Nickel and Its 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. -
The Study of Hems Based on the Mechanically Activated Intermetallic Al12mg17 Powder
molecules Article The Study of HEMs Based on the Mechanically Activated Intermetallic Al12Mg17 Powder Sergei Sokolov * , Alexander Vorozhtsov, Vladimir Arkhipov and Ilya Zhukov Laboratory of Metallurgy Nanotechnologies, National Research Tomsk State University, Lenin Avenue, 36, 634050 Tomsk, Russia; [email protected] (A.V.); [email protected] (V.A.); [email protected] (I.Z.) * Correspondence: [email protected]; Tel.: +7-923-406-77-01 Academic Editor: Svatopluk Zeman Received: 30 May 2020; Accepted: 19 July 2020; Published: 5 August 2020 Abstract: In this work, Al–Mg intermetallic powders were characterized and obtained by melting, casting into a steel chill and subsequent mechanical activation in a planetary mill. The method for producing Al12Mg17 intermetallic powder is presented. The dispersity, morphology, chemical composition, and phase composition of the obtained powder materials were investigated. Certain thermodynamic properties of high-energy materials containing the Al-Mg powder after mechanical activation of various durations were investigated. The addition of the Al-Mg powders to the high-energy composition (synthetic rubber SKDM-80 + ammonium perchlorate AP + boron B) can significantly increase the burning rate by approximately 47% and the combustion heat by approximately 23% compared with the high-energy compositions without the Al-Mg powder. The addition of the Al12Mg17 powder obtained after 6 h of mechanical activation provides an increase in the burning rate by 8% (2.5 0.1 mm/s for the mechanically activated Al Mg powder and ± 12 17 2.3 0.1 mm/s for the commercially available powder) and an increase in the combustion heat by 3% ± (7.4 0.2 MJ/kg for the mechanically activated Al-Mg powder and 7.1 0.2 MJ/kg for the commercially ± ± available powder). -
Development of Filler Metals and Procedures for Vacuum Brazing Of
Development of Filler Metals and Procedures for Vacuum Brazing of Aluminum Several brazing filler metal compositions have been developed which offer significant improvements over existing compositions. They braze in vacuum at temperatures lower than normal flow temperatures and have equal or better flowability BY W. J. WERNER, G. M. SLAUGHTER AND F. B. GURTNER Introduction ry cleanliness levels under production vantages. As a single entity, it was This report documents work per conditions. The maximum allowable immediately more desirable from a formed toward the development of lag between cleaning and brazing was cleaning, assembling and material found to be 12 hours. handling standpoint. Metallurgically, new brazing filler metals for vacuum- 2 fluxless brazing (1 X 10~6 torr) C. S. Beuyukian developed tech the 4045 brazing filler metal with its certain aluminum alloys of interest to niques for vacuum or inert gas fluxless lower silicon content allowed greater the Army. The base metals under brazing of aluminum cold plates for latitude in processing parameters than consideration were alloys 6061, 2219, use in Apollo command modules. In did alloy No. 718. 7075 and 2024. Brazing filler metal this work, brazing filler metal No. 718 Finally, the workers at Aeronca, and No. 23 brazing sheet were evalu Inc. completed a study on inert gas flow temperatures needed for these 3 alloys encompass the temperature ated. Alloy No. 718 is nominally 88% brazing of aluminum in early 1967. range 900 to 1200F. Specifically, the aluminum, 12% silicon; No. 23 braz Their work was concerned with de contract called for the development of ing sheet is comprised of 6951 base velopment of high strength brazed alloys with flow temperatures of 950, alloy clad on one side with 4045 aluminum honeycomb structures 1000, and 1050F. -
Maec.19 70 (University of London) London
COMPLEX & INCREMENTAL STRESS CREEP OF A HIGH STRENGTH ALUMINIUM ALLOY AT ELEVATED TEMPERATURES (ALLOY: HIDUMINIUM RR58 SPECIFICATION DTD 731) by SURINDAR BAHADUR MATHUR Thesis presented in the Department of Mechanical Engineering for the Award of the Doctor of Philosphy in Mechanical Engineering of the University of London. Mechanical Engineering Department Imperial College of Science and Technology mAec.19 70 (University of London) London. ABSTRACT A theory for creep rates under complex and incremental stresses is deduced from experimental data concerning complex creep at elevated temperatures for the test material HIDUMINIUM RR 58 - Specification DID 731. The most important results are for tubular specimens tested at 150°C and 250°C under incremental loads. The analysis of results relates to steady state creep only. Modified relationships in stress equivalence and strain equivalence are proposed to account for thermal softening, polygonization, recrystallization and the resulting exaggerated flow in the direction of the applied shear. (The original equations are based on the hypothesis of Von Mises). A further relationship is suggested between the immediate total energy of distortion and the subsequent creep work rate. Results of the static tests and the results of the tests for creep behaviour under complex loading are presented and compared with the results of static torsion and simple incremental torsion creep tests on the basis of the proposed equations. An appendix describes the complex creep testing machine, furnace, extensometers -
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. -
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. -
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. -
Microstructual and Thermal Analysis of Aluminum-Silicon and Magnesium-Aluminum Alloys Subjected to High Cooling Rates
University of Windsor Scholarship at UWindsor Electronic Theses and Dissertations Theses, Dissertations, and Major Papers 2012 Microstructual and Thermal Analysis of Aluminum-Silicon and Magnesium-Aluminum Alloys Subjected to High Cooling Rates Paul Marchwica University of Windsor Follow this and additional works at: https://scholar.uwindsor.ca/etd Recommended Citation Marchwica, Paul, "Microstructual and Thermal Analysis of Aluminum-Silicon and Magnesium-Aluminum Alloys Subjected to High Cooling Rates" (2012). Electronic Theses and Dissertations. 5572. https://scholar.uwindsor.ca/etd/5572 This online database contains the full-text of PhD dissertations and Masters’ theses of University of Windsor students from 1954 forward. These documents are made available for personal study and research purposes only, in accordance with the Canadian Copyright Act and the Creative Commons license—CC BY-NC-ND (Attribution, Non-Commercial, No Derivative Works). Under this license, works must always be attributed to the copyright holder (original author), cannot be used for any commercial purposes, and may not be altered. Any other use would require the permission of the copyright holder. Students may inquire about withdrawing their dissertation and/or thesis from this database. For additional inquiries, please contact the repository administrator via email ([email protected]) or by telephone at 519-253-3000ext. 3208. Microstructual and Thermal Analysis of AlSi and MgAl Alloys Subjected to High Cooling Rates By Paul C. Marchwica A Thesis Submitted to the Faculty of Graduate Studies through the Department of Mechanical, Automotive and Materials Engineering in Partial Fulfillment of the Requirements for the Degree of Master of Applied Science at the University of Windsor Windsor, Ontario, Canada 2012 © 2012 P. -
Aluminum Alloy Weldability: Identification of Weld Solidification Cracking Mechanisms Through Novel Experimental Technique and Model Development
Dipl.-Ing. Nicolas Coniglio Aluminum Alloy Weldability: Identifi cation of Weld Solidifi cation Cracking Mechanisms through Novel Experimental Technique and Model Development BAM-Dissertationsreihe • Band 40 Berlin 2008 Die vorliegende Arbeit entstand an der BAM Bundesanstalt für Materialforschung und -prüfung. Impressum Aluminum Alloy Weldability: Identifi cation of Weld Solidifi cation Cracking Mechanisms through Novel Experimental Technique and Model Development 2008 Herausgeber: BAM Bundesanstalt für Materialforschung und -prüfung Unter den Eichen 87 12205 Berlin Telefon: +49 30 8104-0 Telefax: +49 30 8112029 E-Mail: [email protected] Internet: www.bam.de Copyright © 2008 by BAM Bundesanstalt für Materialforschung und -prüfung Layout: BAM-Arbeitsgruppe Z.64 ISSN 1613-4249 ISBN 978-3-9812354-3-2 Aluminum Alloy Weldability: Identification of Weld Solidification Cracking Mechanisms through Novel Experimental Technique and Model Development Dissertation zur Erlangung des akademischen Grades Doktor-Ingenieur (Dr.-Ing.) genehmigt durch die Fakultät für Maschinenbau der Otto-von-Guericke-Universität Madgeburg am 02.06.08 vorgelegte Dissertation von Dipl.-Ing. Nicolas Coniglio Thesis Committee: Prof. Dr.-Ing. A. Bertram Prof. Dr.-Ing. T. Böllinghaus Prof. C.E. Cross Prof. S. Marya Date of Examination: 23 October 2008 Abstract Abstract The objective of the present thesis is to make advancements in understanding solidification crack formation in aluminum welds, by investigating in particular the aluminum 6060/4043 system. Alloy 6060 is typical of a family of Al-Mg-Si extrusion alloys, which are considered weldable only when using an appropriate filler alloy such as 4043 (Al-5Si). The effect of 4043 filler dilution (i.e. weld metal silicon content) on cracking sensitivity and solidification path of Alloy 6060 welds are investigated. -
The Tensile and Creep Behavior of Mg–Zn Alloys with and Without Y and Zr As Ternary Elements
J Mater Sci (2007) 42:3675–3684 DOI 10.1007/s10853-006-1352-5 The tensile and creep behavior of Mg–Zn Alloys with and without Y and Zr as ternary elements C. J. Boehlert Received: 28 July 2005 / Accepted: 28 February 2006 / Published online: 30 January 2007 Ó Springer Science+Business Media, LLC 2007 Abstract Tensile–creep experiments were conducted effects on the tensile properties and creep behavior in the temperature range 100–200 °C and stress range are discussed in comparison to other Mg-based alloy 20–83 MPa for a series of magnesium–zinc–yttrium systems. (Mg-Zn-Y) and mangnesium-zinc–zirconium (Mg-Zn- Zr) alloys ranging from 0 to 5.4 wt% Zn, 0 to 3 wt% Y, and 0 to 0.6 wt.% Zr. The greatest tensile– creep resistance was exhibited by an Mg–4.1Zn–0.2Y alloy. The room-temperature yield strength increased Introduction with increasing Y content for Mg–1.6–2.0Zn alloys. The greatest tensile strength and elongation was In order to improve the creep strength of magnesium exhibited by Mg–5.4Zn–0.6Zr. This alloy also exhibited (Mg) alloys, rare earth and/or alkaline earth elements the finest grain size and the poorest creep resistance. in small quantities have been effectively used as alloy The measured creep exponents and activation energies additions [1–14]. For example, the creep rate of suggested that the creep mechanisms were dependent Mg–8wt.%Y1 has been observed to be four orders of on stress. For applied stresses greater than 40 MPa, the magnitude lower than AZ91 at 277 °C in the stress creep exponents were between 4 and 8. -
Aircraft Metallurgy (According to the Syllabus Prescribed by Director General of Civil Aviation, Govt
L.N.V.M. Society Group of Institutes, Palam Extn., Part-1, Sec.-7, Dwarka, New Delhi - 45 1 Aircraft Metallurgy (According to the Syllabus Prescribed by Director General of Civil Aviation, Govt. of India) 2 Aircraft Metallurgy L.N.V.M. Society Group of Institutes, Palam Extn., Part-1, Sec.-7, Dwarka, New Delhi - 45 3 CONTENTS 1. FERROUS METALS : PRODUCTION OF STEELS AND ALLOY STEELS 1 2. NON-FERROUS METALS AND IT’S ALLOYS 12 3. NICKEL ALLOYS 19 4. COPPER AND ITS ALLOYS 29 5. WROUGH ALUMINIUM ALLOYS 36 6. MAGNESIUM ALLOYS 43 7. HEAT TREATMENT OF NON-FERROUS METALS AND ALLOYS 58 8. IDENTIFICATION OF METALS 65 9. MECHANICAL TESTING OF METALS 67 10. CORROSION : REMOVAL AND RECTIFICATION 77 11. CORROSION : METHODS OF PROTECTION 82 12. NDE : OIL AND CHALK PROCESSES 86 13. NDE : PENETRANT DYE PROCESSES 88 14. NDE : MAGNETIC FLAW DETECTION 93 15. NDE : FLUORESCENT PENETRANT PROCESSES 98 16. NDE : ENDOSCOPE INSPECTIONS 103 17. NDE : ULTRASONIC FLAW DETECTION AND THICKNESS MEASUREMENT 107 18. NDE : RADIOLOGICAL EXAMINATION OF AIRCRAFT STRUCTURE 111 19. NDE : EDDY CURRENT METHODS 114 20. ADVANCED COMPOSITES MATERIALS 118 L.N.V.M. Society Group of Institutes, Palam Extn., Part-1, Sec.-7, Dwarka, New Delhi - 45 1 UNIT - I FERROUS METAL: PRODUCTION OF STEELS AND ALLOYS STEELS STEEL Steel basically differs from cast iron in the amount of carbon content contained by it. It is not only the quantity of carbon which makes the difference but also the form in which it is present. In steel the amount of carbon present is upto 1.5 percent and it is completely in the combined form. -
Thermomechanical Processing of Mg-Li-Al Ultralight Alloys Rezawana Islam
University of North Dakota UND Scholarly Commons Theses and Dissertations Theses, Dissertations, and Senior Projects January 2019 Thermomechanical Processing Of Mg-Li-Al Ultralight Alloys Rezawana Islam Follow this and additional works at: https://commons.und.edu/theses Recommended Citation Islam, Rezawana, "Thermomechanical Processing Of Mg-Li-Al Ultralight Alloys" (2019). Theses and Dissertations. 2462. https://commons.und.edu/theses/2462 This Thesis is brought to you for free and open access by the Theses, Dissertations, and Senior Projects at UND Scholarly Commons. It has been accepted for inclusion in Theses and Dissertations by an authorized administrator of UND Scholarly Commons. For more information, please contact [email protected]. THERMOMECHANICAL PROCESSING OF Mg-Li-Al ULTRALIGHT ALLOYS by Rezawana Islam Bachelor of Science, Military Institute of Science and Technology A Thesis Submitted to the Graduate Facility of the University of North Dakota in partial fulfillment of the requirements for the degree of Master of Science Grand Forks, North Dakota May 2019 i Copyright 2019 Rezawana Islam ii PERMISSION Title Thermomechanical processing of Mg-Li-Al ultralight alloys. Department Mechanical Engineering Degree Master of Science In presenting this thesis in partial fulfillment of the requirements for a graduate degree from the University of North Dakota, I agree that the library of this University shall make it freely available for inspection. I further agree that permission for extensive copying for scholarly purposes may be granted by the professor who supervised my thesis work or, in her (or his) absence, by the Chairperson of the department or the Dean of the School of Graduate Studies.