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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. -
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. -
Aluminium Products Coil
Helping manufacturers across the globe achieve sustainable leaner manufacturing processes Aluminium Coil, Foil, Products Sheet & Wire Commercially Pure Aluminium Alloys Series 1000 Series 2000 Series 3000 Fast Series 4000 Series 5000 Turnaround Series 6000 Processing Series 7000 Series 8000 Clad Aluminium WIDE STOCK RANGE Low Width Thickness Ratio 3:1 unique to the industry (normal minimum is 8:1) Over 75 years Experience Knight Group Visit our websites: Main: www.knight-group.co.uk Offcuts: www.ksmdirect.co.uk www.pmdirect.be Head Office Linkside, Summit Road Cranborne Industrial Estate Potters Bar, Hertfordshire EN6 3JL United Kingdom Main Office : +44(0)1707 650251 Fax: +44(0)1707 651238 [email protected] Knight Strip Metals Ltd Sales, Processing & Warehouse Saltley Business Park Cumbria Way, Saltley Birmingham B8 1BH United Kingdom Telephone: +44 (0)121 322 8400 Fax: +44 (0)121 322 8401 Sales 08456 447 977 [email protected] Precision Metals EU Industriezone Mechelen-Noord (D) Omega Business Park Wayenborgstraat 25 2800 Mechelen Belgium Telephone: +32 (0) 15 44 89 89 Fax: +32 (0) 15 44 89 90 [email protected] The information contained herein is given in good faith and is based on our present knowledge and experience. However, no liability will be accepted by the Knight Group and its subsidiaries in respect of any action taken by any third party in reliance thereon. Any advice given by the Company to any third party is given for that party’s assistance only and without any liability on the part of the Company. The contents of this brochure are subject to change and the most recent edition of all Knight Group documentation can be found on our website or by written request. -
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 -
Catalogue Short 1..178
Serving The Needs of Science and Industry Worldwide Au service de la Science et de l'Industrie dans le monde entier Weltweiter Lieferant fuÈ r Wissenschaft und Industrie Metals and Alloys Ceramics Polymers Composites Me taux et Alliages Ce ramiques PolymeÁ res Composites Metalle und Legierungen Keramiken Polymere Verbundwerkstoffe Ermine Business Park, Huntingdon PE29 6WR England Telephone +44 1480 424 800 : Fax +44 1480 424 900 Goodfellow Cambridge Limited Ermine Business Park HUNTINGDON PE29 6WR England Tel: +44 1480 424 800 or +44 1480 424 800 Fax: +44 1480 424 900 or +44 1480 424 900 Goodfellow Corporation 305 High Tech Drive Oakdale, PA 15071 USA Tel: 1-800-821-2870 (USA and Canada) or +1 724 695 7060 Fax: 1-800-283-2020 (USA and Canada) or +1 724 695 7063 Goodfellow SARL 229, rue Solfe rino F-59000 Lille France Tel : 0800 917 241 (nume ro vert) or +44 1480 424 813 Fax : 0800 917 313 (nume ro vert) or +44 1480 424 900 Goodfellow GmbH Postfach 13 43 D-61213 Bad Nauheim Germany Tel: 0800 1000 579 (freecall) or +44 1480 424 810 Fax: 0800 1000 580 (freecall) or +44 1480 424 900 Web : www.goodfellow.com Email: [email protected] Check out www.goodfellow.com or email [email protected] for latest prices #Goodfellow Cambridge Limited February 2009 Email: [email protected] Telephone +44 1480 424 800 : Fax +44 1480 424 900 CONTENTS Introduction 1 Product Descriptions 2 General Information 6 Order information 7 Company Details 8 Metals 9 Alloys 68 Compounds 100 Intermetallics 105 Ceramics 106 Polymers 114 Composites 136 Metal Data -
Microstructures and Mechanical Properties of AA- 5754 and AA-6061 Aluminum Alloys Formed by Single Point Incremental Forming Process
Microstructures and Mechanical properties of AA- 5754 and AA-6061 Aluminum alloys formed by Single Point Incremental Forming Process Sahand Pourhassan Shamchi Submitted to the Institute of Graduate Studies and Research in partial fulfillment of the requirements for the Degree of Master of Science in Mechanical Engineering Eastern Mediterranean University September 2014 Gazimağusa, North Cyprus Approval of the Institute of Graduate Studies and Research _____________________________________ Prof. Dr. Elvan Yilmaz Director I certify that this thesis satisfies the requirements as a thesis for the degree of Master of Science in Mechanical Engineering. ________________________________ Prof. Dr. Uğur Atikol Chair, department of Mechanical Engineering We certify that we have read this thesis and that in our opinion it is fully adequate in scope and quality as a thesis for the degree of Master of Science in Mechanical Engineering. _____________________________________ Asst. Prof. Dr. Ghulam Hussain Supervisor Examining Committee 1. Prof. Dr. Fuat Egelioğlu __________________________ 2. Prof. Dr. Majid Hashemipour __________________________ 3. Asst. Prof. Dr.Ghulam Hussain __________________________ ABSTRACT Single point incremental forming (SPIF) process is considered as a cost-effective method to fabricate sheet metals because there is no need for dedicated dies which are used in other conventional processes. Due to the capability of forming sheets on CNC machines, the flexibility of this process is high which allows the operator to modify the geometry of the product much easier than the other methods like stamping. This study is carried out to investigate the effects of different forming parameters on the mechanical properties and microstructures of formed parts. The effects of wall angle, feed rate, spindle speed and lubrication are explored on AA5754 and AA6061 Aluminium Alloys. -
Extruded Aluminium Profiles
Aluminium Al Product format: Extruded Technical characteristics : Flats, rods, tubes and extruded aluminium profiles www.bronmetal.com Aluminium Al Product format: Extruded Technical Characteristics: Flats, rods, tubes and extruded aluminium profiles EQUIVALENCES 1050 PURE ALUMINIUM (99,5%) EQUIVALENTS NATIONAL STANDARDS AND TRADE NAMES ISO SPAIN GERMANY CANADA E.E.U.U. FRANCE UNITED KINGDOM ITALY OTHERS Al-99,5 L-3051 Al-99,5 Al-99,5 A5 1B 9001/2 17010 Puraltok 99,5 3,0255 1S Durcilium T 4007 WG-1S Hiduminium A1 1150/55 Impalco 0,5 Aluran 99,5 EQUIVALENCES 1200 PURE ALUMINIUM (99 %) EQUIVALENTS NATIONAL STANDARDS AND TRADE NAMES ISO SPAIN GERMANY CANADA E.E.U.U. FRANCE UNITED KINGDOM ITALY OTHERS Al 99,0 L-3001 Al 99,0 2S 1100 A-4 1C 3567 4010 Puraltok 99 3,0205 2S 1100 5090 WG-2S Birmetal 2 9001/1 17005 90 Hiduminium-1C 1008 1010 NA-2S 1191 2584 A0 Aluran 99 www.bronmetal.com Aluminium Al Product format: Extruded Technical Characteristics: Flats, rods, tubes and extruded aluminium profiles EQUIVALENCES 2007 ALUMINIUM-COPPER EQUIVALENTS NATIONAL STANDARDS AND TRADE NAMES SPAIN GERMANY FRANCE SUIZA L-3121 DIN 1725 A U4Pb Al-CuMgPb Cobreltok 07 DIN 1746 Al-CuMgCd DIN 1747 Decotal 200 Tordal 1970 Aludur D 505 Spanal 320 MFK Aludur 570 A Automat EQUIVALENCES 2011 ALUMINIUM-COPPER COMMERCIAL EQUIVALENT SPAIN CANADA E.E.U.U. FRANCE SUIZA ITALY UNITED KINGDOM L-3192 CB 60 2011 A-U5PbBi Decotal 500 Recidal 11 28 S 28-S CSA HA,5 ASTM B 211 Fortal 2011 28 S QQ-R-225/3 QQ-R-365 WW-P-471 Ty III QQ-R-566 www.bronmetal.com Aluminium Al Product format: Extruded Technical Characteristics: Flats, rods, tubes and extruded aluminium profiles EQUIVALENCES 2030 ALUMINIUM-COPPER EQUIVALENTS NATIONAL STANDARDS AND TRADE NAMES SPAIN GERMANY FRANCE SUIZA L-3121 Al CuMgPb A U4Pb Al-CuMgPb 3,1645 NF A 57.350 Al-CuMgCd DIN 1725 Fortal D Decotal 200 DIN 1746 Fortal 2030 Aludur D 505 DIN 1747 Carbium al Pbl MFK Tordal 1970 Duralumin DE Spanal 320 Aludur 570 A Automat EQUIVALENCES2014 ALUMINIUM-COPPER EQUIVALENTS NATIONAL STANDARDS AND TRADE NAMES ISO SPAIN GERMANY CANADA E.E.U.U. -
Dissimilar Materials of Friction Stir Welding - Overview
International Journal of Engineering Trends and Technology (IJETT) – Volume-44 Number-3 -February 2017 Dissimilar Materials of Friction Stir Welding - Overview K. Nagendra Kumar1, P. Ravikanth Raju2 1Asistance Professor, Department of Mechanical Engineering, Bhaskar Engineering College, Yenkapally, Moinabad (M), R.R.(Dist), Hyderabad-500075, Telangana State, India. 2Department of Mechanical Engineering, Anurag Group of Institutions, Venkatapur (V), Ghatkesar (M), R.R. Dist -500088, Telangana State, India Abstract - Friction Stir Welding is a joining process welding of metal-to-polymer is given greater which involves the deformation of materials. In this emphasis in this section than metal to- metal and process tool will generate the pressure and polymer-to-polymer welding, since metal-to- temperature and form solid state weld. This process polymer is a novel technique and there are fewer is suitable for joining different materials, different publications in this area [15]. The schematic mechanical and chemical properties, and different representation of FSW process is shown in Fig. material structures. Fusion welding processes 1. exhibits poor weldability by Welding of dissimilar aluminium alloys. Because of thin oxide layer formation, oxide layer tends to thicken at higher temperatures on the surface of aluminium alloys. This review addresses the Friction stir welding overview which includes the basic concept of the process, microstructure formation, influencing process parameters, typical defects in FSW process and some recent applications. The paper will also discuss some of the process variants of FSW such as Friction Stir Processing. Keywords - Tool rotational speed, Friction Stir welding, dissimilar aluminium alloy. 1. INTRODUCTION Fig 1: FSW Process [14] FSW was invented in UK in December, 1991 at The shoulder is pressed against the surface of the The Welding Institute (TWI). -
Fatigue Behavior of 2618-T851 Aluminum Alloy Under Uniaxial and Multiaxial Loadings
Open Archive Toulouse Archive Ouverte (OATAO) OATAO is an open access repository that collects the wor of some Toulouse researchers and ma es it freely available over the web where possible. This is an author's version published in: https://oatao.univ-toulouse.fr/24572 Official URL : https://doi.org/10.1016/j.ijfatigue.2019.105322 To cite this version : BenaÕssa, Malek and Mabru, Catherine and Chaussumier, Michel Fatigue behavior of 2618-T851 aluminum alloy under uniaxial and multiaxial loadings. (2020) International Journal of Fatigue, 131 (105322). 1-9. ISSN 0142-1123 Any correspondence concerning this service should be sent to the repository administrator: [email protected] Fatigue behavior of 2618-T851 aluminum alloy under uniaxial and multiaxial loadings ⁎ Benaïssa Malek, Catherine Mabru, Michel Chaussumier Université de Toulouse, Institut Clément Ader (ICA), UMR CNRS 5312, UPS/INSA/ISAE/ Mines Albi, 3 Rue Caroline Aigle, 31400 Toulouse, France ABSTRACT Keywords: AA2618 aeronautical aluminum alloy has been largely used in the past, especially in well-known Concorde AA2618-T851 aircraft, developed during sixties decade. In more recent aircraft, this alloy has been largely replaced by others Multiaxial fatigue such as 7075 which present greater fatigue resistance. Forgotten for a time, AA2618 comes back in new aircrafts Roughness for structural parts submitted to fatigue loading at high temperature because of only a slight decrease of fatigue Crossland criterion resistance of this alloy compared to room temperature fatigue resistance. In this paper, a complete fatigue characterization of 2618-T851 aluminum alloy is presented: fatigue tests under uniaxial tensile or torsion cyclic loadings, with mean tensile or shear stress have been realized; fatigue tests under combined tensile-torsion, in or out-of-phase have also been conducted as well as some combined tensile-torsion-internal pressure fatigue tests. -
Abstracts from the Scientific and Technical Press Titles And
December, ig4j Abstracts from the Scientific and Technical Press " (No. 117. October, 1943) AND Titles and References of Articles and Papers Selected from Publications (Reviewed by R.T.P.3) TOGETHER WITH List of Selected Translations (No. 63)' London : "THE ROYAL AERONAUTICAL SOCIETY" with which is incorporated "The Institution of Aeronautical Engineers" 4, Hamilton Place, W.I Telephone: Grosvenor 3515 (3 lines) ABSTRACTS FROM THE SCIENTIFIC AND TECHNICAL PRESS. Issued by the Directorate's of Scientific Research and Technical Development, Ministry of Air craft Production. (Prepared by R.T.P.3.) No. 117. OCTOBER, 1943. Notices and abstracts from the Scientific and Technical Press are prepared primarily for_ the information of Scientific and Technical Staffs. Particular attention is paid to the work carried out in foreign countries, on the assumption that the more accessible British work (for example that published by the Aeronautical Research Committee^ is already known to these Staffs. Requests from scientific and technical staffs for further information of transla tions should be addressed to R.T,P.3, Ministry of Aircraft Production, and not to the Royal Aeronautical Society. Only a limited number of the articles quoted from foreign journals are trans lated and usually only the original can be supplied on loan. If, however, translation is required, application should be made in writing to R.T.P.3, the requests being considered in accordance with existing facilities. ' NOTE.—As far as possible, the country of origin quoted in the items refers to the original source. The Effect of Nitrogen on the Properties of Certain Austenitic Valve Steels. -
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. -
THE VACUUM CHAMBERIN the INTERACTION REGIÓN of PARTIÓLE COLLIDERS: a HISTORICAL STUDY and DEVELOPMENTS IMPLEMENTED in the Lhcb EXPERIMENT at CERN
Departamento de Física Aplicada a la Ingeniería Industrial Escuela Técnica Superior de Ingenieros Industriales THE VACUUM CHAMBERIN THE INTERACTION REGIÓN OF PARTIÓLE COLLIDERS: A HISTORICAL STUDY AND DEVELOPMENTS IMPLEMENTED IN THE LHCb EXPERIMENT AT CERN Autor: Juan Ramón Klnaster Refolio Ingeniero Industrial por la E.T.S.I. Industriales Universidad Politécnica de Madrid Directores: Raymond J.M. Veness Ph; D. Mechanics of Materials and Plasticity University of Leicester (England) Linarejos Gámez Mejías Doctor Ingeniero Industrial por la E.T.S.I.I. Universidad Politécnica de Madrid 2004 Whatever you dream, you can do, begin it! Boldness has power, magic and genius in it Goethe Homo sum: humani nihil a me alienum puto (Je suis homme, et rien de ce que est humain ne m'est étraxiger) Terence Loving softly and deeply... Elsje Tout proche d'étre un Boudha paresseusement réve le vieux pin Issa En nuestra cabeza, en nuestro pecho es donde están los circos en que, vestidos con los disfraces del tiempo, se enfrentan la Libertad y el Destino Jünger This Thesis has been possible thanks to the support of many people that duñng last 15 months have helped me in different ways. I would like to thank my co- lleagues R. Aehy, P. Bryant, B. Calcagno, G. Corii, A. Gerardin, G. Foffano, M. Goossens, C. Hauvüler, H. Kos, J. Kruzelecki, P. Lutkiewicz, T. Nakada, A. Rossi, J.A. Rubio, B. Szybinski, D. Tristram, B. Ver- solatto, L. Vos and W. Witzeling for their contribu- tions in different moments. Neither would I have ever managed to finish it without those moments of peace shared with mes fréres d'Independance et Verité á VOr :.