(Extremely Resistible to Corrosion by Sea Water.) 2. Non-Corrodibility
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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. -
Inhaltsverzeichnis Seite Schrifttum 5 Abkürzungen 6 Einleitung I Waren
Inhaltsverzeichnis Seite Schrifttum 5 Abkürzungen 6 Einleitung i Waren. — Warenkunde. — Einteilung der Waren. — Hilfs- wissenschaften der Warenkunde 7— 8 I. Metalle und Metallwaren 8 A. Edelmetalle. 1. Gold. — 2. Silber. — 3. Platin. — 4. Queck- silber 10—18 B. Unedle Schwermetalle. 1. Eisen und Eisenwaren (Roh- eisen, schmiedbares Eisen, Erzeugnisse aus Eisen und Stahl). — 2. Kupfer. — 3. Blei. — 4. Zink. — 5. Zinn. — 6. Nickel. — 7. Arsen. — 8. Antimon. — 9. Wismut 18—35 C. Leichtmetalle. 1. Aluminium. — 2. Magnesium 35—37 D. Legierungen. 1. Bronze. — 2. Tombak. — 3. Messing. — 4. Neusilber. — 5. Konstantan .— 6. Britanniametall. — 7. Schriftmetall. — 8. Lagermetalle. — 9. Duralumin. — lO.Hydronalium. — 11. Silumin. —12. Elektron. — 13. Heus- ler'sche Legierungen 37—40 II. Edelsteine und Schmucksteine 40 A. Edelsteine. 1. Diamant. — 2. Rubin und Saphir. — 3. Spinell. — 4. Chrysoberyll. — 5. Smaragd. — 6. Topas. — 7. Zirkon. — 8. Granat. — 9. Türkis. — 10. Edelopal 41—46 B. Schmucksteine. 1. Quarz. — 2. Chalcedon. — S.Mond- stein. — 4. Lasurstein. — 5. Malachit. — 6. Blutstein. — 7. Bernstein 46—48 III. Bildhauersteine 48 1. Marmor. — 2. Alabaster. — 3. Serpentin. — 4. Meer- schaum. — 5. Talk 48—51 IV. Baustoffe 51 A. Bausteine. 1. Kalkstein. — 2. Sandsteine. — 3. Granit. — 4. Porphyr. — 5. Basalt. — 6. Magnesit. — 7. Kunststeine .... 51—53 B. Bindemittel. 1. Branntkalk. — 2. Zement. — 3. Gips 54—56 V. Schleif- und Glättemittel, Mühlsteine 57 1. Schleifsteine. — 2. Schmirgel. — 3. Gemeiner Korund. — 4. Siliziumkarbid. — 5. Bimsstein. — 6. Tripel. — 7. Polier- rot. — 8. Zinnasche. — 9. Wiener Kalk. — 10. Schlämm- kreide.—11. Mühlsteine 67—58 VI. Tonwaren 59 Ton. — 1. Porzellan. — 2. Steinzeug. — 3. Steingut. — 4. Töpferware. — 5. Ziegel. — 6. Feuerfeste Steine 59—67 VII. -
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. -
Aluminium Appications CML514 2016.Pdf
Elements of Gr. 13 Unique Property Applications Boron Lewis acid Nuclear reactors‐ control 10B‐ High Nuclear cross rods section for thermal Lewis acid, BNCT neutrons Light metal Bulk usage: Airplanes, Aluminium Surface passivity ships, cars, trains Good strength to weight AlCl3: Friedel Crafts rxn ratio and conductivity MAO: In olefin m.p. 660.3 °C polymerization Gallium Liquid metal Gallium Arsenide solar m.p.29.77 °C cells Gallium nitride LED Low melting soft solid ITO Indium (m.p.156 °C) production of transparent conductive coatings Thallium Poison, non metallic The poisoner's poison“ (tasteless , odorless) Chemistry of Aluminium More than its compounds, the bulk usage of aluminium, especially its alloys dominate the industry •Lightest metal; also relatively inexpensive metal . •Tin was 19,830 USD/Metric Ton, zinc was 2,180 USD/MT and aluminium was 1,910 USD/MT •Third most abundant element on the earths crust: combined in 270 minerals •Low density and ability to resist corrosion by passivation. Pure aluminium has about one‐third the density and stiffness of steel. The yield strength of pure aluminium is 7–11 MPa, while aluminium alloys have yield strengths ranging from 200 MPa to 600 MPa. Yield strength of mild steel is 250 Mpa while that of high strength alloy steel is 690 Mpa A yield strength or yield point of a material is defined as the stress at which a material begins to deform plastically. Prior to the yield point the material will deform elastically and will return to its original shape when the applied stress is removed. ( Mpa = megapascal = 145psi) Three main reasons why aluminium alloys are used instead of pure aluminium •Increased strength to weight ratio over pure aluminium. -
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. -
Applied Chemistry-Ii L T P 3 - 2
2.4 APPLIED CHEMISTRY-II L T P 3 - 2 RATIONALE The role of chemistry in every branch of engineering and technology is expanding greatly. Now a days, various chemical products are playing important role in the field of engineering with increasing number of such products each successive years. The strength of materials, the chemical composition of substances, their behaviour when subjected to different treatment and environment, and the laws of heat and dynamic energy have entered in almost every activity of modern life. Chemistry is considered as one of the core subjects for diploma students in engineering and technology for developing in them scientific temper and appreciation of chemical properties of materials, which they have to handle in their professional career. Effort should be made to teach this subject through demonstrations/ minor projects and with the active involvement of students. Note:- Teachers should give examples of engineering/technology applications of various concepts and principles in each topic so that students are able to appreciate learning of these concepts and principles. DETAILED CONTENTS 1. Metallurgy (08 hrs) A brief introduction of the terms: Metallurgy (types), mineral, ore, gangue or matrix, flux, slag, concentration (methods of concentrating the ores), ore, roasting, calcinations, smelting and refining of metal. Metallurgy of (i) Aluminium (ii) Iron Definition of an alloy, purposes of alloying, composition, properties and uses of alloys- brass, bronze, monel metal, magnalium, duralumin, alnico, stainless steel and invar. 2. Fuels (10 hrs) 2.1 Definition of a „Fuel‟, characteristics of a good fuel and classification of fuels with suitable examples 2.2 Definition of Calorific value of a fuel and determination of calorific value of a solid fuel with the help of Bomb calorimeter. -
Aluminium Laminate
Aluminum Al Product format: Laminate Technical characteristics: Aluminum sheet and strip rolled www.bronmetal.com Aluminum Al Product format: Laminate Technical characteristics : Aluminum sheet and strip rolled 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 Aluminum Al Product format: Laminate Technical characteristics : Aluminum sheet and strip rolled 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 EQUIVALENCIAS COMERCIALES 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 Aluminum Al Product format: Laminate Technical characteristics : Aluminum sheet and strip rolled 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 EQUIVALENCES 2014 ALUMINIUM-COPPER EQUIVALENTS NATIONAL STANDARDS AND TRADE NAMES ISO SPAIN GERMANY CANADA E.E.U.U. -
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. -
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]. -
A Study of Interrupted Aging in Al-Cu-Mg Alloys
A STUDY OF INTERRUPTED AGING IN AL-CU-MG ALLOYS by Joseph Ming-Ju Tsai A thesis submitted to the Faculty and Board of Trustees of the Colorado School of Mines in partial fulfillment of the requirements for the degree of Doctor of Philosophy (Metallurgy and Materials Engineering). Golden, Colorado Date: Signed: Joseph Ming-Ju Tsai Signed: Michael J. Kaufman Thesis Advisor Golden, Colorado Date: Signed: Professor Michael J. Kaufman, Department Head Department of Metallurgical and Materials Engineering ii ABSTRACT Recently, a novel interrupted aging treatment, T6I6, was reported to improve the strength and toughness of heat treatable Al alloys. It consisted of the following three stages, namely, 1) artificially underaging at a typical temperature (150-200 ◦C) and quenching to room temperature, 2) reheating to a lower aging temperature (60-100 ◦C) for times that result in hardening, and 3) reheating to the initial aging temperature again and holding until peak hardness is observed. The improvements were reported to be due to precipitate refinement and secondary precipitation during the low temperature age. However, the improvements in properties have not been consistently reproduced in the litera- ture, and an explanation for the discrepancies remains unclear. Therefore, the focus of this study was to investigate the interrupted aging processes and the effects of each aging stage, as well as the effect of cold work, on precipitate development in commercial 2024 Al and a high-purity variant of the commercial 2014 alloy, Al-4.2Cu-0.4Mg (wt%). The aging responses, precipitation behavior, and microstructural changes were examined using Vickers microhardness, electrical resistivity, and electron microscopy.