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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. -
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. -
Establishing a Correlation Between Interfacial Microstructures and Corro- Sion Initiation Sites in Al/Cu Joints by SEM-EDS and AFM-SKPFM
This may be the author’s version of a work that was submitted/accepted for publication in the following source: Sarvghad Moghaddam, Madjid, Parvizi, R., Davoodi, Ali, Haddad- Sabzevar, Mohsen, & Imani, Amin (2014) Establishing a correlation between interfacial microstructures and corro- sion initiation sites in Al/Cu joints by SEM-EDS and AFM-SKPFM. Corrosion Science, 79, pp. 148-158. This file was downloaded from: https://eprints.qut.edu.au/95930/ c Consult author(s) regarding copyright matters This work is covered by copyright. Unless the document is being made available under a Creative Commons Licence, you must assume that re-use is limited to personal use and that permission from the copyright owner must be obtained for all other uses. If the docu- ment is available under a Creative Commons License (or other specified license) then refer to the Licence for details of permitted re-use. It is a condition of access that users recog- nise and abide by the legal requirements associated with these rights. If you believe that this work infringes copyright please provide details by email to [email protected] License: Creative Commons: Attribution-Noncommercial-No Derivative Works 2.5 Notice: Please note that this document may not be the Version of Record (i.e. published version) of the work. Author manuscript versions (as Sub- mitted for peer review or as Accepted for publication after peer review) can be identified by an absence of publisher branding and/or typeset appear- ance. If there is any doubt, please refer to the published source. https://doi.org/10.1016/j.corsci.2013.10.039 Accepted Manuscript Establishing a Correlation between Interfacial Microstructures and Corrosion Initiation Sites in Al/Cu Joints by SEM-EDS and AFM-SKPFM M. -
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. -
191002 Knowledge: K1.02 [2.7/2.9] Qid: P6 (B1806)
NRC Generic Fundamentals Examination Question Bank--PWR May 2020 TOPIC: 191002 KNOWLEDGE: K1.02 [2.7/2.9] QID: P6 (B1806) Density input is normally used in steam flow instruments to convert __________ into __________. A. mass flow rate; volumetric flow rate B. volumetric flow rate; mass flow rate C. mass flow rate; differential pressure D. differential pressure; volumetric flow rate ANSWER: B. TOPIC: 191002 KNOWLEDGE: K1.02 [2.7/2.9] QID: P305 (B2906) If the steam pressure input to a density-compensated steam flow instrument fails high, the associated flow rate indication will... A. decrease, because the density input has decreased. B. increase, because the density input has decreased. C. decrease, because the density input has increased. D. increase, because the density input has increased. ANSWER: D. -1- Sensors and Detectors NRC Generic Fundamentals Examination Question Bank--PWR May 2020 TOPIC: 191002 KNOWLEDGE: K1.02 [2.7/2.9] QID: P406 (B1606) The density compensating input to a steam flow instrument is used to convert volumetric flow rate into… A. velocity flow rate. B. gallons per minute. C. mass flow rate. D. differential flow rate. ANSWER: C. -2- Sensors and Detectors NRC Generic Fundamentals Examination Question Bank--PWR May 2020 TOPIC: 191002 KNOWLEDGE: K1.02 [2.7/2.9] QID: P1212 If the steam pressure input to a density-compensated steam flow instrument fails low, the indicated flow rate will... A. increase, because the density input has increased. B. decrease, because the density input has increased. C. increase, because the density input has decreased. D. decrease, because the density input has decreased. -
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. -
Corrosion Behaviour of Aluminum Alloys Weldments: a Literature Survey
6 III March 2018 http://doi.org/10.22214/ijraset.2018.3464 International Journal for Research in Applied Science & Engineering Technology (IJRASET) ISSN: 2321-9653; IC Value: 45.98; SJ Impact Factor: 6.887 Volume 6 Issue III, March 2018- Available at www.ijraset.com Corrosion Behaviour of Aluminum Alloys Weldments: A Literature Survey Vilas Hans1, Prabdeep Singh Bajwa2 1, 2 Department of Mechanical Engineering, LRIET, Solan, Himachal Pradesh, India Abstract: Aluminum alloys of 5xxx series and their welded joints show good resistance to corrosion in sea water. Metallic corrosion takes place in marine environments. In the ship manufacturing industries, welding is used to join the different aluminum parts of the ship structure, these weldments are generally remaining dip in saline water of sea or remain in salt foggy atmosphere, which gets eroded early when comes in contact with salt-water solution. A literature survey has been carried out to understanding of welding and corrosion of aluminum alloys. Keywords: 5xxx Aluminum alloys; marine corrosion; welding. I. INTRODUCTION Metallic corrosion takes place in wet environments when the chemical or electrochemical reaction between a metal and the surrounding environment results in the oxidation of the metal. For corrosion to occur, electrons are produced by the anodic oxidation of the metal must be consumed in a cathodic reaction. These two processes can take place on different parts of a metal structure providing that there is a conducting path for the electrons between the two, and a continuous electrolyte path for ion transport. Aluminium is highly reactive, with a negative standard electrode potential of - 1660mV, and is therefore unstable in the presence of water. -
Thermophysical Properties of Materials for Water Cooled Reactors
XA9744411 IAEA-TECDOC-949 Thermophysical properties of materials for water cooled reactors June 1997 ¥DL 2 8 fe 2 Q The IAEA does not normally maintain stocks of reports in this series. However, microfiche copies of these reports can be obtained from IN IS Clearinghouse International Atomic Energy Agency Wagramerstrasse 5 P.O. Box 100 A-1400 Vienna, Austria Orders should be accompanied by prepayment of Austrian Schillings 100,- in the form of a cheque or in the form of IAEA microfiche service coupons which may be ordered separately from the IN IS Clearinghouse. IAEA-TECDOC-949 Thermophysical properties of materials for water cooled reactors WJ INTERNATIONAL ATOMIC ENERGY AGENCY /A\ June 1997 The originating Section of this publication in the IAEA was: Nuclear Power Technology Development Section International Atomic Energy Agency Wagramerstrasse 5 P.O. Box 100 A-1400 Vienna, Austria THERMOPHYSICAL PROPERTIES OF MATERIALS FOR WATER COOLED REACTORS IAEA, VIENNA, 1997 IAEA-TECDOC-949 ISSN 1011-4289 ©IAEA, 1997 Printed by the IAEA in Austria June 1997 FOREWORD The IAEA Co-ordinated Research Programme (CRP) to establish a thermophysical properties data base for light and heavy water reactor materials was organized within the framework of the IAEA's International Working Group on Advanced Technologies for Water Cooled Reactors. The work within the CRP started in 1990. The objective of the CRP was to collect and systematize a thenmophysical properties data base for light and heavy water reactor materials under normal operating, transient and accident conditions. The important thermophysical properties include thermal conductivity, thermal diffusivity, specific heat capacity, enthalpy, thermal expansion and others. -
Design of a Kite Controller for Airborne Wind Energy
Dissertation for Masters of Science in Engineering Design of a Kite Controller for Airborne Wind Energy Matteo Milandri February 2015 University of Cape Town University of Cape Town Faculty Engineering and the Built Environment Electrical Engineering Department The copyright of this thesis vests in the author. No quotation from it or information derived from it is to be published without full acknowledgement of the source. The thesis is to be used for private study or non- commercial research purposes only. Published by the University of Cape Town (UCT) in terms of the non-exclusive license granted to UCT by the author. University of Cape Town Supervised by Samuel Ginsberg Dr. Ian de Vries Declaration I know the meaning of plagiarism and declare that all the work in the document, save for that which is properly acknowledged, is my own. Matteo F. Milandri ___________________ i Abstract Airborne wind energy is a field of technology being developed to make use of the vast, renewable wind power resource which is above the reach of traditional wind turbines, without the need for a large tower. Much analytical research has been undertaken in recent years to better understand the problem space. However, there are relatively few working systems that demonstrate their functioning and can be compared with simulations and theory. Off-grid power systems still rely heavily on diesel generators, so devices that tap renewable energy sources with similar ease of deployment and lower cost of energy would help this sector to reduce its reliance on expensive, polluting, fossil fuels. The development of these systems is often performed by teams with business interests leaving little open access content available regarding the design process of such devices or the data that they provide. -
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 -
Applications for Aluminum Alloys and Tempers
CHAPTER 6 Applications for Aluminum Alloys and Tempers THERE ARE AT LEAST two approaches to overviewing important applications of aluminum alloys: by alloy class, as initiated in Chapter 3 and carried out in greater detail subsequently, and by type of application. Both approaches are considered in this chapterϪa review first by alloy class and then by application. Readers are referred to Aluminum: Technology, Applications and Environment (see Chapter 8) for more detailed information on many of the applications mentioned in this chapter. All photographs are courtesy of the Aluminum Association unless otherwise indicated, many from the reference noted in the previous paragraph. Applications by Alloy Class Wrought Alloys 1xxx, Pure Aluminum. The major characteristics of the 1xxx series are: O Strain hardenable O Exceptionally high formability, corrosion resistance, and electrical conductivity O Typical ultimate tensile strength range: 70 to 185 MPa (10–27 ksi) O Readily joined by welding, brazing, and soldering The 1xxx series represents the commercially pure (CP) aluminum, ranging from the baseline 1100 (99.00% min Al) to relatively purer 1050/1350 88 / Introduction to Aluminum Alloys and Tempers (99.50% min Al) and 1175 (99.75 % min Al). The 1xxx series of alloys are strain hardenable but would not be used where strength is a prime consideration. The primary uses of the 1xxx series would be applications in which the combination of extremely high corrosion resistance and formability are required (e.g., foil and strip for packaging, chemical equipment, tank car or truck bodies, spun hollowware, and elaborate sheet metal work). Electrical applications are one major use of the 1xxx series, primarily 1350, which has relatively tight controls on those impurities that might lower electrical conductivity.