BS EN 4632-002-2008 Aerospace series - Welded and brazed assemblies for aerospace constructions - Weldability and brazeability of materials - Part 002 Homogeneous assemblies nalumi.pdf
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1、BS EN 4632-002:2008ICS 49.025.01NO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBRITISH STANDARDAerospace series Welded and brazed assemblies for aerospace constructions Weldability and brazeability of materialsPart 002: Homogeneous assemblies aluminium and aluminium alloysLice
2、nsed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 15/12/2009 07:35, Uncontrolled Copy, (c) BSIThis British Standardwas published underthe authority of theStandards Policy andStrategy Committee on 30September 2009 BSI 2009ISBN 978 0 580 60592 5Amendments/corrigenda issued since publicationDate Comme
3、ntsBS EN 4632-002:2008National forewordThis British Standard is the UK implementation of EN 4632-002:2008.The UK participation in its preparation was entrusted to TechnicalCommittee ACE/61, Metallic materials for aerospace purposes.A list of organizations represented on this committee can be obtaine
4、d onrequest to its secretary.This publication does not purport to include all the necessary provisionsof a contract. Users are responsible for its correct application.Compliance with a British Standard cannot confer immunityfrom legal obligations.Licensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS
5、, 15/12/2009 07:35, Uncontrolled Copy, (c) BSIBS EN 4632-002:2008EUROPEAN STANDARDNORME EUROPENNEEUROPISCHE NORMEN 4632-002April 2008ICS 49.025.01English VersionAerospace series - Welded and brazed assemblies foraerospace constructions - Weldability and brazeability ofmaterials - Part 002: Homogeneo
6、us assemblies aluminium andaluminium alloysSrie arospatiale - Assemblages souds et brass pourconstructions arospatiales - Soudabilit et brasabilit desmatriaux - Partie 002 : Assemblages homognes delaluminium et des alliages daluminiumLuft- und Raumfahrt - Schwei- und Ltverbindungen frdie Luft- und R
7、aumfahrt - Schweibarkeitsgrad undLtbarkeitsgrad von Werkstoffen - Teil 002: GleichartigeVerbingungen Aluminium und AluminiumlegierungenThis European Standard was approved by CEN on 7 March 2008.CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions f
8、or giving this EuropeanStandard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such nationalstandards may be obtained on application to the CEN Management Centre or to any CEN member.This European Standard exists in three official
9、 versions (English, French, German). A version in any other language made by translationunder the responsibility of a CEN member into its own language and notified to the CEN Management Centre has the same status as theofficial versions.CEN members are the national standards bodies of Austria, Belgi
10、um, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland,France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal,Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.EUROPEAN COMMITTEE FOR STA
11、NDARDIZATIONCOMIT EUROPEN DE NORMALISATIONEUROPISCHES KOMITEE FR NORMUNGManagement Centre: rue de Stassart, 36 B-1050 Brussels 2008 CEN All rights of exploitation in any form and by any means reservedworldwide for CEN national Members.Ref. No. EN 4632-002:2008: ELicensed Copy: Wang Bin, ISO/EXCHANGE
12、 CHINA STANDARDS, 15/12/2009 07:35, Uncontrolled Copy, (c) BSIBS EN 4632-002:2008EN 4632-002:2008 (E) 2 Contents Page Foreword3 1 Scope 4 2 Normative references 4 3 Terms, definitions, symbols and abbreviations .5 4 Use of this standard 5 5 Updating this standard5 6 Index of aluminium and aluminium
13、alloy sheets6 7 Material sheets.7 Bibliography 31 Licensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 15/12/2009 07:35, Uncontrolled Copy, (c) BSIBS EN 4632-002:2008EN 4632-002:2008 (E) 3 Foreword This document (EN 4632-002:2008) has been prepared by the Aerospace and Defence Industries Associati
14、on of Europe - Standardization (ASD-STAN). After enquiries and votes carried out in accordance with the rules of this Association, this Standard has received the approval of the National Associations and the Official Services of the member countries of ASD, prior to its presentation to CEN. This Eur
15、opean Standard shall be given the status of a national standard, either by publication of an identical text or by endorsement, at the latest by October 2008, and conflicting national standards shall be withdrawn at the latest by October 2008. Attention is drawn to the possibility that some of the el
16、ements of this document may be the subject of patent rights. CEN and/or CENELEC shall not be held responsible for identifying any or all such patent rights. According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this
17、European Standard: Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the Un
18、ited Kingdom. Licensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 15/12/2009 07:35, Uncontrolled Copy, (c) BSIBS EN 4632-002:2008EN 4632-002:2008 (E) 4 1 Scope This standard defines degrees of weldability and brazeability for materials or families of materials used in the aerospace industry. It c
19、omprises a series of sheets, by materials or by material family which: indicate the main titles, the typical chemical composition and the main characteristics, contain recommendations for welding and brazing, indicate a degree of weldability or brazeability for a given process under defined conditio
20、ns. indicate a value of the mechanical strength coefficient of the welded joint for each welding process, when it could be extracted from bibliographic references referring to it. The joint coefficient is expressed as a ratio of the tensile strength of the welded joint to the tensile strength of the
21、 base alloy. It is applicable without restriction for the manufacturing of new parts or for repair. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the edition cited applies. For undated references, the late
22、st edition of the referenced document (including any amendments) applies. EN 485-1, Aluminium and aluminium alloys Sheet, strip and plate Part 1: Technical conditions for inspection and delivery. EN 485-2, Aluminium and aluminium alloys Sheet, strip and plate Part 2: Mechanical properties. EN 515, A
23、luminium and aluminium alloys Wrought products Temper designations. EN 573-2, Aluminium and aluminium alloys Chemical composition and form of wrought products Part 2: Chemical symbol based designation system. EN 573-3, Aluminium and aluminium alloys Chemical composition and form of wrought products
24、Part 3: Chemical composition and form of products. EN 1011-4, Welding Recommendations for welding of metallic materials Part 4: Arc welding of aluminium and aluminium alloys. EN 1706, Aluminium and aluminium alloys Castings Chemical composition and mechanical properties. EN 2032-1, Aerospace series
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