Guide to High Performance Alloys

Total Page:16

File Type:pdf, Size:1020Kb

Guide to High Performance Alloys Table of Contents Alloy Guide 3 The Alloys of Materion Brush Performance Alloys 4 Chemical Composition 6 Alloy Products 6 Physical Properties 8 Product Guide 10 Strip and Wire Temper Designations 11 Strip 12 Strip Product Specifications 13 Spring Bend Limits of Strip Alloys 19 Wire 20 Rod, Bar, Tube and Plate Temper Designations 22 Rod and Bar 22 Tube 26 Plate and Rolled Bar 29 MoldMAX® and PROtherm™ Plastic Tooling Alloys 31 ToughMet® and Alloy 25 Oilfield Products 32 Alloy 25 Drill String Temper (25 DST) 33 BrushCAST® Casting Ingot & Master Alloys 34 Forged and Extruded Finished Components 36 Cast Shapes 37 Recommended Replacements for Discontinued Alloys 38 Materion Brush Performance Alloys Value-Added Services 39 Custom Fabrication Capabilities 40 Customer Technical Service 40 Other Services 42 Processing and Fabrication Guide 43 Heat Treating Fundamentals 44 Forming of Strip 47 Cleaning and Finishing 50 Joining 51 Machining 53 Hardness 56 Microstructures 57 Other Attributes and Application Engineering Data 59 Fatigue Strength 60 Stress Relaxation Resistance 62 Corrosion Resistance 64 Magnetic Properties 67 Galling Resistance 68 Bearing Properties 69 Friction & Wear Properties 69 Resilience and Toughness 70 Elevated Temperature Properties 71 Cryogenic Properties 72 Other Attributes 72 Your Supplier 73 Company and Corporate History 74 Materion Corporate Profile 75 Brush Performance Alloys Mining & Manufacturing 77 Product Distribution 78 Customer Service 79 Quality 80 Health and Safety, Environment and Recycling 81 Alloy Guide The copper and nickel alloys commonly supplied in wrought product form are highlighted in this section. Wrought products are those in which final shape is achieved by working rather than by casting. Cast alloys are described in a later section of this publication. Although the alloys in this guide are foremost in the line that has estab- lished Materion Brush Performance Alloys’ worldwide reputation for quality, they are not the only possibilities. We welcome the opportunity to work with you in selecting or developing an alloy to make your application succeed. THE ALLOYS OF MAtERiON BRUSH PERFORMANCE ALLOYS 4 CHEMiCAL COMpOSitiON 6 ALLOY PROdUCtS 6 PHYSiCAL PROpERtiES 8 3 Alloy Guide The Alloys of Materion Brush Performance Alloys In addition to the standard alloys listed here, Materion Brush Alloy 165 contains less beryllium than Alloy 25. and may Performance Alloys has the capability to produce other copper be substituted when strength is less demanding. Alloy 165 alloys, or to provide toll processing of alloys cast elsewhere. Please is available in wrought product forms in heat treatable and consult with your local sales representative for further information. aged tempers. Copper Beryllium Alloys 3 and 10 combine moderate yield strength, up Materion Brush Performance Alloys manufactures copper beryllium to 125 ksi, with electrical and thermal conductivity from in several distinct compositions. These fall into two categories: alloys 45 to 60 % of pure copper. Alloys 3 and 10 are available selected for high strength (Alloys 25, 190, 290, M25 and 165) in wrought product forms and can be supplied fully and alloys selected for high conductivity (Alloys 3, 10, 174 and hardened. Hardened products are identified by the temper Brush 60®). Alloy 390® combines both attributes, high strength and designation AT or HT, and have good formability. high conductivity. Many of these alloys are available in both heat ® treatable and mill hardened (pre-heat treated) conditions. Brush 60 and Brush Alloy 174 offer users the opportunity to upgrade component performance over Alloy 25 is the most commonly specified copper beryllium and is bronzes and brasses, particularly where conductivity and available in the wrought forms listed on page 7. In its age hardened stress relaxation resistance are design considerations. condition, Alloy 25 attains the highest strength and hardness of any They are supplied with yield strength up to 125 ksi, commercial copper base alloy. The ultimate tensile strength can superior to other copper alloys such as phosphor bronze, exceed 200 ksi, while the hardness approaches HRC 45. Also, in silicon bronze, aluminum, brass and copper nickel alloys. the fully aged condition, the electrical conductivity is a minimum of Furthermore, they offer up to five-fold better electrical 22% IACS (International Annealed Copper Standard, where 100% conductivity than those alloys, and exhibit better stress IACS = 0.679 micro-ohm-inches or 1.72 micro-ohm-cm). Alloy 25 relaxation resistance. These alloys offer an excellent also exhibits exceptional resistance to stress relaxation at elevated combination of elastic modulus, strength, formability and temperatures. conductivity. Both are available as mill hardened strip. Alloy 190 is a mill hardened strip product. The strip is Alloy 390® and Alloy 390E® combine the best age hardened to a specified strength level as part of the attributes of the two separate families of commercial copper manufacturing process at Brush Performance Alloys prior to beryllium alloys – the strength of the “high strength” Alloy shipment. This alloy is similar to Alloy 25 in chemical composition. 25 with the conductivity of “high conductivity” Alloys 3 and Alloy 190 is supplied with tensile strength up to 190 ksi. Cost 174. In addition to the combination of high strength and effectiveness is realized by elimination of the need for age conductivity, Alloys 390® and 390E® have excellent stress hardening and cleaning of stamped parts. relaxation resistance at elevated temperatures. In applications where durability is important, their excellent fatigue strength Alloy 290 is a mill hardened strip product that is similar in extends product life and improves product quality. Alloy 390® strength properties and composition to Alloy 190, but exhibits and 390E® are available as prehardened strip. improved formability. Component reliability and fabrication considerations may require a high strength material with good Alloy 310 is a copper nickel cobalt beryllium alloy formability. The improved strength/formability relationship of with high electrical and thermal conductivity. It possesses Alloy 290 makes it a cost effective alternative to conventional mill good strength and hardness, and has been shown to have hardened product for such applications. excellent thermal fatigue resistance. It is typically used in welding electrodes as well as dies, plunger tips and nozzles Alloy M25 offers the strength properties of Alloy 25 with the for metal die casting. added benefit of being “free machining.” Alloy M25 rod and wire contain a small amount of lead to provide an alloy tailored for Nickel Beryllium automatic machining operations. Lead promotes formation of Alloy 360 nickel beryllium strip features high strength and finely divided chips and extends cutting tool life. stiffness usually associated with steel and nickel alloys, while retaining excellent formability. It can withstand temperatures up to 700° F (375 °C) without losing spring properties, and will retain over 90% of its initial stress over 1,000 hours at that temperature. © 2012 Materion Brush Inc. 4 Alloy Guide ToughMet® FormaMet® is a machinable die bronze used for deep drawing Materion Brush Performance Alloys produces a number or forming of stainless and low carbon steels. It combines high of engineered high performance copper alloys using a hardness (typically 39 HRC) with excellent lubricity and high patented technology called EquaCast®. The process produces resistance to wear and galling. It promotes extended tool life and an extremely uniform, fine-grained microstructure and minimizes wrinkling and tearing of drawn parts. promotes excellent dispersion of alloy elements for high quality, consistent products. Plastic Tooling Alloys Materion Brush Performance Alloys also manufactures ToughMet® 2 is a spinodally hardened copper nickel tin MoldMAX® and PROtherm™ alloys for use as tooling and inserts alloy possessing outstanding lubricity and machinability. Its in the plastic molding industries. corrosion resistance is superior to most other copper alloys, MoldMAX HH® is a high strength copper beryllium alloy, with with hardness up to HRC 27. It is used for wear plates and typical hardness of HRC 40 and thermal conductivity of 75 BTU/ low friction bushings and bearings. ft·hr·°F (130 W/m·°C). Its hardness and wear resistance make ToughMet® 3 is a spinodally hardened copper nickel it suitable for injection mold components and long life in wear- tin alloy, possessing much higher strength and hardness, prone blow mold components. equivalent to Alloy 25. It has exceptional tarnish resistance MoldMAX LH® is heat treated to an optimum toughness at room temperature, and its corrosion resistance is even at a hardness of HRC 30. It has higher thermal conductivity of greater than that of Alloy 25 or ToughMet® 2. It is used for 90 BTU/ft·hr·°F (155 W/m·°C) and greater impact strength. heavily loaded bushings or bearings commonly found in It is used in place of the HH temper where faster cycles and aircraft, off-road equipment and industrial machinery. It is improved toughness are needed. often used for sour oilfield service, and is compliant to NACE MR0175/ISO 15156 with no restriction on hardness. PROtherm™ (formerly MoldMAX SC®) is a high conductivity copper beryllium alloy, with hardness around HRC 20 and a Other Alloys thermal conductivity of 145 BTU/ft·hr·°F (250 W/m·°C). It is BrushForm® 158 is a spinodally hardened copper typically used for blow
Recommended publications
  • Investigation of Mg and Zr Addition on the Mechanical Properties of Commercially Pure Al Samiul Kaiser, M
    World Academy of Science, Engineering and Technology International Journal of Mechanical and Materials Engineering Vol:13, No:9, 2019 Investigation of Mg and Zr Addition on the Mechanical Properties of Commercially Pure Al Samiul Kaiser, M. S. Kaiser stable against particle coarsening. It causes additional Abstract—The influence of Mg and Zr addition on mechanical distribution of dislocations which pin grain boundaries and properties such as hardness, tensile strength and impact energy of inhibit recrystallization. The Al3Zr particles form from the commercially pure Al are investigated. The microstructure and melt as a primary phase during rapid solidification, act as fracture behavior are also studied by using Optical and Scanning nuclei for the solidification of Al, and Zr can thus operate as Electron Microscopy. It is observed that magnesium addition improves the mechanical properties of commercially pure Al at the grain refiner of Al [13]-[15]. Based on the above point of view, Mg is added to expense of ductility due to formation of β″ (Al3Mg) and β′ (Al3Mg2) phase into the alloy. Zr addition also plays a positive role through commercially pure Al used in this study to form the binary grain refinement effect and the formation of metastable alloy. The other element Zr is subsequently added with Mg to L12 Al3Zr precipitates. In addition, it is observed that the fractured study their mutual effect on the mechanical properties of cast surface of Mg added alloy is brittle and higher numbers of dimples Al at room temperatures. are observed in case of Zr added alloy. II. EXPERIMENTAL PROCEDURE Keywords—Al-alloys, hardness, tensile strength, impact energy, microstructure.
    [Show full text]
  • UNIT 5 MODERN MACHINING METHOD Method
    Modern Machining UNIT 5 MODERN MACHINING METHOD Method Structure 5.1 Introduction Objectives 5.2 Working Principle of Energy 5.3 Non-conventional Machining Processes 5.4 Electrical Discharge Machining 5.5 Wire Cut Electric Discharge Machining 5.6 Ultrasonic Machining 5.7 Chemical Machining Processes 5.8 Electrochemical Machining 5.9 Laser Beam Machining 5.10 Plasma Arc Machining 5.11 Summary 5.12 Answers to SAQs 5.1 INTRODUCTION Modern machining methods are also named as non-conventional machining methods. These methods form a group of processes which removes excess material by various techniques involving mechanical, thermal, electrical chemical energy or combination of these energies. There is no cutting of metal with the help of metallic tool having sharp cutting edge. The major reasons of development and popularity of modern machining methods are listed below. (a) Need of machine newly developed metals and non-metals having some special properties like high strength, high hardness and high toughness. A material possing the above mentioned properties are difficult to be machined by the conventional machining methods. (b) Sometimes it is required to produce complex part geometries that cannot be produced by following conventional machining techniques. Non-conventional machining methods also provide very good quality of surface finish which may also be an encouragement to these methods. There can be a very long list of non-conventional machining methods. These methods can be classified as the basis of their base principle of working. Objectives After studying this unit, you should be able to understand introduction of modern machining methods and their difference with conventional machining methods, different classification criteria of modern machining methods and their classifications, and working principle, process details, applications and advantages and disadvantages machining.
    [Show full text]
  • 70/30 Cupronickel
    70/30 cupronickel www.columbiametals.com CN107 / C71500 / CW354H / DEF STAN 02-780 [email protected] 70/30 is a copper nickel alloy noted for its excellent resistance to corrosion, erosion and pitting combined with a good strength, workability and weldability. It has enjoyed a long and successful history in the marine sector that has since extended to industries including offshore oil and gas, power generation, desalination and cooling plants. 70/30 cupronickel The most popular specifications covering this alloy are the CN107 and C71500 designations, although the Naval Engineering specifications DEF STAN 02-780 or NES 780 offer tighter controls on impurities and mechanical properties together with a mandatory impact value. 70/30 is best renowned for its excellent corrosion and erosion resistance, especially in marine environments. Its corrosion resistance is improved in higher velocity waters (up to 4.5m/s) and polluted seawater. It is also highly resistant to stress corrosion cracking and corrosion fatigue and has a high retention of mechanical properties from sub-zero temperatures to ~300oC. In the annealed condition, 70/30 offers moderate strength levels which enable it to be used in more demanding applications. In addition, it displays inherent resistance to biofouling. A protective oxide film forms naturally over the material during the initial period of use, creating an inhospitable surface that deters marine growth. 70/30 responds well to most fabrication processes and is readily hot and cold worked. It is also easily joined by soldering, brazing and a variety of welding methods. With good hot and cold formability and a malleability approaching that of copper, 70/30 does not harden rapidly, lending the material to drawing and spinning.
    [Show full text]
  • Fire Apparatus Specifications
    CLARE FIRE DEPARTMENT FIRE APPARATUS SPECIFICATIONS CUSTOM PUMPER 1 CLARE FIRE DEPARTMENT Y___N___ INTENT OF SPECIFICATIONS It is the intent of these specifications to cover the furnishing and delivery to the Clare Fire Department of a complete fire apparatus equipped as hereinafter specified. With the view of obtaining the best results and the most acceptable apparatus for service, these specifications cover only the general requirements as to the type of construction and tests to which the apparatus must conform, together with certain details to furnish equipment and appliances with which the successful bidder must conform. Minor details of construction and materials, where not otherwise specified, are left to the discretion of the contractor who shall be solely responsible for the design and construction of all features. The NATIONAL FIRE PROTECTION ASSOCIATION pamphlet #1901 current edition for Motor Vehicle Apparatus, unless otherwise specified in these specifications shall prevail. ONLY THE SPECIFIED FIREFIGHTING SUPPORT EQUIPMENT LISTED IN THESE SPECIFICATIONS SHALL BE PROVIDED. The apparatus shall conform to all Federal motor vehicle safety standards. Bids will only be considered from companies that have an established reputation in the field of fire and/or rescue apparatus manufacturing. Each bid must be accompanied by a set of detailed contractors specifications consisting of a detailed description of the apparatus and equipment proposed. These specifications shall include size, location, type, and model of all component parts being furnished. Detailed information shall be provided on the materials used to construct all facets of the apparatus body. Any bidder who fails to submit detailed construction specifications shall be considered non-responsive and shall render their proposal ineligible for award.
    [Show full text]
  • Photochemical Machining
    Design Guide to Photochemical Machining A World Apart in a World of Parts This “Design Guide to Photochemical Machining” was cre- ated for those involved with the designing or purchasing of Fotofab uses a special process called Photochemical Machining. Also known as chemical etching, acid etching, or milling, this process metal parts. While it provides general guidelines, Fotofab’s offers many advantages over traditional metal fabrication methods: Technical Sales Staff is available to assist Speed you with your specifi c requirements. • Tooling can be produced rapidly. • Parts can be produced and shipped within hours of receiving a print. By designing with an awareness of our process capabilities, you will minimize Flexibility • Many intricate part geometries, like those found in fi ne resolution the cost and delivery time of your metal screens, can be photochemically machined easily and economically. parts. We are ready to work with you, • Revisions to part designs are implemented quickly and inexpensively. • Brittle metals, which often fracture during conventional stamping, are machined without diffi culty. Just tell us what you need! Repeatability • Prototype and production quantities can be made using the same process and tooling. Contents • Extremely thin metal can be machined without distortion; dimensional accuracy actually increases as metal thickness decreases. The Fotofab Process • page 4 • Physical properties of the metal, such as hardness, strength and formability, are not changed by the process. Value-Added Services • page 7 • Magnetically soft materials can be fabricated while retaining their optimum permeability. Applications • page 8 • Parts are inherently free of burrs. Material Selection • page 10 Cost Effectiveness • Tooling and set-up costs are extremely low compared to hard tooling.
    [Show full text]
  • Able Electropolishing
    ELECTROPOLISHING THE FINAL STEP IN PROTOTYPING ENHANCING YOUR METAL PARTS FOR ACCELERATED SPEED TO MARKET CONTENTS 01 TECHNICAL SUMMARY 03 DIRECT METAL LASER SINTERING 05 INVESTMENT CASTING 07 PHOTOCHEMICAL MACHINING 09 METAL INJECTION MOLDING 11 ELECTRICAL DISCHARGE MACHINING 14 3D PRINTING 15 LASER CUTTING 17 METAL STAMPING 19 ABOUT ABLE ELECTROPOLISHING WHAT IS ELECTROPOLISHING? // WHAT IT DOES TECHNICAL SUMMARY While the process is best known for the bright polish left on a surface, there are some important, often overlooked, benefits of this metal finishing method. These benefits include deburr- ing, size control, microfinish improvement, ultraclean finishing, corrosion resistance and others. These metal improvement Electropolishing is often referred to as a “reverse plating” process. Electrochemical in nature, benefits are highly desirable to design and production engi- electropolishing uses a combination of rectified current and a blended chemical electrolyte neers for cost savings and product lifespan improvement. bath to remove flaws from the surface of a metal part. When speed to market is critical, electropolishing offers the necessary // HOW IT WORKS part enhancements needed in the final step of production. Figure 1 The typical electropolishing installation is deceptively Since the development of electropolishing in the 1950s, substantial refinements have taken similar to a plating line. A power source converts AC current place. Able has many electrolytes to allow for electropolishing on a broad range of metals. to DC at low voltages. A rubber-lined tank, usually fabricated These newer electrolytes, combined with advanced parts handling techniques, have improved from steel, is used to hold the chemical bath. production yields on a wide range of metal products.
    [Show full text]
  • Regulations and Standards for Clean Trucks and Buses on the Right Track?
    CPB Corporate Partnership Board Regulations and Standards for Clean Trucks and Buses On the Right Track? Decarbonising Transport Regulations and Standards for Clean Trucks and Buses On the Right Track? Decarbonising Transport The International Transport Forum The International Transport Forum is an intergovernmental organisation with 62 member countries. It acts as a think tank for transport policy and organises the Annual Summit of transport ministers. ITF is the only global body that covers all transport modes. The ITF is politically autonomous and administratively integrated with the OECD. The ITF works for transport policies that improve peoples’ lives. Our mission is to foster a deeper understanding of the role of transport in economic growth, environmental sustainability and social inclusion and to raise the public profile of transport policy. The ITF organises global dialogue for better transport. We act as a platform for discussion and pre- negotiation of policy issues across all transport modes. We analyse trends, share knowledge and promote exchange among transport decision-makers and civil society. The ITF’s Annual Summit is the world’s largest gathering of transport ministers and the leading global platform for dialogue on transport policy. The Members of the Forum are: Albania, Armenia, Argentina, Australia, Austria, Azerbaijan, Belarus, Belgium, Bosnia and Herzegovina, Bulgaria, Canada, Chile, China (People’s Republic of), Croatia, Czech Republic, Denmark, Estonia, Finland, France, Georgia, Germany, Greece, Hungary, Iceland, India, Ireland, Israel, Italy, Japan, Kazakhstan, Korea, Latvia, Liechtenstein, Lithuania, Luxembourg, Malta, Mexico, Republic of Moldova, Mongolia, Montenegro, Morocco, the Netherlands, New Zealand, North Macedonia, Norway, Poland, Portugal, Romania, Russian Federation, Serbia, Slovak Republic, Slovenia, Spain, Sweden, Switzerland, Tunisia, Turkey, Ukraine, the United Arab Emirates, the United Kingdom, the United States and Uzbekistan.
    [Show full text]
  • Brazing Compilation of Literature References from 1973 to 1978
    OCTOBER 1979 BRAZING COMPILATION OF LITERATURE REFERENCES FROM 1973 TO 1978. BY J.C. RÖMER N et hf^rlfi rids E norqy R o soa re h \ oundation ECN does not assume any liability with respect to the use of, or for damages resulting from the use of any information, apparatus, method or process disclosed in this document. Netherlands Energy Research Foundation ECN P.O. Box 1 1755 ZG Petf.n(NH) The Netherlands Telephone (0)2246 - 62».. Telex 57211 ECN-7* OCTOBER 1979 BRAZING COMPILATION OF LITERATURE REFERENCES FROM 1973 T01978. BY J.C. ROMER -2- ABSTRACT This report is a compilation of published literature on high temperature brazing covering the period 1973-1978. The references are listed alphabetically with regard to the base material or combination of base materials to be brazed. Trade names are treated as base materials. The report contains approximately 1500 references, of which 300 are to patents. KEYWORDS BRAZING BRAZING ALLOYS FILLER METALS JOINING - 3 CONTENTS ABSTRACT 1. ALUMINIUM 2. ALUMINIUM (FLVXLESS) 3. ALUMINIUM - BERYLLIUM 4. ALUMINIUM/BORON COMPOSITES 5. ALUMINIUM - COPPER 5.1. Aluminium - graphite 5.2. Aluminium - nickel alloys 5.3. Aluminium - niobium 5.4. Aluminium ~ molyldenum 5.5. Aluminium - stainless steel 5.6. Aluminium - steels 5.7. Aluminium - tantalum 5.8. Aluminium - titanium 5.9. Aluminium - tungsten 6. BERYLLIUM 7. BORONNITRIDE• 8. BRASS 8.1. Brass - aluminium 8.2. Brass - steels 9. BRONZE 9.1. Bronze - stainless steels 10. CERAMICS 10.1. Ceramics - metal - 4 - CERMETS 61 11.1. Cermets - stainless steels 62 COBALT 63 COPPER ALLOYS 64 13.1. Copper alloys - brass 68 13.2.
    [Show full text]
  • Chemical Machining and Milling
    CHEMICAL MACHINING AND MILLING Introduction Chemical machining (CM) is the controlled dissolution of workpiece material (etching) by means of a strong chemical reagent (etchant). In CM material is removed from selected areas of workpiece by immersing it in a chemical reagents or etchants; such as acids and alkaline solutions. Material is removed by microscopic electrochemical cell action, as occurs in corrosion or chemical dissolution of a metal. This controlled chemical dissolution will simultaneously etch all exposed surfaces even though the penetration rates of the material removal may be only 0.0025–0.1 mm/min. The basic process takes many forms: chemical milling of pockets, contours, overall metal removal, chemical blanking for etching through thin sheets; photochemical machining (pcm) for etching by using of photosensitive resists in microelectronics; chemical or electrochemical polishing where weak chemical reagents are used (sometimes with remote electric assist) for polishing or deburring and chemical jet machining where a single chemically active jet is used. A schematic of chemical machining process is shown in Figure 6. Figure 6: (a) Schematic of chemical machining process (b) Stages in producing a profiled cavity by chemical machining (Kalpakjain & Schmid) Chemical milling In chemical milling, shallow cavities are produced on plates, sheets, forgings and extrusions. The two key materials used in chemical milling process are etchant and maskant. Etchants are acid or alkaline solutions maintained within controlled ranges of chemical composition and temperature. Maskants are specially designed elastomeric products that are hand strippable and chemically resistant to the harsh etchants. Steps in chemical milling Residual stress relieving: If the part to be machined has residual stresses from the previous processing, these stresses first should be relieved in order to prevent warping after chemical milling.
    [Show full text]
  • X-Ray Diffraction Studies of 145 Mev Proton-Irradiated Albemet 162
    X-Ray Diffraction Studies of 145 MeV proton-irradiated AlBeMet 162 Mohamed Elbakhshwan1, Kirk T. McDonald2, Sanjit Ghose3, Zhong Zhong3, Nikolaos Simos1,3* 1Nuclear Science and Technology Department, Brookhaven National Laboratory, Upton, NY 11973 2Joseph Henry Laboratories, Princeton University, Princeton, NJ 08544 3National Synchrotron Light Source II, Brookhaven National Laboratory, Upton, NY 11973 Abstract AlBeMet 162 (Materion Co., formerly Brush Wellman) has been irradiated with 145 MeV protons up to 1.2x1020 cm-2 fluence, with irradiation temperatures in the range of 100-220oC. Macroscopic post- irradiation evaluation on the evolution of mechanical and thermal properties was integrated with a comprehensive x-ray- diffraction study using high-energy monochromatic and polychromatic x-ray beams, which offered a microscopic view of the irradiation damage effects on AlBeMet. The study confirmed the stability of the metal-matrix composite, its resistance to proton damage, and the continuing separation of the two distinct phases, fcc aluminum and hcp beryllium, following irradiation. Furthermore, based on the absence of inter-planar distance change during proton irradiation, it was confirmed that the stacking faults and clusters on the Al (111) planes are stable, and thus can migrate from the cascade region and be absorbed at various sinks. XRD analysis of the unirradiated AlBeMet 162 showed clear change in the texture of the fcc phase with orientation especially in the Al (111) reflection which exhibits a “non-perfect” six-fold symmetry, implying lack of isotropy in the composite. * Corresponding author Tel.: +1 631 344 7229 E-mail address: [email protected] 1. Introduction AlBeMet, an aluminum-beryllium compound with high Be content, is better described as a metal-matrix composite rather than an alloy, since the two metals remain as separate phases.
    [Show full text]
  • A Survey of Al7075 Aluminium Metal Matrix Composites
    International Journal of Science and Research (IJSR) ISSN (Online): 2319-7064 Index Copernicus Value (2013): 6.14 | Impact Factor (2013): 4.438 A Survey of Al7075 Aluminium Metal Matrix Composites Rajendra .S .K1, Ramesha .C .M2 1Research Scholar, Jain University, Bengaluru, Department of Industrial Engineering and Management, Dr. Ambedkar Institute of Technology, Bengaluru 2Department of Mechanical Engineering, M S Ramaiah Institute of Technology, Bengaluru Abstract:A composite material is a combination of two or more chemically distinct and insoluble phases; its properties and structural performance are superior to those of the constituents acting independently. Metals and ceramics, as well, can be embedded with particles or fibers, to improve their properties; these combinations are known as Metal-Matrix composites. Aluminum 7075 alloy constitutes a very important engineering material widely employed in the aircraft and aerospace industry for the manufacturing of different parts and components. It is due to its high strength to density ratio that it a sought after metal matrix composite. In this paper we present a survey of Al 7075 Metal Matrix Composites. Keywords: Metal Matrix Composites (MMC’s), Aluminium Metal Matrix, Beryl, Al7075, Aluminium alloy 1. Introduction Aluminium alloy 7075 is an aluminium alloy, with zinc as the primary alloying element. It is strong, with a strength The effects of research in Aluminium based Metal Matrix comparable to many steels, and has good fatigue strength and Composites (MMC’s) are far reaching these days. These average machinability, but has less resistance to corrosion composites find various applications in the automobile than many other Al alloys. Its relatively high cost limits its industry, the aerospace industry and in defence and marine use to applications where cheaper alloys are not suitable.
    [Show full text]
  • The Effect of Heat Treatment on Precipitation in the Cu-Ni-Al Alloy Hiduron®
    Materials Science & Engineering A 692 (2017) 192–198 Contents lists available at ScienceDirect Materials Science & Engineering A journal homepage: www.elsevier.com/locate/msea ff ® The e ect of heat treatment on precipitation in the Cu-Ni-Al alloy Hiduron MARK 130 ⁎ Katerina A. Christofidoua, ,1, K. Jennifer Robinsona, Paul M. Mignanellia, Ed J. Pickeringb, Nicholas G. Jonesa, Howard J. Stonea a Department of Materials Science and Metallurgy, University of Cambridge, 27 Charles Babbage Road, Cambridge CB3 0FS, UK b School of Materials, The University of Manchester, Manchester M13 9PL, UK ARTICLE INFO ABSTRACT Keywords: Cupronickel alloys, reinforced by L12 precipitates, offer a high strength, corrosion resistant and anti-bio fouling Copper alloys material for marine engineering applications. These alloys exhibit complex precipitate nucleation and growth L12 phase mechanisms that must be fully understood in order to optimise the mechanical properties. In this work, the Microstructure microstructural characteristics of the Cu-Ni-Al based alloy, Hiduron® 130, have been assessed in the as-received SEM condition and following 100-h thermal exposures at 500, 600, 700 and 900 °C and after a two-stage exposure at TEM 900 °C for 100 h followed by 500 °C for 100 h. The L1 phase was observed to precipitate both discontinuously XRD 2 and continuously and its subsequent coarsening was characterised alongside measurements of the lattice misfit. The hardness of the alloy was found to decrease with increasing exposure temperature up to the L12 solvus and correlated with the evolution of the L12 precipitates, the alloy grain size and the fraction of the discontinuously formed L12 phase.
    [Show full text]