Advantages of Aluminium
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
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. -
Isothermes Kurzzeitermüdungsverhalten Der
i N Osama Khalil u2Mg1,5 C l A ISOTHERMES KURZZEITERMÜDUNGS- VERHALTEN DER HOCHWARMFESTEN ALUMINIUM-KNETLEGIERUNG 2618A verhalten von (AlCu2Mg1,5Ni) SCHRIFTENREIHE DES INSTITUTS FÜR ANGEWANDTE MATERIALIEN BAND 34 Isothermes Kurzzeitermüdungs O. KHALIL Osama Khalil Isothermes Kurzzeitermüdungsverhalten der hochwarm- festen Aluminium-Knetlegierung 2618A (AlCu2Mg1,5Ni) Schriftenreihe des Instituts für Angewandte Materialien Band 34 Karlsruher Institut für Technologie (KIT) Institut für Angewandte Materialien (IAM) Eine Übersicht über alle bisher in dieser Schriftenreihe erschienenen Bände finden Sie am Ende des Buches. Isothermes Kurzzeitermüdungs- verhalten der hochwarmfesten Aluminium-Knetlegierung 2618A (AlCu2Mg1,5Ni) von Osama Khalil Dissertation, Karlsruher Institut für Technologie (KIT) Fakultät für Maschinenbau Tag der mündlichen Prüfung: 15. Januar 2014 Impressum Karlsruher Institut für Technologie (KIT) KIT Scientific Publishing Straße am Forum 2 D-76131 Karlsruhe KIT Scientific Publishing is a registered trademark of Karlsruhe Institute of Technology. Reprint using the book cover is not allowed. www.ksp.kit.edu This document – excluding the cover – is licensed under the Creative Commons Attribution-Share Alike 3.0 DE License (CC BY-SA 3.0 DE): http://creativecommons.org/licenses/by-sa/3.0/de/ The cover page is licensed under the Creative Commons Attribution-No Derivatives 3.0 DE License (CC BY-ND 3.0 DE): http://creativecommons.org/licenses/by-nd/3.0/de/ Print on Demand 2014 ISSN 2192-9963 ISBN 978-3-7315-0208-1 DOI 10.5445/KSP/1000040485 Isothermes Kurzzeitermüdungsverhalten der hochwarmfesten Aluminium-Knetlegierung 2618A (AlCu2Mg1,5Ni) Zur Erlangung des akademischen Grades Doktor der Ingenieurwissenschaften an der Fakultät für Maschinenbau des Karlsruher Institut für Technologie (KIT) genehmigte Dissertation von Dipl.-Ing. -
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. -
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. -
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 -
Modeling, Optimization and Performance Evaluation of Tic/Graphite Reinforced Al 7075 Hybrid Composites Using Response Surface Methodology
materials Article Modeling, Optimization and Performance Evaluation of TiC/Graphite Reinforced Al 7075 Hybrid Composites Using Response Surface Methodology Mohammad Azad Alam 1,* , Hamdan H. Ya 1,*, Mohammad Yusuf 2 , Ramaneish Sivraj 1, Othman B. Mamat 1, Salit M. Sapuan 3,4, Faisal Masood 5 , Bisma Parveez 6 and Mohsin Sattar 1 1 Mechanical Engineering Department, Universiti Teknologi PETRONAS, Seri Iskandar 32610, Malaysia; [email protected] (R.S.); [email protected] (O.B.M.); [email protected] (M.S.) 2 Chemical Engineering Department, Universiti Teknologi PETRONAS, Seri Iskandar 32610, Malaysia; [email protected] 3 Laboratory of Biocomposite Technology, Institute of Tropical Forest, and Forest Products (INTROP), Universiti Putra Malaysia, Serdang 43400, Malaysia; [email protected] 4 Advanced Engineering Materials and Composites Research Centre (AEMC), Department of Mechanical and Manufacturing Engineering, Faculty of Engineering, Universiti Putra Malaysia, Serdang 43400, Malaysia 5 Electrical and Electronics Engineering Department, Universiti Teknologi PETRONAS, Seri Iskandar 32610, Malaysia; [email protected] 6 Department of Manufacturing and Materials Engineering, International Islamic University Malaysia, Kuala Lumpur 53100, Malaysia; [email protected] * Correspondence: [email protected] (M.A.A.); [email protected] (H.H.Y.) Citation: Alam, M.A.; Ya, H.H.; Abstract: The tenacious thirst for fuel-saving and desirable physical and mechanical properties Yusuf, M.; Sivraj, R.; Mamat, O.B.; of the materials have compelled researchers to focus on a new generation of aluminum hybrid Sapuan, S.M.; Masood, F.; Parveez, B.; composites for automotive and aircraft applications. This work investigates the microhardness Sattar, M. Modeling, Optimization behavior and microstructural characterization of aluminum alloy (Al 7075)-titanium carbide (TiC)- and Performance Evaluation of graphite (Gr) hybrid composites. -
Residual Stress, Microstructure and Mechanical Properties in Thick 6005A-T6 Aluminium Alloy Friction Stir Welds
metals Article Residual Stress, Microstructure and Mechanical Properties in Thick 6005A-T6 Aluminium Alloy Friction Stir Welds 1, 2, 3 4 5 1 Xiaolong Liu y, Pu Xie y , Robert Wimpory , Wenya Li , Ruilin Lai , Meijuan Li , Dongfeng Chen 1, Yuntao Liu 1 and Haiyan Zhao 6,* 1 Department of Nuclear Physics, China Institute of Atomic Energy, Beijing 102413, China 2 CRRC Changchun Railway Vehicles Co. Ltd., Changchun 130000, China 3 Helmholtz-Zentrum Berlin für Energie und Materialien, Hahn Meitner Platz 1, 14109 Berlin, Germany 4 Shanxi Key Laboratory of Friction Welding Technologies, School of Materials Science and Engineering, Northwestern Polytechnical University, Xi’an 710072, China 5 Department of Mechanical and Electrical Engineering, Central South University, Changsha 410083, China 6 State Key Laboratory of Tribology, Department of Mechanical Engineering, Tsinghua University, Beijing 100084, China * Correspondence: [email protected]; Tel.: +86-10-6278-4578 These authors contributed equally to this work and should be considered as co-first authors. y Received: 3 July 2019; Accepted: 18 July 2019; Published: 21 July 2019 Abstract: Plates (37 mm thick) of 6005A-T6 aluminum alloy were butt joined by a single-sided and double-sided friction stir welding (FSW). The 3D residual stresses in the joints were determined using neutron diffraction. The microstructures were characterized by a transmission electron microscope (TEM) and electron backscatter diffraction (EBSD). In the single-sided FSW specimen, there were acceptable mechanical properties with a tensile strength of 74.4% of base metal (BM) and low residual stresses with peak magnitudes of approximately 37.5% yield strength of BM were achieved. -
Age Hardening of Extruded AA 6005A Aluminium Alloy Powders
Article Age Hardening of Extruded AA 6005A Aluminium Alloy Powders Iria Feijoo 1,*, Marta Cabeza 1, Pedro Merino 1, Gloria Pena 1 and Pilar Rey 2 1 Department of Materials Engineering, Applied Mechanical and Construction, ENCOMAT Group, University of Vigo, EEI, E36310 Vigo, Spain 2 AIMEN, Technological Centre, Polígono de Cataboi, E36418 Porriño, Pontevedra, Spain * Correspondence: [email protected]; Tel.: +34-986-81-22-29 Received: 14 June 2019; Accepted: 18 July 2019; Published: 19 July 2019 Abstract: Pre-alloyed micron-sized 6005A Al alloy (AA 6005A) powders, with a Mg/Si atomic ratio of 0.75, obtained by high pressure inert gas atomization were consolidated by uniaxial cold pressing at 200 MPa into cylindrical Al containers and hot extruded at 450, 480 and 500 °C with an extrusion rate of 7:1, followed by artificial T6 precipitation hardening. Ageing conditions were varied between 170 °C and 190 °C and times of 6, 7 and 8 hours. The microstructure of the extruded profiles was analysed using X-Ray diffractometry (XRD), light optical microscopy (LOM), scanning electron microscopy (SEM), and transmission electron microscopy (TEM). Differential scanning calorimetry (DSC) was used to study the possible phase transformations. After our results, the peak-aging hardness condition was achieved at 180 °C for 6 h. Mechanical properties of the powder metallurgy (P/M) aluminium alloys consolidated by hot extrusion were superior to those of the extruded profiles of wrought alloy using conventional ingot metallurgy (I/M) billets. AA 6005A wrought P/M alloy via T6 heat treatment shown yield stress of 317 MPa and elongation of 21% at the extrusion pre-heating temperature of 500 °C. -
Aluminium Sheet, Coil, Plate, Treadplate & Extrusions
Aluminium Sheet, Coil, Plate, Treadplate & Extrusions & & Treadplate , luminium Sheet, Coil, Plate Coil, Sheet, luminium A Extrusions 8 8 Photography courtesy of Alcoa Aluminium and INCAT. www.atlassteels.com.au Atlas Steels – Product Reference Manual Section 8 – Aluminium Sheet, Coil, Plate, Treadplate & Extrusions Aluminium Advantages of using Aluminium 1 Light weight – approximately /3 the density of steel. Strength – some alloys can be substantially strengthened by work or by heat treatment. Workability – easy formability, machinability and readily welded. Corrosion resistance – varies depending on the alloy; the best resist marine exposure. Non-toxic – often used in contact with food. Non-magnetic and non-sparking. Electrical conductivity – very high; sometimes used for electrical conductors. Thermal conductivity – high. Reflectivity – bright finish options available. Specifications Flat rolled aluminium alloy products stocked by Atlas generally comply with ASTM B209M or ASTM B928M with dimensions in ANSI H35.2. There is very close agreement between these standards and Australian/New Zealand standard AS/NZS 1734 and again close agreement with European standard EN 573. Aluminium Association publication “Aluminium standards and data” gives a very accessible summary of both specified data and useful information. Aluminium products are often cited as compliant with “AA specs” based on this. Treadplate is specified in ASTM B632M but this does not cover the product well. Most mills produce to their own specifications and particularly