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Characteristics of Al-Si Alloys with High Melting Point Elements for High Pressure Die Casting
materials Article Characteristics of Al-Si Alloys with High Melting Point Elements for High Pressure Die Casting Tomasz Szymczak 1,* , Grzegorz Gumienny 1,* , Leszek Klimek 2 , Marcin Goły 3 , Jan Szymszal 4 and Tadeusz Pacyniak 1 1 Department of Materials Engineering and Production Systems, Lodz University of Technology, 90-924 Lodz, Poland; [email protected] 2 Institute of Materials Science and Engineering, Lodz University of Technology, 90-924 Lodz, Poland; [email protected] 3 Department of Physical & Powder Metallurgy, AGH University of Science and Technology, 30-059 Krakow, Poland; [email protected] 4 Department of Technical Sciences and Management, University of Occupational Safety Management in Katowice, 40-007 Katowice, Poland; [email protected] * Correspondence: [email protected] (T.S.); [email protected] (G.G.); Tel.: +48-426312276 (T.S.); +48-426312264 (G.G.) Received: 9 October 2020; Accepted: 29 October 2020; Published: 29 October 2020 Abstract: This paper is devoted to the possibility of increasing the mechanical properties (tensile strength, yield strength, elongation and hardness) of high pressure die casting (HPDC) hypoeutectic Al-Si alloys by high melting point elements: chromium, molybdenum, vanadium and tungsten. EN AC-46000 alloy was used as a base alloy. The paper presents the effect of Cr, Mo, V and W on the crystallization process and the microstructure of HPDC aluminum alloy as well as an alloy from the shell mold. Thermal and derivative analysis was used to study the crystallization process. The possibility of increasing the mechanical properties of HPDC hypoeutectic alloy by addition of high-melting point elements has been demonstrated. -
Case File Copy
NTS 31493 NASA CR-121221 CASE FILE COPY CHARACTERIZATION OF THE MECHANICAL AND PHYSICAL PROPERTIES OF TD-NiCr (Ni-20Cr-2ThO2) ALLOY SHEET by L. J. Fritz, W. P. Koster, and R. E. Taylor* METCUT RESEARCH ASSOCIATES INC. *THERMOPHYSICAL PROPERTIES RESEARCH CENTER prepared for NATIONAL AERONAUTICS AND SPACE ADMINISTRATION NASA Lewis Research Center Contract NAS3-15558 1 Report No. 2. Government Accession No. 3. Recipient's Catalog No. NASA CR- 12 1221 4. Title and Subtitle 5. Report Date Characterization of the Mechanical and Physical Properties of TD-NiCr (Ni-20Cr-2ThO2 ) Alloy 6. Performing Organization Code Sheet 7. Authof(s) 8. Performing Organization Report No. L. J. Fritz- W. P. Koster, and R. E. Taylor 10. Work Unit No. 9. Performing Organization Name and Address Metcut Research Associates Inc. 11. Contract or Grant No. 3980 Rosslyn Drive NAS3-15558 Cincinnati, OH 45209 13. Type of Report and Period Covered 12. Sponsoring Agency Name and Address National Aeronautics and Space Administration 14. Sponsoring Agency Code Washington, D.C. 20546 15. Supplementary Notes Project Manager, John D. Whittenberger, Materials and Structures Division, NASA Lewis Research Center, Cleveland, OH 16. Abstract Sheets of TD-NiCr processed using techniques developed to produce uniform material were tested to supply mechanical and physical property data. Two heats each of 0. 025 and 0. 051 cm thick sheet were tested. Mechanical properties evaluated included tensile, modulus of elasticity, Poisson's Ratio, compression, creep-rupture, creep strength, bearing strength, shear strength, sharp notch and fatigue strength. Test temperatures covered the range from ambient to 1589K. Physical properties were also studied as a function of temperature. -
Metallurgical Abstracts (General and Non-Ferrous)
METALLURGICAL ABSTRACTS (GENERAL AND NON-FERROUS) Volume 2 1935 Part 13 I —PROPERTIES OF METALS (Continued from pp. 553-568.) Refined Aluminium. Robert GaDeau (Metallurgist (Suppt. to Engineer), 1936, 11, 94-96).—Summary of a paper presenteD to the Congrès Inter nationale Des Mines, De la Métallurgie, et De la Géologie Appliquée, Paris. See Met. Abs., this vol., pp. 365 anD 497.—R. G. _ On the Softening and Recrystallization of Pure Aluminium. ------ (A lu minium, 1935, 17, 575-576).—A review of recent work of Calvet anD his collaborators ; see Met. Abs., this vol., pp. 453, 454. A. R. P. *Some Optical Observations on the Protective Films on Aluminium in Nitric, Chromic, and Sulphuric Acids. L. TronstaD anD T. HbverstaD (Trans. Faraday Soc., 1934, 30, 362-366).—The optical properties of natural films on aluminium were measureD in various solutions anD their change with time of immersion observeD. Little change occurs in such films in chromic aciD solutions with or without chloriDe ; the films are not protective in concentrateD sulphuric aciD, anD in concentrateD nitric aciD the protective films are alternately DissolveD anD re-formeD. The mean thickness of natural films on aluminium is 100 p. or more than 10 times as thick as those on iron.—A. R. P. *Light from [Burning] Aluminium and Aluminium-Magnésium [Alloy], J. A. M. van Liempt anD J. A. De VrienD (Bee. trav. chim., 1935, 54, 239-244). „ . —S. G. ’"Investigations Relating to Electrophotophoresis Exhibited by Antimony Gisela Isser anD AlfreD Lustig (Z . Physik, 1935, 94, 760-769).—UnchargeD submicroscopic particles subjecteD to an electric fielD in an intense beam of light are founD to move either in the Direction of, or against, the fielD. -
Machining of Aluminum and Aluminum Alloys / 763
ASM Handbook, Volume 16: Machining Copyright © 1989 ASM International® ASM Handbook Committee, p 761-804 All rights reserved. DOI: 10.1361/asmhba0002184 www.asminternational.org MachJning of Aluminum and AlumJnum Alloys ALUMINUM ALLOYS can be ma- -r.. _ . lul Tools with small rake angles can normally chined rapidly and economically. Because be used with little danger of burring the part ," ,' ,,'7.,','_ ' , '~: £,~ " ~ ! f / "' " of their complex metallurgical structure, or of developing buildup on the cutting their machining characteristics are superior ,, A edges of tools. Alloys having silicon as the to those of pure aluminum. major alloying element require tools with The microconstituents present in alumi- larger rake angles, and they are more eco- num alloys have important effects on ma- nomically machined at lower speeds and chining characteristics. Nonabrasive con- feeds. stituents have a beneficial effect, and ,o IIR Wrought Alloys. Most wrought alumi- insoluble abrasive constituents exert a det- num alloys have excellent machining char- rimental effect on tool life and surface qual- acteristics; several are well suited to multi- ity. Constituents that are insoluble but soft B pie-operation machining. A thorough and nonabrasive are beneficial because they e,,{' , understanding of tool designs and machin- assist in chip breakage; such constituents s,~ ,.t ing practices is essential for full utilization are purposely added in formulating high- of the free-machining qualities of aluminum strength free-cutting alloys for processing in alloys. high-speed automatic bar and chucking ma- Strain-hardenable alloys (including chines. " ~ ~p /"~ commercially pure aluminum) contain no In general, the softer ailoys~and, to a alloying elements that would render them lesser extent, some of the harder al- c • o c hardenable by solution heat treatment and ,p loys--are likely to form a built-up edge on precipitation, but they can be strengthened the cutting lip of the tool. -
Aluminium Alloys Chemical Composition Pdf
Aluminium alloys chemical composition pdf Continue Alloy in which aluminum is the predominant lye frame of aluminum welded aluminium alloy, manufactured in 1990. Aluminum alloys (or aluminium alloys; see spelling differences) are alloys in which aluminium (Al) is the predominant metal. Typical alloy elements are copper, magnesium, manganese, silicon, tin and zinc. There are two main classifications, namely casting alloys and forged alloys, both further subdivided into heat-treatable and heat-free categories. Approximately 85% of aluminium is used for forged products, e.g. laminated plates, foils and extrusions. Aluminum cast alloys produce cost-effective products due to their low melting point, although they generally have lower tensile strength than forged alloys. The most important cast aluminium alloy system is Al–Si, where high silicon levels (4.0–13%) contributes to giving good casting features. Aluminum alloys are widely used in engineering structures and components where a low weight or corrosion resistance is required. [1] Alloys composed mostly of aluminium have been very important in aerospace production since the introduction of metal leather aircraft. Aluminum-magnesium alloys are both lighter than other aluminium alloys and much less flammable than other alloys containing a very high percentage of magnesium. [2] Aluminum alloy surfaces will develop a white layer, protective of aluminum oxide, if not protected by proper anodization and/or dyeing procedures. In a wet environment, galvanic corrosion can occur when an aluminum alloy is placed in electrical contact with other metals with a more positive corrosion potential than aluminum, and an electrolyte is present that allows the exchange of ions. -
International Alloy Designations and Chemical Composition Limits for Wrought Aluminum and Wrought Aluminum Alloys
International Alloy Designations and Chemical Composition Limits for Wrought Aluminum and Wrought Aluminum Alloys 1525 Wilson Boulevard, Arlington, VA 22209 www.aluminum.org With Support for On-line Access From: Aluminum Extruders Council Australian Aluminium Council Ltd. European Aluminium Association Japan Aluminium Association Alro S.A, R omania Revised: January 2015 Supersedes: February 2009 © Copyright 2015, The Aluminum Association, Inc. Unauthorized reproduction and sale by photocopy or any other method is illegal . Use of the Information The Aluminum Association has used its best efforts in compiling the information contained in this publication. Although the Association believes that its compilation procedures are reliable, it does not warrant, either expressly or impliedly, the accuracy or completeness of this information. The Aluminum Association assumes no responsibility or liability for the use of the information herein. All Aluminum Association published standards, data, specifications and other material are reviewed at least every five years and revised, reaffirmed or withdrawn. Users are advised to contact The Aluminum Association to ascertain whether the information in this publication has been superseded in the interim between publication and proposed use. CONTENTS Page FOREWORD ........................................................................................................... i SIGNATORIES TO THE DECLARATION OF ACCORD ..................................... ii-iii REGISTERED DESIGNATIONS AND CHEMICAL COMPOSITION -
Alloys for Aeronautic Applications: State of the Art and Perspectives
metals Review Alloys for Aeronautic Applications: State of the Art and Perspectives Antonio Gloria 1, Roberto Montanari 2,*, Maria Richetta 2 and Alessandra Varone 2 1 Institute of Polymers, Composites and Biomaterials, National Research Council of Italy, V.le J.F. Kennedy 54-Mostra d’Oltremare Pad. 20, 80125 Naples, Italy; [email protected] 2 Department of Industrial Engineering, University of Rome “Tor Vergata”, 00133 Rome, Italy; [email protected] (M.R.); [email protected] (A.V.) * Correspondence: [email protected]; Tel.: +39-06-7259-7182 Received: 16 May 2019; Accepted: 4 June 2019; Published: 6 June 2019 Abstract: In recent years, a great effort has been devoted to developing a new generation of materials for aeronautic applications. The driving force behind this effort is the reduction of costs, by extending the service life of aircraft parts (structural and engine components) and increasing fuel efficiency, load capacity and flight range. The present paper examines the most important classes of metallic materials including Al alloys, Ti alloys, Mg alloys, steels, Ni superalloys and metal matrix composites (MMC), with the scope to provide an overview of recent advancements and to highlight current problems and perspectives related to metals for aeronautics. Keywords: alloys; aeronautic applications; mechanical properties; corrosion resistance 1. Introduction The strong competition in the industrial aeronautic sector pushes towards the production of aircrafts with reduced operating costs, namely, extended service life, better fuel efficiency, increased payload and flight range. From this perspective, the development of new materials and/or materials with improved characteristics is one of the key factors; the principal targets are weight reduction and service life extension of aircraft components and structures [1]. -
PBM-2020-CATALOG-1 Layout 1
LEGAL NOTICES PBM PERFORMANCE PRODUCTS LIMITED ONE YEAR WARRANTY LIMITED WARRANTY There is absolutely no warranty on the following: PBM Performance Products warrants that all of its prod- 1) Any parts used in racing applications ucts are free from defects in material and workmanship, 2) Any product that has been physically and against excessive wear for a period of 12 months altered, improperly installed or main- from date of purchase. Due to the nature of modifications tained; made on performance engines that may affect perform- 3) Any product used in improper applica- ance, economy and engine life, PBM Performance Prod- tions, abused, or not used in conjunc ucts’ obligation under this warranty is limited to the repair tion with the proper parts. or replacement, only of PBM Performance Products, when the consumer returns these PBM products to : There are no implied warranties of merchantability 7301 Global Drive, Louisville, KY 40258. PBM Per- or fitness for a particular purpose. There are no war- formance Products retains sole discretion in determining ranties, which extend beyond the description of the defective merchandise and assumes no responsibility for face hereof. PBM Performance Products will not be re- diagnosis, removal, and/or installation labor, inconven- sponsible for incidental and consequential damages, ience or any other damages or expenses including tow- property damage or personal injury damages to the ex- ing. There is absolutely no warranty, implied or tent permitted by law. Where required by law, implied otherwise, on PBM Performance Products used in com- warranties of merchantability and fitness are limited for petition (racing) engine applications. -
Bibliography and Index on Vacuum And
NATL INST OF STANDARDS & TECH R.I.C. All 100988737 /NBS monograph QC100 .U556 W5;SUPP1;1967 C.I NBS-PUB-C NBS PUBLICATIONS NBS MONOGRAPH 35—Supplement 1 Bibliography and Index on Vacuum and Low Pressure IVIeasurement January 1960 to December 1965 U.S. DEPARTMENT OF COMMERCE NATIONAL BUREAU OF STANDARDS — THE NATIONAL BUREAU OF STANDARDS The National Bureau of Standards^ provides measurement and technical information services essential to the efficiency and effectiveness of the work of the Nation's scientists and engineers. The Bureau serves also as a focal point in the Federal Government for assuring maximum application of the physical and engineering sciences to the advancement of technology in industry and commerce. To accomplish this mission, the Bureau is organized into three institutes covering broad program areas of research and services: THE INSTITUTE FOR BASIC STANDARDS . provides the central basis within the United States for a complete and consistent system of physical measurements, coordinates that system with the measurement systems of other nations, and furnishes essential services leading to accurate and uniform physical measurements throughout the Nation's scientific community, industry, and commerce. This Institute comprises a series of divisions, each serving a classical subject matter area: —Applied Mathematics—Electricity—Metrology—Mechanics—Heat—Atomic Physics—Physical Chemistry—Radiation Physics—Laboratory Astrophysics-—Radio Standards Laboratory,^ which includes Radio Standards Physics and Radio Standards Engineering- -Office of Standard Refer- ence Data. THE INSTITUTE FOR MATERIALS RESEARCH . conducts materials research and provides associated materials services including mainly reference materials and data on the properties of ma- terials. Beyond its direct interest to the Nation's scientists and engineers, this Institute yields services which are essential to the advancement of technology in industry and commerce. -
Adams Catalog 6.20 W.Pdf
Magnetic products for engineering performance, innovation and design. Magnetic products for engineering performance, innovation and design. Founded in 1950, Adams Magnetic Products is a custom manufacturer, fabricator and distributor of all types of permanent magnets, magnetic assemblies and devices. Our technical experts are ready to answer your questions Military and Defense Materials and address your magnetic needs. Whether it’s selecting Adams Magnetic Products has the knowledge, understanding a magnet to fit an application, choosing the most cost and systems in place to fully comply with the Arms Export effective material or reviewing options from what is Control Act (AECA) and International Traffic in Arms available in the market, we are here to help with: Regulations (ITAR). We are your partner in fabricating magnets and magnetic products for the defense and • Application and Design Engineering Assistance military industries. As an ITAR registered supplier, you can • Testing/Analysis of Magnetic Materials rest assured your data and confidential information is safe • Magnetic Circuit Analysis/FEA with us. We are also your source for Defense Acquisition • Value Analysis/Value Engineering Support Regulations System (DFARS) compliant materials. Let our technical staff assist you in obtaining the right materials • Inventory Management Programs for your DoD needs. A Commitment to Value We define value as having the right products available at the right time and delivering them as promised, defect-free, at competitive prices. Adams is committed to delivering outstanding value to customers at every opportunity. Certified Quality Management Adams maintains ISO 9001:2015 certification, reinforcing our strong operational processes and commitment to continual improvement. We have a standard of zero defects in everything we do. -
2000 TMS Annual Meeting Program
TECHNICAL PROGRAM 12 9 thTMS ANNUAL MEETING & The 129th TMS Annual Meeting & Exhibition EXHIBITION Opryland Convention Center ❈ ❈ ❈ Nashville, Tennessee USA ❈ ❈ ❈ March 12 - March 16, 2000 MONDAY AM the cost of these increasingly complex materials. This paper will re- AIME/TMS KEYNOTE ADDRESS view some of the work currently being undertaken both at engine "FutureView...A Look Ahead" manufacturers, and at component suppliers in consortia such as the AM MONDAY Daniel Burrus Engine Supplier Base Initiatives and the Metals Affordability Initia- 11:30am-1:00pm tive. The creation of such consortia to reduce component cost has Convention Center, Presidential Ballroom made significant progress possible in focusing the entire supply chain ✦✦✦ and the customer on this critical issue of affordability Tutorial Luncheon Lecture 8:55 AM Invited "Advanced Rechargeable Batteries: A Materials Science Perspective" Application of Lean Concepts to the Aerospace Forging Value Donald R. Sadoway Stream: Dan Krueger1; Rod Boyer2; David Furrer3; Mary Lee 12:00noon-1:30pm Gambone4; Beth Lewis5; 1GE Aircraft Engines, One Neumann Way, Convention Center, Lincoln C MD H85, Cincinnati, OH 45215 USA; 2Boeing Company, Commercial ✦✦✦ Airplanes Grp., Seattle, WA 98124 USA; 3Ladish Company, Inc., 5481 AIME & TMS Banquet & Awards Presentation S. Packard Ave., Cudahy, WI 53110 USA; 4Rolls-Royce Allison, P.O. 6:00pm Reception Box 420, Indianapolis, IN 46206-0420 USA; 5Wyman Gordon Com- 7:00pm Dinner pany, 244 Worcester St., Grafton, MA 01563 USA Convention Center, Presidential Ballroom Forged components comprise approximately one-third the cost of a propulsion system, and are major cost drivers for airframe systems. +Indicates Student Traditionally, cost reduction efforts have focused on improving indi- vidual operations or steps in the value stream. -
Metal Matrix Composites: History, Status
METAL MATRIX COMPOSITES: HISTORY, STATUS, FACTORS AND FUTURE By AJITH JAMES CYRIAC Bachelor of Technology in Mechanical Engineering Cochin University of Science and Technology Cochin, Kerala, INDIA 2005 Submitted to the Faculty of the Graduate College of the Oklahoma State University in partial fulfillment of the requirements for the Degree of MASTER OF SCIENCE July 2011 METAL MATRIX COMPOSITES: HISTORY, STATUS, FACTORS AND FUTURE Thesis Approved: Dr. Jay C. Hanan Thesis Adviser Dr. Sandip P. Harimkar Dr. Ranji Vaidyanathan Dr. Mark E. Payton Dean of the Graduate College ii ACKNOWLEDGMENT As I sit down to write this page, I am filled with a great feeling of gratitude towards so many individuals who have made this endeavor possible. Above all, I would like to thank my thesis and academic advisor Dr. Jay C. Hanan for accepting me to his team and helping me with his kindness and patience throughout the project. Initially I was reluctant to take the task of doing a thesis, but his confidence in my abilities and the motivation from him and motivated me to take on such a great endeavor. I wish to thank Dr. Ranji Vaidyanathan and Dr. Sandip Harimkar for being part of my committee. I would like to thank our graduate coordinator Dr.Afshin Ghajar and his assistant Shelli Stapleton for supporting me throughout the program. I specially need to acknowledge help I received from the Kevin Drees of Edmon Low Library and Dona Donldson of O.S.U Tulsa Library for their assistance. I do not have any qualms in admitting that I would not be able to finish this project without their help.