composite materials. weighed 2,504 pounds compared to a similar Current vehicles that include high volumes of steel production vehicle of 3,750 pounds, vehi- fiber-reinforced plastic (FRP) have been designed cle evaluation tests indicated no perceptible dif- specifically for FRP materials, as opposed to be- ing patterned after a steel vehicle. Consequently, 3P. Beard more, J.J. Harwood, and E.J. Horton, paper presented it is not possible to make a direct comparison be- at the International Conference on Composite Materials, Paris, Au- gust 1980. 2 lbid. ‘Beard more, Johnson, and Strosberg, op. cit., footnote 1. Figure 7.2.—Ford Graphite Fiber Composite (GrFRP) Vehicle SOURCE: P. Beardmore, C.F. Johnson, and G.G. Strosberg, Ford Motor Co., “Impact of New Materials on Basic Manufacturing Industries, A Case Study: Composite Automobile Structure, ” contractor report for OTA, 1987 Ch. 7—Case Study: Polymer Matrix Composites in Automobiles s 159 Figure 7-3.— Ford GrFRP Vehicle With the Composite Components Shown er s SMC W , , ~ production grille opening panel lower control arms SOURCE: P Beardmore, C F Johnson, and G.G. Strosberq, Ford Motor Co., “lmpact of New Materials on Basic Manufacturing Industries, A Case Study Composite Automobile Structure, ” contractor report for OTA, 1987 ference between the vehicles.5 The GrFRP auto’s steel LTD autos. Thus, on a direct comparison ride quality and vehicle dynamics were judged basis, a vehicle with an entire FRP structure was at least equal to those of top-quality production proven at least equivalent to a steel vehicle from ‘Ibid, a vehicle dynamics viewpoint at a weight level only 67 percent of the steel vehicle. b The GrFRP auto clearly showed that high-cost Table 7-1 .—Major Weight Savings of GrFRPa fibers (graphite) and high-cost fabrication tech- Over Steel in Ford “Graphite LTD” Vehicle Prototype Weight in pounds Component Steel GrFRP Reduction Body-in-white...... 423.0 160.0 253.0 Table 7-2.—Crash Energy Absorption Associated Front end ...... 95.0 30.0 65.0 With Fracture of Composites Compared With Steel Frame ...... 283.0 206.0 77,0 (typical properties) Wheel(s) ...... 91.7 49.0 42.7 Hood ...... 49.0 17.2 32.3 Relative energy absorption Decklid ...... 42.8 14.3 28.9 Material (per unit weight) Doors (4)...... 141.0 55.5 85.5 High performance composites ...... 100 Bumpers (2) ...... 123.0 44.0 79.0 Commercial composites ...... 60-75 Driveshaft...... 21.1 14.9 6.2 —— Mild steel ...... 40 Total vehicle ...... 3750 2504 1246 a For example, graphite fiber-reinforced. aGrFRP = Graphite Fiber-Reinforced Plastic b For example, glass fiber. reinforced. SOURCE: P. Beardmore, C F Johnson, and G.G. Strosberg, Ford Motor Co , “lm- SOURCE: P. Beardmore, C.F. Johnson, and G.G. Strosberg, Ford Motor Co., “Im- pact of New Materials on Basic Manufacturing Industries, A Case pact of New Materials on Basic Manufacturing Industries, A Case Study: Composite Automobile Structure, ” contractor report for OTA, Study Composite Automobile Structure, ” contractor report for OTA, 1987 1987 160 . Advanced Materials by Design niques (hand lay-up) can yield a vehicle that is quently, these vehicles cannot be used to develop wholly acceptable in terms of handling, perform- guidelines for extensive PMC usage in high-vol- ance, and vehicle dynamics. However, crash and ume applications. durability performance were not demonstrated, The governing design guidelines for PMCs need and these issues will need serious development to be further developed to ascertain, for instance, work to achieve better-than-steel results. An even how to design using low-cost PMC materials, and bigger challenge is to translate the GrFRP auto’s to ascertain allowable for stiffness in situations performance into realistic economics through the where major integration of parts in PMCs elimi- use of cost-effective fibers, resins, and fabrication nates a myriad of joints. The following sections procedures. summarize information on composite materials, Specialty autos of high PMC content use steel performance criteria, and potential manufactur- es the major load-carrying structure and are not ing techniques. generally priced on a competitive basis. Conse- POLYMER MATRIX COMPOSITE MATERIALS By far the most comprehensive property data find specialized applications (in much the same have been developed on aerospace-type PMCs, way as graphite fibers), even though their ultimate in particular graphite fiber-reinforced epoxies properties may be somewhat superior. fabricated by hand lay-up of prepreg materials. The form of the glass fiber used will be very Relatively extensive databases are available on application-specific, and both chopped and con- these materials, and it would be very convenient tinuous glass fibers should find extensive use. to be able to build off this database for less eso- Most structural applications involving significant teric applications such as automobile structures. load inputs will probably use a combination of Graphite fibers are the favored choice in aero- both chopped and continuous glass fibers with space because of their superb combination of the particular proportions of each depending on stiffness, strength, and fatigue resistance. Unfor- the component or structure. Because all the fabri- tunately for the cost-conscious mass-production cation processes likely to play a significant role industries, these properties are attained only at in automotive production are capable of handling significant expense. Typical graphite fibers cost mixtures of continuous and chopped glass, this in the range of $25 per pound. There are inten- requirement should not present major restrictions. sive research efforts devoted to reducing these costs by using a pitch-based precursor but the One potential development likely to come about most optimistic predictions are for fibers in the if glass fiber PMCs come to occupy a significant range of $5 to 10 per pound, which would still portion of the structural content of an automo- keep them in the realm of very restricted poten- bile is the tailoring of glass fibers and correspond- tial for consumer-oriented industries.7 ing specialty resin development. The size of the industry (each pound of PMC per vehicle trans- The fiber with the greatest potential for automo- lates into approximately 10 million pounds per bile structural applications is E-glass fiber–cur- year in North America) dictates that it would be rently, $0.80 per pound—based on the optimal 8 economically feasible to have fiber and resin pro- combination of cost and performance. Similarly, duction tailored exclusively for the automotive the resin systems likely to dominate at least in the market. 9 The advantage of such an approach is near term are polyester and vinyl-ester resins that these developments will lead to incremental based primarily on a cost/processability trade-off improvements in specific PMC materials, which versus epoxy. Higher performance resins will only in turn should lead to increased applications and increased cost-effectiveness. ‘Ibid. 8 lbid. 9Ibid. Ch. 7—Case Study: Polymer Matrix Composites in Automobiles ● 161 Although thermoset matrix PMCs will probably in heat resistance and/or environmental sensitivity constitute the buIk of the structural applications, relative to vehicle requirements for high-perfor- thermoplastic-based PMCs formed by a compres- mance structures. sion molding process may well have a significant Other thermoplastic matrices for glass fiber- but lesser role to play. reinforced PMCs are under development, and Most of the compression-molded thermoplas- materials such as polyethyleneterephthalate (PET) tics in commercial use today tend to concentrate hold significant promise for the future. The ex- on polypropylene or nylon as the base resin. The tent to which thermoplastic PMCs will be used reason is simply the economic fact that these ma- in future structures will be directly dependent on terials tend to be the least expensive of the engi- material developments and the associated eco- neering thermoplastics and are easily processed. nomics. Both of these materials are somewhat deficient PERFORMANCE CRITERIA From a structural viewpoint, there are two ma- Figure 7-4.—Typical Fatigue Curves for jor categories of material response critical to ap- Unidirectional Glass Fiber Composite (GIFRP) as a Function of Volume Fraction of Glass Fibers (V ) plying PMCs to automobiles. These are fatigue F (durability) and energy absorption. In addition, there is another critical vehicle requirement, ride quality, which is usually defined in terms of noise, vibration, and ride harshness, and is generally perceived as directly related to vehicle stiffness and damping. Material characteristics play a sig- nificant role i n this category of vehicle response. These three categories will be discussed below. Fatigue 2 3 4 7 The specific fatigue resistance of glass fiber- 1 10 10 10 10 10’ 10’ 10 2N reinforced plastics (GIFRP) is a sensitive function F of the precise constitution of the material. How- ó A is defined as the amplitude of the cyclicly applied stress. ever, there are also preliminary research indica- NF is the number of cycles to failure. tions of the sensitivity to cyclic stresses. (For a fur- Fatigue is described by the number of cycles to failure at a given cyclicly applied stress. ther discussion of chopped and continuous glass fibers, see ch. 3.) SOURCE: P. Beardmore, C.F. Johnson, and G.G. Strosberg, Ford Motor Co., “Im- pact of New Materials on Basic Manufacturing Industries, A Case Study: Composite Automobile Structure, ” contractor report for OTA, For unidirectional GIFRP materials, the fatigue 1987. behavior can be characterized as illustrated in fig- ure 7-4. The most important characteristic in fig- ure 7-4 is the fairly well-defined fatigue limit ex- tends to produce less reliable fatigue test data. hibited by these materials; as a guiding principle Figure 7-5 shows the scatter in fatigue test data 11 12 this limit can be estimated as approximately 35 for SMC. 10 to 40 percent of the ultimate strength. A chopped It is also important to note that the different fail- glass PMC, by contrast, would have a fatigue limit ure modes in PMCs (in comparison to metals) can closer to 25 percent of the ultimate strength and I IT. R, Smith and M.). Owen, Modern P/astics, April 1969, pp. 124-29. 10 C.K. H. Dharan, Journal oiMater/a/s .$c/ence, VOI. 10, 1975, PP. 12A, po t em and z. Hashim, A/AA jourr?a/, VOI. 14, 1976, PP. 1665-70. 868-72. 162 ● Advanced Materials by Design Figure 7-5.—Typical Fatigue Curve for base is available such that conservative estimates Sheet Molding Compound can be developed and lead to reliable designs. It should be emphasized, however, that the me- 2.0 chanical properties of PMCs (much more than isotropic materials) are very sensitive to the fabri- 1.5 cation process. It is imperative that properties be related to the relevant manufacturing technique 1.0 to prevent misuse of baseline data. 0.5 Energy Absorption a 2 5 The elongation (strain) behavior of a material 0 10’ 10 10’ 10 10 10’ under stress can indicate a great deal about the Number of cycles to failure material’s ability to absorb crash energy. Metals SMC exhibits significant scatter in fatigue test data. exhibit linear stress-strain behavior only up to a SOURCE: P. Beardmore, CF. Johnson, and G.G. Strosberg, Ford Motor Co., “im- certain point, beyond which they plastically de- pact of New Materials on Basic Manufacturing Industries, A Case Study: Composite Automobile Structure, ” contractor report for OTA, form (see figure 7-6). This plastic deformation ab- 1987. sorbs a large amount of crash energy that could otherwise injure passengers. result in different design criteria for these mate- The stress-strain curves of all high-performance rials, depending on the functionality involved. For PMCs are essentially linear in nature, as shown instance, a decrease in stiffness can occur under in figure 7-7. This resembles the behavior of brittle cyclic stressing long before physical cracking and materials such as ceramics. Materials that are es- strength deterioration occur. If stiffness is a criti- cal part of the component function, the loss in stiffness under the cyclic road loads could result Figure 7-6.—Tensile Stress-Strain Curves for in loss of the stiffness-controlled function with no Steel and Aluminum accompanying danger of any loss in mechanical function. This phenomenon does not occur in 50 350 steel. 300 As a guiding principle, it follows from the above 40 that wherever possible, automotive structures 250 should be designed such that continuous fibers 30 take the primary stresses and chopped fibers 200 should be present to develop some degree of isotropic behavior. It is critical to minimize the 20 150 stress levels, particularly fatigue stresses, that have 100 to be borne by the chopped fibers, 10 There is emerging evidence from both funda- 50 mental research data and field experience with PMC components that glass fiber-reinforced PMCs 0.002 0.006 0.01 can be designed to withstand the rigorous fatigue Strain loads experienced under vehicle operating con- HRLC—hot rolled leaded carbon steel ditions. The success of PMC leaf springs and SMC 1100-H12—strain hardened low alloy aluminum components attests to the capability of PMCs to The plastic region of metal stress-strain behavior absorbs withstand service environments. crash energy. SOURCE: P. Beardmore, C.F. Johnson, and G.G. Strosberg, Ford Motor Co., “im- Although the data for all combinations of PMC pact of New Materials on Basic Manufacturing Industries, A Case Study: Composite Automobile Structure,” contractor report for OTA, materials are not yet available, a sufficient data- 1987. Ch. 7—Case Study: Polymer Matrix Composites in Automobiles “ 163 Figure 7-7.—Tensile Stress-Strain Curves for Graphite Figure 7.8.—Energy Dissipation Mechanism Fiber Composite (GrFRP), Kevlar Fiber Composite in- Ceramics (KFRP), and Glass Fiber Composite (GIFRP) Energy dissipation D “cone” Projectile Energy absorption occurs in ceramics and brittle PMCs by spreading local impact energy into a high-volume cone of fractured material. SOURCE: P. Beardmore, CF. Johnson, and G.G. Strosberg, Ford Motor Co., “im- pact of New Materials on Basic Manufacturing Industries, A Case Study: Composite Automobile Structure,” contractor report for OTA, 1987, This analogy leads directly to the conclusion that high-performance PMCs may well be able to ab- sorb energy by a controlled disintegration (frac- ture) process. 1.0 1.5 2.0 2.5 3.0 3.5 Evidence is emerging from laboratory test data Strain, 0/0 on the axial collapse of PMC tubes that efficient The linearity of the curves means that these composites be- energy absorption needed for vehicle structures have as brittle materials during fracture (cf fig. 7-6). There is no plastic region to absorb crash energy. can be achieved in these materials. A compari- 3 son between the collapse mechanisms of metals 1 KSI = 10 psi and PMCs is shown in figure 7-9. Glass fiber- and SOURCE’ P Beardmore, C.F. Johnson, and G.G. Slrosberg, Ford Motor Co., “im- pact of New Materials on Basic Manufacturing Industries, A Case graphite fiber-reinforced PMCs behave as shown Study Composite Automobile Structure, ” contractor report for OTA, in figure 7-9(b). By contrast, PMCs using fibers 1987 consisting of highly oriented long-chain polymers (e.g., Kevlar) collapse in a metal-like fashion using sentially elastic to failure (PMCs, ceramics) might plastic deformation as the energy absorbing mech- be thought to have no capacity for energy ab- anism. The fragmentation/fracture mechanism sorption since no energy can be absorbed through typical of glass fiber PMCs can be very effective plastic deformation. However, ceramics have in absorbing energy, as illustrated in table 7-2. been used for decades as armored protection against high-velocity projectiles. It is particularly significant that although high- performance, highly oriented PMCs provide the In fact, energy absorption is achieved by spread- maximum energy absorption, commercial-type ing the localized impact energy into a high-vol- PMCs yield specific energy numbers considera- ume cone of fractured ceramic material, as shown bly superior to metals. Thornton and coworkers schematically in figure 7-8. A large amount of have accumulated extensive data on energy ab- fracture surface area is created by fragmentation sorption in composites .13 14 15 of the solid ceramic, and the impact energy is converted into surface energy resulting in suc- 13p H. T~OrntOn and P.j. Edwards, journa/ of Composite Materi- cessful protection and very efficient energy dis- als, vol. 13, 1979, pp. 274-82. sipation. Brittle materials can be very effective 14P. H. Thornton and P.j. Edwards, Journa/ of cOrnP05;te Mater/- d/s, VOI. 16, 1982, pp. 521-45. energy absorbers, but the mechanism is fracture I sp H, Thornton, j.j. Harwood, and P. Beard more, International surface energy rather than plastic deformation. Journal of Composite Structures, 1985. 164 Advanced Materials by Design Figure 7-9.—C)ifferent Collapse Mechanisms in normally plays a significant part in the collapse (a) Metal and (b) Composite Tubes, for of the vehicle structure, and it is consequently Energy Absorption of considerable importance to evaluate energy absorption of composites in bending failure. Just as in metals, little data are available on energy absorption characteristics in bending. There is no reason to believe that the energy ab- sorption values of metals relative to PMCs in bending should change significantly from the ra- tios in axial collapse except that bending failure (fracture) in PMCs may tend to occur on a more localized basis than plastic bending in metals. If this does indeed occur, then the ratio could change in the favor of metals. Other crash issues involve the capacity to ab- sorb multiple and angular impacts and the long- term effects of environment on energy absorp- tion capability. In general, practical data from a realistic, vehicle viewpoint are not yet in hand. An additional, significant factor is the consumer acceptance of these materials as perceived in re- lation to safety. A negative perception would be a) energy, absorption by plastic deformation a serious issue on something as sensitive as safety, b) fracture surface energy dissipation and better-than-steel crash behavior will be re- quired before wide-scale implementation of PMCs can occur. Conversely, a positive perception would be a valuable marketing feature and pro- vide an additional impetus for PMC applications. Stiffness and Damping Glass fiber-reinforced PMCs are inherently less stiff than steel. Some typical values for various types of PMC are listed in table 7-3. There are two offsetting factors to compensate for these ma- terial limitations. First, an increase in wall thick- ness can be used to offset partially the lesser ma- terial stiffness. Also, local areas can be thickened as required to optimize properties. Because PMCs SOURCE: P. Beardmore, C.F. Johnson, and G.G. Strosberg, Ford Motor Co., “lm. have a density approximately one-third that of pact of New Materials on Basic Manufacturing Industries, A Case steel, a significant increase in thickness can be Study: Composite Automobile Structure,” contractor report for OTA, 1987. achieved while maintaining an appreciable weight reduction. Virtually all the energy absorption data avail- able to date have been developed for axial col- The second, and perhaps the major, offsetting lapse of relatively simple structures, usually tubes. factor is the additional stiffness attained in PMCs The ability to generate the same effective fracture as a result of part integration. This integration mechanisms in complex structures is still unre- leads directly to the elimination of joints, which solved. In addition, it is well known from obser- results in significant increases in effective stiffness. vations on metal vehicles that bending collapse It is becoming increasingly evident that this syn- Ch. 7—Case Study: Polymer Matrix Composites in Automobiles ● 165 Table 7-3.—Typical Stiffness of Selected Composites The stiffness requirement for vehicles is nor- mally dictated by vehicle dynamics characteris- Material Stiffness (lO6psi) tics. The historical axiom in the vehicle engineer’s Unidirectional GrFRP ...... 20 Unidirectional GIFRP ...... 6 design principles is the stiffer the better. How- Unidirectional Kevlar...... 11 ever, there are some intangible factors that en- XMC ...... 4.5 ter the overall picture, in particular the damping SMC-R50 ...... 2.3 SMC-25 ...... 1.3 factor. SOURCE: P. Beardmore, C.F. Johnson, and G.G. Stromberg, Ford Motor Co. ’’lm- pact of New Materials on Basic Manufacturing Industries, A Case Study: Composite Automobile Structure, ” contractor report for OTA, 1987. It is an oversimplification to assume stiffness alone dictates vehicle dynamics, although it un- ergism is such that structures of acceptable stiff- questionably dominates certain categories. Damp- ness and considerably reduced weight are feasi- ing effects can play an equally significant role i n ble in glass fiber-reinforced PMCs. As a rule of many categories of body dynamics, and the fact thumb, a glass FRP structure with significant part that the damping of PMC materials considerably integration relative to the steel structure being exceeds that of metals is relevant to the overall replaced can be designed for a nominal stiffness scenario. Most experts involved with PMC com- level of 50 to 60 percent of the steel structure.16 ponent/structure prototype development feel that Such a design procedure should lead to adequate some aspect of body dynamics (usually noise or stiffness and to typical weight reductions of 20 vibration) is improved but few quantitative data to 50 percent.17 are available to document the degree of improve- lbgeardmore, Johnson, and Strosberg, Op. cit., footnote 1, ment. If customers share this perception, PMCs 1‘Ibid. will receive impetus for structural usage. POTENTIAL MANUFACTURING TECHNIQUES The successful application of PMCs to automo- transfer molding, and filament winding. Each of tive structures is more dependent on the ability these processes is examined below. to use rapid, economic fabrication processes than on any other single factor. The fabrication proc- esses must also be capable of close control of Compression Molding PMC properties to achieve lightweight, efficient This section discusses compression molding structures. techniques; these are most often used with ther- Currently, the only commercial process that mosetting resins but can be used with thermo- comes close to satisfying these requirements is plastic resins. compression molding of sheet molding com- pounds (SMCs) or some variant on this process. Thermosetting Compression Molding There are, however, several developing processes Figure 7-11 presents a schematic of the SMC that hold distinct promise for the future in that process, depicting both the fabrication of the they have the potential to combine high rates of production, precise fiber control, and high degrees SMC material and the subsequent compression molding into a component. This technology has of part integration. been widely used in the automobile industry for The requirements for precise fiber control, rapid the fabrication of grille-opening panels on many production rates, and high complexity demand auto lines, and for some exterior panels on se- that automotive processes be in the region of de- lected vehicles. Tailgates (figure 7-12), and hoods veloping processes shown schematically in fig- (figure 7-13) are examples on autos and light ure 7-10. The three most important evolving proc- trucks; the entire cab on some heavy trucks (fig- esses are compression molding, high-speed resin ure 7-14) is constructed in this manner. 766 . Advanced Materials by Design Figure 7-10.—Relationship Between Performance and The above description of the SMC process de- Fabrication for Composites lineates material primarily used for semistructural Automotive Composite Process Development applications rather than high load bearing seg- ments of the structure that must satisfy severe Hand durability and energy absorption requirements. lay-up / Figure 7.12.—Typical Sheet Molding Compound Size, complexity, Region of developing processes Production Aerostar Tailgate performance (i.e., high-speed resin transfer) / Thermoplastic stamping Viable commercial processes must be able to produce a large number of high performance parts. SOURCE: P. Beardmore, C.F. Johnson, and G.G. Strosberg, Ford Motor Co., “im- pact of New Materials on Basic Manufacturing Industries, A Case Study: Composite Automobile Structure,” contractor report for OTA, 1987. Figure 7-11 .—Sheet Molding Compound Material Preparation and Component Fabrication Sheet Molding - Chopped galss SOURCE: P. Beardmore, CF. Johnson, and G.G. Strosberg, Ford Motor Co., “im- pact of New Materials on Basic Manufacturing Industries, A Case Study: Composite Automobile Structure, ” contractor report for OTA, 1987. The process consists of placing sheets of SMC (1 to 2 inch long chopped glass fibers in chemi- cally thickened thermoset resin) into a heated mold (typically at 3000 F) and closing the mold under pressures of 1,000 pounds per square inch (psi) for about 2 to 3 minutes to cure the mate- rial. Approximately 80 percent of the mold sur- face is covered by the SMC charge, and the ma- SOURCE: P. Beardmore, C.F. Johnson, and G.G. Strosberg, Ford Motor Co., “im- terial flows to fill the remaining mold cavity as pact of New Materials on Basic Manufacturing Industries, A Case Study: Composite Automobile Structure,” contractor report for OTA, the mold closes. 1987, Ch. 7—Case Study: Polymer Matrix Composites in Automobiles ● 167 To sustain the more stringent structural demands, Figure 7-14.—Typical SMC Truck Cab it is normalIy necessary to incorporate apprecia- Figure 7-13.—Typical SMC Production Aerostar Hood SOURCE: P. Beardmore, C.F. Johnson, and G.G. Strosberg, Ford Motor Co., “im- pact of New Materials on Basic Manufacturing Industries, A Case Study: Composite Automobile Structure, ” contractor report for OTA, 1987. ble amounts of continuous fibers in predesignated locations and orientations. The same basic SMC operation can be used to incorporate such material modifications either by formulating the material to include the continu- ous fibers along with the chopped fibers or by using separate charge patterns of two different types of material. The complexity of shape and degree of flow possible are governed by the amount and location of the continuous glass ma- terial. Careful charge pattern development is nec- essary for components of complex geometry. A typical example of a prototype rear floor pan fabricated by this technique is shown in figure 7-15.18 The limitations of compression molding of SMC- type materials in truly structural applications have yet to be established. Provided that continuous fiber is strategically incorporated, these materials promise to be capable of providing high structural integrity and may well prove to be the pioneer- ing fabrication procedure in high load bearing ap- plications. The state of commercialization of this process is advanced compared to other evolving techniques and this will provide a lead time for SOURCE P Beardmore, CF. Johnson, and G G Strosberg, Ford Motor Co , “im- 18c, F. Johnson and N .G. Chavka, ‘‘An Escort Rear Floor pan, pact of New Materials on Basic Manufacturing Industries, A Case Study Composite Automobile Structure, ” contractor report for OTA, Proceedings ot’the 40th Annual TechrricJ/ Conference, Atlanta, GA, 1987 Society of the Plastics Industry, January 1985, 168 . Advanced Materials by Design Figure 7-15.—Prototype Escort Composite Rear that yield a heavier-than-necessary component Floor Pan or structure. Currently, extensive research efforts are underway to develop SMC-type materials that will allow 100 percent charge pattern coverage and that will attain high, uniform mechanical properties with minimal flow. These materials can also be molded at lower pressures on smaller ca- pacity presses. Materials developments such as these may well make the newer breed of SMCs much more applicable to highly loaded structures than has hitherto been envisioned. Another potential limitation of compression molding is the degree of part integration that is attainable. The basic strategy in PMC applications is to integrate as many individual (steel) pieces as possible to minimize fabrication and assem- bly costs (which offsets increased material costs) and to minimize joints (which increases effective stiffness). Compression molding requires fairly high molding pressures (about 1,000 pounds psi) and thus limits potential structures in area size and complexity (particularly in three-dimensional geometries requiring foam cores). Consequently, although compression molding is likely to play a key role in the development of PMCs in structural automotive applications in the next decade, ultimately the process is unlikely to provide composite parts of optimum structural SOURCE: P. Beardmore, C.F. Johnson, and G.G. Strosberg, Ford Motor Co., “im- pact of New Materials on Basic Manufacturing Industries, A Case efficiency and weight. Nevertheless, compression Study: Composite Automobile Structure,” contractor report for OTA, molding is currently the only commercial PMC 1987. process capable of satisfying the economic con- straints of a mass-production industry. compression molding to branch into higher per- formance parts. Thermoplastic Compression Molding Although compression molding of SMC-type The process of thermoplastic compression materials is an economically viable, high produc- molding (stamping) is attractive to the automo- tion rate process in current use, there are some tive industry because of the rapid cycle time and limitations inherent in the process. In the longer the potential use of some existing metal stamp- term, these will restrict applications and tend to ing equipment. Thermoplastic compression mold- favor the developing processes. For instance, ma- ing at its current level of development achieves terial flow in the compression step results in cycle times of 1 minute for large components. imprecise control of fiber location and orienta- Figure 7-16 presents a schematic of the proc- tion. Typically, variations in mechanical proper- ess. Typically, a sheet of premanufactured ther- ties of a factor of 2 throughout the component moplastic and reinforcement is preheated above are not unusual based on an initial charge-pattern the melting point of the matrix material and then coverage of approximately 70 percent. rapidly transferred to the mold. The mold is Such uncertainty in properties introduces relia- quickly closed until the point where the mate- bility issues and encourages conservative designs rial is contacted, and then the closing rate is Ch. 7—Case Study: Polymer Matrix Composites in Automobiles ● 169 Figure 7-16.—Thermoplastic Compression Molding Although effective for simple configurations, location of the oriented reinforcement and repro- ducibility of location are problems in complex parts. To be most effective, these types of rein- forcements ultimately will have to be part of the premanufactured sheet or be robotically applied. Current research is in progress in the area of ther- moplastic sheet materials with oriented reinforce- ment in critical areas. For application to automo- tive structures, these materials will have to retain the geometric flexibility in molding (i. e., ability Heated blank loaded Mold closing, compressing to form complex shapes with the reinforcement material to fill cavity into mold in the correct location) exhibited by today’s com- SOURCE” P. Beardmore, C F. Johnson, and G.G. Strosberg, Ford Motor Co., “im- mercial materials. pact of New Materials on Basic Manufacturing Industries, A Case Study: Composite Automobile Structure” contractor report for OTA, 1987 The question of part integration is a major is- sue in the expanded use of this process. The high pressures (1 ,000 to 3,000 psi) required limit the slowed. The material is formed to shape and flows to fill the mold cavity much the same as ther- size of components that can be manufactured on moset compression-molded SMC. The material conventional presses. Thermoplastic compression is cooled in the mold for a short period of time molding is also limited in its ability to incorporate complex three-dimensional cores required for op- to allow the part to harden, and then the mold is opened and the component is removed. timum part integration. Thermoplastic compression molding is cur- If very large integrated structures are required from an overall economic viewpoint, thermoplas- rently used in automobiles to form low-cost semi- tic compression molding will be restricted to structural components such as bumper backup beams, seats, and load floors. Commercially avail- smaller components such as door, hood, and deck lid inner panels in which geometry is rela- able materials range from wood-filled polypropy- lene and short glass-filled polypropylene with tively simple and/or part integration is limited due relatively low physical properties, to continuous to physical part constraints. If very large-scale in- tegration proves too expensive, then thermoplas- random glass-reinforced materials based on poly- propylene or PET which offer somewhat higher tic compression molding will exhibit increased physical properties. Other materials, based on market penetration. Ongoing long-range research in the area of low-pressure systems and incorpo- highly oriented reinforcements and such resins ration of foam cores in moldings could signifi- as polyetheretherketone (PEEK) and polyphony - Iene sulfide (PPS), are in use in the aerospace in- cantly alter this outlook in the longer term. dustry. These materials are expensive and are limited in their conformability to complex shapes. High-Speed Resin Transfer Molding Higher levels of strength and stiffness must be Fabrication processes that permit precise fiber developed in low-cost materials before they can control with rapid processability would overcome be used in structural automotive applications. At- many of the deficiencies outlined above. The use tempts have been made to improve the proper- of some kind of preform of oriented glass fibers ties of stampable materials through the use of preplaced in the mold cavity, followed by the in- separate, preimpregnated, unidirectional rein- troduction of a resin with no resultant fiber move- forcement tapes. These materials are added to ment would satisfy the requirements for optimum the heated material charge at critical locations performance and high reliability. to improve the local strength and stiffness. Using these materials adds to the cost of the material The basic concepts required for this process are and increases cycle times slightly. practiced fairly widely today in the boat-building 170 ● Advanced Materials by Design and specialty-auto business. However, with few There are two basic elements associated with exceptions, the glass preform is hand-constructed the high-speed resin transfer molding (HSRTM) and the resin injection and cure times are of the process that must be developed. The assemblage order of tens of minutes or greater. Also, dimen- of the glass preform must be developed such that sional consistency necessary for assembling high- it can be placed in the mold as a single piece. quality products has not been studied for this In addition, the introduction of the resin into the process. mold must be rapid and the cure cycle must be equally fast to provide a mold-closed/mold-open Major reductions in manufacturing time and cycle time of only a few minutes, A schematic automation of all phases of the process are nec- of the process is presented in figure 7-17. essary to increase automotive production rates. However, the basic ingredients of precise fiber control and highly integrated complex part ge- There are two processes currently in use that ometries (including, for instance, box sections) may have the potential to offer rapid resin injec- are an integral part of this process and offer po- tion and cure times. One is resin transfer mold- tentially large cost benefits. ing. Currently in widespread use at slow rates, Figure 7-17.–High-Speed Resin Transfer Molding (HSRTM) Glass preform Dry glass fiber Epoxy shaping die J Heated steel/aluminum die ‘“ Q Resin pump SOURCE: P. Beardmore, C.F, Johnson, and G.G. Strosberg, Ford Motor-Co., “Impact of New Materials on Basic Manufacturing Industries, A Case Study: Composite Automobile Structure,” contractor report for OTA, 1987. Ch. 7—Case Study: Polymer Matrix Composites in Automobiles ● 171 it could be accelerated dramatically by the use Full three-dimensional geometries including of low-viscosity resins, multiport injection sites, box sections, are attainable by preform molding. computer-controlled feedback injection controls, In addition, only low-pressure presses are nec- and sophisticated heated steel tools. There do not essary. The high degree of part integration max- appear to be any significant technological bar- imizes effective stiffness and minimizes assembly. riers to these kinds of developments, but it will In principle, major portions of vehicles could require a strong financial commitment to prove be molded in one piece; for instance, Lotus auto out such a system. A schematic of the process body structures consist of two major pieces (al- is presented in figure 7- I 8, which also illustrates beit molded very slowly) with one circumferen- a variant on the process usually termed squeeze tial bond. If similar-size complex pieces could be molding. molded in minutes, a viable volume production technique could result. The second process that promises rapid injec- tion and cure cycles is reaction injection mold- Filament Winding ing (RIM). In reaction injection molding, two chemicals are mixed and injected simultaneously; Filament winding is a PMC fabrication process during injection the chemicals react to form a that for some geometric shapes can bridge the thermosetting resin. Once the dry glass preform gap between slow, labor-intensive aerospace fabri- is in the mold, the resin can be introduced by cation techniques and the rapid, automated fabri- any appropriate procedure, and reaction injec- cation processes needed for automotive manu- tion would be ideal, provided the resultant resin facturing. The basic process uses a continuous has adequate mechanical properties. The inher- fiber reinforcement to form a shape by winding ent low viscosity of RIM resins would be ideal over some predetermined path. Figure 7-19 pro- for rapid introduction into the mold. vides a process schematic. Figure 7-18.—Squeeze Molding and Resin Transfer Molding Squeeze molding Resin transfer molding Fiber preform .1 L SOURCE: P. Beardmore, C.F. Johnson, and G.G, Strosberg, Ford Motor Co., “Impact of New Materials on Basic Manufacturing Industries, A Case Study: Composite Automobile Structure, ” contractor report for OTA, 1987. 172 ● Advanced Materials by Design Figure 7.19.—Filament Winding Process Glass Filament impregnated application reinforcement head tape /. Resin impregnation bath Rotating . — component mandrel SOURCE: P. Beardmore, C.F. Johnson, and G.G. Strosberg, Ford Motor Co., “Impact of New Materials on Basic Manufacturing Industries, A Case Study: Composite Automobile Structure,” contractor report for OTA, 1987. The complexity and accuracy of the winding ment fibers are combined (referred to as wetting path are highly controllable with microcomputer- out of the reinforcement) immediately prior to controlled winding machines. Thin, hollow shapes the winding of the fibers onto the part. The having high fiber-to-resin ratios are possible, wetting-out and winding processes require pre- thereby making the process well suited to light- cise control of several variables. Reinforcement weight, high-performance components. Glass fi- tension, resin properties, and the fiber/resin ra- ber, aramid, or carbon fiber can be used as the tio all relate directly to the final physical proper- winding material. Filament winding can use ei- ties of the part. As the winding speed and part ther thermosetting or thermoplastic resin systems. complexity increase, these variables become in- The uniform fiber alignment afforded by the creasingly difficult to control. process provides high reliability and repeatabil- ity in filament-wound components. Some simple Winding of complex parts at automotive pro- shapes, such as leaf springs, can be fabricated by duction rates will require major process devel- this process and are currently in production on opments. The likely potential of thermoset fila- a limited basis. ment winding in automotive applications is in the fabrication of simple shapes such as leaf springs, Thermoset Filament Winding in which the cost penalty involved due to slow The majority of filament winding done today production speeds can be offset by a need for uses thermosetting resin systems. In the thermoset high reliability and maximum use of material filament-winding process, the resin and reinforce- properties. Ch. 7—Case Study: Polymer Matrix Composites in Automobiles ● 173 Thermoplastic Filament Winding The limitations with respect to filament tension, filament wet-out, and speed at which a wet fila- Filament winding of thermoplastic materials ment can be pulled through a payout eye are no represents both the leading edge of this technol- longer a major concern with thermoplastic fila- ogy and the area in which its potential benefit ment winding. Thick sections can be rapidly to the automotive industry is greatest. wound, and nongeodesic and concave sections Thermoplastic filament winding uses a rein- can be formed. However, the applicability to ge- forcement preimpregnated with a thermoplastic ometries as complex as body structures is not resin rather than a reinforcement impregnated established. Currently, problem areas exist in the with a thermosetting resin at the time of wind- carryover of physical properties due to the limited ing. The preimpregnated filament or, more often, amount of research that has been done on the tape, is wound into the appropriate shape in a process. There are problems with the control of manner similar to the thermosetting filament- the heating and consolidation of the thermoplas- winding process, with the exception of a local tic materials that yield less than predicted values heating and compaction step. for tensile strength and interlaminar shear strength. The reinforcement tape is heated with hot air Although the thermoplastic materials will likely or laser energy as it first touches the mandrel. The expand the structural component applications in heat melts the thermoplastic matrix both on the which thermoplastic filament winding can eco- tape and locally on the substrate permitting a nomically compete with thermoset filament wind- slight pressure applied by a following roller to ing, the increased speed and shape capabilities consolidate the material in the heated area. Be- will not entirely offset the limited degree of part cause the reinforcement filament is already wet integration possible. The inability to integrate box out in a prepregging process, the substrate is so- sections with large flat paneIs in a one-piece struc- lidified over its entirety with the exception of a ture having complex geometry will tend to limit small zone of molten material in the area of con- the penetration of filament winding in body solidation. structures. IMPACT ON PRODUCTION METHODS The following sections discuss the various im- An auto body is a complex structure, and its pacts of these candidate technologies on automo- design is influenced by many demanding factors. bile production methods. At the present time, it appears that two systems can be considered as possible processes to build Manufacturing Approach the structural panels for PMC auto bodies. The manufacturing approach for producing One system consists of compression molding. autos with PMC structural parts will be consider- Compression molded thin-walled panels are first ably different from the methods employed for bonded together to form structural panels (see building conventional vehicles with steel bodies. figure 7-21) and then the structural panels, are Currently, many domestic automotive assembly assembled to form auto bodies. The other sys- plants for steel vehicles are used for very little tem involves HSRTM, in which preforms of fiber basic manufacturing. Instead, high-volume sheet reinforcement are combined with foam cores, steel stamping plants, geographically located to placed in a mold, and resin-injected to form large, service several assembly plants, produce body three-dimensional structural panels (see figure 7- components and small assemblies and ship them 22). These panels are then assembled into auto to the assembly pIants. The plants assemble the bodies. It is important to note that the filament- sheet metal components into an auto body struc- winding process is viewed as a limited construc- ture as presented in table 7-4 and figure 7-20a tion method largely due to the restricted com- and b. plexity that is available with this technique. 174 ● Advanced Materials by Design Table 7-4.—Typical Body Construction System: bining the preform with foam cores, and inject- Steel Panels ing resin into the mold to infiltrate the preform. ● Build front structure—assemble aprons, radiator support, First, dry glass preform reinforcements must be torque boxes, etc. to dash panel fabricated. The preform may be composed of pri- ● Build front floor pan assembly ● Assemble front and rear floor pan into underbody assembly marily randomly oriented glass fibers with added ● Complete spot welding of underbody assembly directional glass fibers or woven glass cloth for ● Transfer underbody to skid ● Build left-hand and right-hand bodyside assemblies ● Move underbody, bodyside assemblies, cowl top, wind- shield header, rear header, etc. into body buck line and Figure 7-20(a).-Typical Assembly of Steel Underbody tack-weld parts ● Complete spot welding of body ● Braze and fusion-weld sheet metal where required ● Assemble, tack-weld and respot roof panel to body ● Assemble front fenders to body ● Assemble closure panels (doors, hood, decklid) to body ● Finish exterior surface where required SOURCE: P. Beardmore, C.F. Johnson, and G.G. Strosberg, Ford Motor Co., “im- pact of New Materials on Basic Manufacturing Industries, A Case Study: Composite Automobile Structure, ” contractor report for OTA, 1987. Therefore, it cannot now be considered as a com- petitive process for high-volume body structure fabrication. Compression Molded Structural Bodies Compression molded structural panels might be produced as presented in table 7-5 and fig- Figure 7=20(b). -Typical Assembly of Underbody, ure 7-21. Panel assemblies (side panels, floor Bodyside Assemblies, Etc. into the Completed pans, roof panels, etc.) are produced from inner Steel Body Shell and outer components. First, SMC sheet must be manufactured and blanks of proper size and weight arranged in a large predetermined pattern on the die surface. The panels are then molded in high-tonnage presses. After molding, the parts are processed in a number of secondary opera- tions, bonded together, and transported to the body assembly line. Body construction commences with the floor panel being placed in an assembly fixture. Side panel assemblies and mating components are bonded in place. Attachment points for the ex- terior body panels are drilled and the body struc- ture is painted prior to transporting to the trim operations. (The body construction sequence is described later, see table 7-9 and figure 7-24.) High-Speed Resin Transfer Molded Structural Bodies SOURCE: P. Beardmore, C.F. Johnson, and G.G. Strosberg, Ford Motor Co., “im- HSRTM processing consists of three stages that pact of New Materials on Basic Manufacturing Industries, A Case Study: Composite Automobile Structure)” contractor report for OTA, involve making a dry glass fiber preform, com- 1907. Ch. 7—Case Study: Polymer Matrix Composites in Automobiles c 175 Figure 7-21 .—Typical Assembly of Composite Table 7-5.—Compression Molded Structural Panels Bodyside Panel by Adhesive Bonding of Inner and Outer SMC Molded Panels ● Fabricate and prepare SMC charge ● Load charge into die and mold panel ● Remove components from molding machine (inner and out- er panels), trim and drill parts as required ● Attach reinforcements, latches, etc., to inner and outer panels, with adhesive/rivets ● Apply mixed, two component adhesive to outer panel ● Assemble inner and outer panels, clamp and cure ● Remove excess adhesive ● Remove body panel from fixture and transport to body con-