2.7 Aluminum – Copper Alloys:
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Hiduminium Technical Data
HIDUMINIUM TECHNICAL DATA HIGH DUTY ALLOYS LTD SLOUGH F oreword Extensive research carried out in recent years, com bined with an increasing demand for " H ID UM IN IUM " high tensile aluminium alloys, has necessitated the revision and increase of the series of data sheets pre viously issued by the Company. As before, our aim is to place before designers and constructors the fullest possible particulars regarding the physical and mechanical properties of " H ID U M IN IU M ," which will enable them to select the materials most suitable for their requirements and to adapt their designs in accordance with the outstanding character istics of this range of alloys. " HIDUMINIUM" is produced under conditions of strict scientific control and progressive inspection and a staff of expert Metallurgists, Research W orkers and Technicians is always ready to give advice on all problems connected with the use of these alloys. Fresh data, as it is revealed by further research, will be issued on additional sheets. This will ensure that all information contained in this volume is up-to-date and may thus be referred to at all times with complete confidence. HIGH DUTY ALLOYS LIMITED 3 CONTENTS Page Index to Specifications 6-9 Hiduminium 15 10-11 Hiduminium 23 12-13 Hiduminium 33 14-15 Hiduminium 35 16-17 H iduminium 40 & 42 18-19 Hiduminium 45 20-21 Hiduminium R.R. 50 22-23 Hiduminium R.R. 53 24-26 Hiduminium R.R. 53.C 27-29 Hiduminium R.R. 56 30-32 H iduminium R.R. 59 33-35 Hiduminium 72 36-37 Hiduminium R.R. -
Parshwamani Metals
+91-8048554624 Parshwamani Metals https://www.indiamart.com/parshwamanimetals/ Parshwamani Metals is one of the leading manufacturers, supplier and traders of Industrial Metal Tube, Beryllium Product, Shim Sheet, SS Round And Square Bar, Aluminium Products, Aluminum Bronze Products etc. About Us Parshwamani Metals was established in the year 2015 as a professionally managed Manufacturer, Trader and Wholesaler specialized in providing premium grade Copper and Brass Metals Products. Today, we endeavor to revolutionize the industry by fabricating a wide gamut of quality products, which includes Brass Products, Copper Products and Copper Alloy. Our claim to success is hallmarked by the offered quality products that gained us huge recognizance for its high strength, wear and tear resistance, accurate dimensions, flexibility and durable finish. Our products find their wide applications in architectural fittings, hardware and telecommunication. Owing to swift delivery schedules, easy payment modes and overt business practices, we have been successful in earning huge client base. We deal in Jindal Brand. Our efforts are determined with the objective of industrial leadership that equips our team members to manufacture customized products. And, to achieve this, we have developed modernized R&D centers and cutting edge manufacturing facilities. Furthermore, the facility is divided into various functional units like procurement, engineering, production, research & development, quality-testing, warehousing & packaging etc. Our organization is backed -
Linear) Thermal Expansion for Selected Materials (COE Or CTE
Appendix 1: Coefcient of (Linear) Thermal Expansion for Selected Materials (COE or CTE) Coefficient of (linear) thermal expansion, α, for selected (continued) − − materials (COE or CTE) (units are ×10 6 °C 1 (i.e. ppm/°C)) Indium–lead 33.0 Lead (95 %) tin solder 28.0 Tin–lead solder 60/40 25.0 A. Pure metals Magnesium, AZ31B 26.0 Aluminium 25 Ni-clad Molybdenum 5–6 Chromium 6 Steel, 1020 12.0 Cobalt 12 Stainless steel (18-8) 17.0 Copper 17 Tungsten/copper (90/10) 6.5 Gold 14 Aluminium MMC with SiC particles 6–14 Iron 12 (80–50 % reinforcement) Lead 29 C. Insulators and substrate materials (for electronic systems)a Magnesium 25 E glass 5.5 Molybdenum 5 S glass 2.6 Nickel 13 Glass–ceramic >3.0 Platinum 9 Silicon 2.6 Silver 19 Diamond 0.9 Tantalum 7 Aluminium nitride 4.5 Tin 20 Silicon nitride 3.7 Titanium 9 Quartz, fused silica 0.5 Tungsten 5 Kevlar 49 –5 Zinc 35 Beryllia 6–9 B. Alloys and MMCs Cubic boron nitride Alloy 42 4.4 x–y 3.7 Aluminium (40 % silicon) 13.5 z 7.2 Aluminium, AA 6061 23.6 E glass/epoxy Aluminium, AA 3003 23.2 x–y 14–17 Aluminium, AA 2017 22.9 z 80–280 Boron aluminium (20 %) 12.7 E glass/polyimide Brass 18.0 x–y 12–16 Copper/invar/copper 20/60/20 thick 5.8 z 40–80 Copper/molybdenum/copper 20/60/20 7.0 E glass/PTFE thick x–y 24 Graphite/aluminium 4–6 z 260 Invar 36 1.6 Kevlar/epoxy Invar 42 4.5 x–y 5–7 Inconel 600 13.0 z 70 Kovar (Fe–Ni–Co) 5.0 (continued) Kevlar/polyimide (continued) © Springer International Publishing Switzerland 2016 557 B.D. -
924 Iaea-Sm-310/ 69P
924 IAEA-SM-310/ 69P RESULTS FROM POST-MORTEM TESTS WITH MATERIAL FROM THE OLD CORE-BOX OF THE HIGH FLUX REACTOR (HFR) AT PETTEN M.I. de Vries Netherlands Energy Research Foundation, ECN, Eetten, The Netherlands M.R.. Cundy Joint Research Centre, Patten, The Netherlands 925 RESULTS FROM POST-MORTEM TESTS WITH MATERIAL FROM THE OLD CORE-BOX OF THE HIGH FLUX REACTOR (HFR) AT PETTEN ABSTRACT Results are reported from hardness measurements, tensile tests and fracture mechanics experiments (fatigue crack growth and fracture toughness) on 5154 aluminium specimens, fabricated from remnants of the old HFR core box. The specimen material was exposed to a maximum thermal neutron fluence of 7.5 * 1026n/m2(E < 0.4eV). Test results for this fluence (ratio of the thermal to fast neutron flux density is 1.17) are: hardness 63HR15N, 0.2 - yield strength 525 MPa and total elongation 2.2% strain. Material which was exposed to a lower thermal fluence of 5.6 * 10 n/m , but with a thermal to fast neutron ratio of about 4, shows more radiation hardening : 67HR15N, 0.2 - yield strength 580 MPa and 1.5% total elongation. -5 -3 Fatigue crack growth rates range from 5 * 10 mm/cycle to 10 mm/cycle for AK ranging from 8 to 20 MPa)|m. The most highly exposed (7.5 * 10 n/m ) material shows accelerated fatigue crack growth due to unstable crack extension at AK of about 15 Mpa^m. The lowermost meaningful measure of plane strain fracture toughness is 18 MPa^m. Except for the fracture toughness which is a factor of about 3 higher the results show reasonable agreement with the expected mechanical properties estimated in the "safe end-of-life" assessment of the old HFR vessel. -
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. -
Heat Treating of Aluminum Alloys
ASM Handbook, Volume 4: Heat Treating Copyright © 1991 ASM International® ASM Handbook Committee, p 841-879 All rights reserved. DOI: 10.1361/asmhba0001205 www.asminternational.org Heat Treating of Aluminum Alloys HEAT TREATING in its broadest sense, • Aluminum-copper-magnesium systems The mechanism of strengthening from refers to any of the heating and cooling (magnesium intensifies precipitation) precipitation involves the formation of co- operations that are performed for the pur- • Aluminum-magnesium-silicon systems herent clusters of solute atoms (that is, the pose of changing the mechanical properties, with strengthening from Mg2Si solute atoms have collected into a cluster the metallurgical structure, or the residual • Aluminum-zinc-magnesium systems with but still have the same crystal structure as stress state of a metal product. When the strengthening from MgZn2 the solvent phase). This causes a great deal term is applied to aluminum alloys, howev- • Aluminum-zinc-magnesium-copper sys- of strain because of mismatch in size be- er, its use frequently is restricted to the tems tween the solvent and solute atoms. Conse- specific operations' employed to increase quently, the presence of the precipitate par- strength and hardness of the precipitation- The general requirement for precipitation ticles, and even more importantly the strain hardenable wrought and cast alloys. These strengthening of supersaturated solid solu- fields in the matrix surrounding the coher- usually are referred to as the "heat-treat- tions involves the formation of finely dis- ent particles, provide higher strength by able" alloys to distinguish them from those persed precipitates during aging heat treat- obstructing and retarding the movement of alloys in which no significant strengthening ments (which may include either natural aging dislocations. -
850°C. Sp. Gray. 3.75 ; S. Ht. .068. Obtained in the Pure State
126 NEWNES PRACTICAL MECHANICS December, 1939 greenish -yellow appearance. In English cent. ; tin, 2.5 per cent. ; zinc, 7.1 per cent. per alloys recently introduced in America. standard gold the silver is replaced by Sometimes about .5per cent. of alu- Typical composition :silver,70.44 per copper. minium is also added. cent.; copper, 28.90 per cent. ; beryllium, Autogenous Soldering. -The uniting of twoBearings Metals. -See Anti -friction Metals. .87 per cent. Used as a resistance -wire pieces of metal together simply by meltingBell Metal. -A type of bronze or copper -tin. material. their edges by means of a blowlamp or alloy containing from 12 to 24 per cent.BessemerSteel. -Steel manufactured by other source of heat. The word " auto- of tin.Technically known as Hard the Bessemer process (the invention of geneous " means " self -generated." Bronze." Sir Henry Bessemer in1856). In the The lead linings of chemical and acidBeryllium. -Formerly named " Gluoinum." Bessemer process, the molten " pig " iron tanks are usually autogenously soldered Metallic element. Chemical symbol, Be ; is run into a receptacle known as a because the presence of any dissimilar At. No. 4 ; At. Wt. 9 ; M.P. 962°C. ; Sp. " converter," in which a blast of air is metal at the joints would set up electro- Gray. 2.1; Sp. Ht. .397. passed through it.Impurities are thus lytic actions which might attain serious Chief ore :Beryl, 3BeO.A1203.6SiO2. burned out of the molten metal. proportions. Occurs also in gems, such as emerald. BibraAlloy. -Composition :Bismuth, 8 Avional.-A Swiss aluminium alloy. Com- Name of the metal derived from its parts; tin, 9 parts; lead, 38 to 40 parts. -
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. -
Aluminum and Aluminum-Alloy Extruded Bars, Rods, Wire, Profiles
Designation: B 221 – 05a Standard Specification for Aluminum and Aluminum-Alloy Extruded Bars, Rods, Wire, Profiles, and Tubes1 This standard is issued under the fixed designation B 221; the number immediately following the designation indicates the year of original adoption or, in the case of revision, the year of last revision. A number in parentheses indicates the year of last reapproval. A superscript epsilon (e) indicates an editorial change since the last revision or reapproval. This standard has been approved for use by agencies of the Department of Defense. 1. Scope* B211 Specification for Aluminum and Aluminum-Alloy 1.1 This specification2 covers aluminum and aluminum- Bar, Rod, and Wire alloy extruded bar, rod, wire, profile, and tube in the aluminum B 241/B 241M Specification for Aluminum and Aluminum- alloys (Note 1) and tempers shown in Table 2. Alloy Seamless Pipe and Seamless Extruded Tube B 429 Specification for Aluminum-Alloy Extruded Struc- NOTE 1—Throughout this specification, the use of the term alloy in the tural Pipe and Tube general sense includes aluminum as well as aluminum alloy. B 557 Test Methods of Tension Testing Wrought and Cast NOTE 2—For rolled or cold-finished bar and rod refer to Specification B211, for drawn tube, Specification B 210, for structural pipe and tube, Aluminum- and Magnesium-Alloy Products Specification B 429, and for seamless pipe and tube, Specification B 594 Practice for Ultrasonic Inspection of Aluminum- B 241/B 241M. Alloy Wrought Products for Aerospace Applications 1.2 Alloy and temper designations are in accordance with B 660 Practices for Packaging/Packing of Aluminum and ANSI H35.1. -
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. -
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.