BS EN 4632-006-2013 Aerospace series Weldability and brazeability of materials in aerospace constructions Homogeneous assemblies of titanium alloys《航空航天系列 航空航天结构用材料的可焊接性和可钎焊性 钛合金的均.pdf

《BS EN 4632-006-2013 Aerospace series Weldability and brazeability of materials in aerospace constructions Homogeneous assemblies of titanium alloys《航空航天系列 航空航天结构用材料的可焊接性和可钎焊性 钛合金的均.pdf》由会员分享，可在线阅读，更多相关《BS EN 4632-006-2013 Aerospace series Weldability and brazeability of materials in aerospace constructions Homogeneous assemblies of titanium alloys《航空航天系列 航空航天结构用材料的可焊接性和可钎焊性 钛合金的均.pdf（30页珍藏版）》请在麦多课文档分享上搜索。

1、raising standards worldwideNO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBSI Standards PublicationBS EN 4632-006:2013Aerospace series Weldabilityand brazeability of materials inaerospace constructionsPart 006: Homogeneous assemblies oftitanium alloysBS EN 4632-006:2013 BRITIS

2、H STANDARDNational forewordThis British Standard is the UK implementation of EN 4632-006:2013.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 beobtained on request

3、to its secretary.This publication does not purport to include all the necessaryprovisions of a contract. Users are responsible for its correctapplication. The British Standards Institution 2013. Published by BSI StandardsLimited 2013ISBN 978 0 580 67022 0ICS 49.025.01Compliance with a British Standa

4、rd cannot confer immunity fromlegal obligations.This British Standard was published under the authority of theStandards Policy and Strategy Committee on 30 April 2013.Amendments issued since publicationDate Text affectedBS EN 4632-006:2013EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4632-006

5、 March 2013 ICS 49.025.01 English Version Aerospace series - Weldability and brazeability of materials in aerospace constructions - Part 006: Homogeneous assemblies of titanium alloys Srie arospatiale - Soudabilit et brasabilit des matriaux pour constructions arospatiales - Partie 006 : Assemblages

6、homognes des alliages de titane Luft- und Raumfahrt - Schweibarkeit und Ltbarkeit von Werkstoffen im Luft- und Raumfahrzeugbau - Teil 006: Gleichartige Verbindungen aus Titanbasislegierungen This European Standard was approved by CEN on 19 January 2013. CEN members are bound to comply with the CEN/C

7、ENELEC Internal Regulations which stipulate the conditions for giving this European Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the CEN-CENELEC Management Centr

8、e or to any CEN member. This European Standard exists in three official versions (English, French, German). A version in any other language made by translation under the responsibility of a CEN member into its own language and notified to the CEN-CENELEC Management Centre has the same status as the

9、official versions. CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherla

10、nds, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG Management Centre: Avenue Marnix 17, B-1000 Brussels 2013 CEN All rights of exploita

11、tion in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4632-006:2013: EBS EN 4632-006:2013EN 4632-006:2013 (E) 2 Contents Page Foreword 3 1 Scope 4 2 Normative references 4 3 Terms, definitions, symbols and abbreviations .7 4 Use of this standard 8 5 Updating of t

12、his standard .8 6 List of titanium alloys sheets .8 7 Material sheets .9 Bibliography . 26 BS EN 4632-006:2013EN 4632-006:2013 (E) 3 Foreword This document (EN 4632-006:2013) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). After enquiries

13、 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 European Standard shall be given the status of a national sta

14、ndard, either by publication of an identical text or by endorsement, at the latest by September 2013, and conflicting national standards shall be withdrawn at the latest by September 2013. Attention is drawn to the possibility that some of the elements of this document may be the subject of patent r

15、ights. 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 organisations of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Croatia

16、, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the

17、United Kingdom. This standard is part 6 of a series of 8 standards, with: EN 4632-001, Aerospace series Welded and brazed assemblies for aerospace constructions Weldability and brazeability of materials Part 001: General requirements EN 4632-002, Aerospace series Welded and brazed assemblies for aer

18、ospace constructions Weldability and brazeability of materials Part 002: Homogeneous assemblies aluminium and aluminium alloys EN 4632-003, Aerospace series Weldability and brazeability of materials in aerospace constructions Part 003: Welding and brazing of homogeneous assemblies of unalloyed and l

19、ow alloy steels EN 4632-004, Aerospace series Welded and brazed assemblies for aerospace constructions Weldability and brazeability of materials Part 004: Homogeneous assemblies highly alloyed steels EN 4632-005, Aerospace series Weldability and brazeability of materials in aerospace constructions P

20、art 005: Homogeneous assemblies of heat resisting Ni or Co base alloys EN 4632-007, Aerospace series Weldability and brazeability of materials in aerospace constructions Part 007: Homogeneous assemblies of miscellaneous alloys BS EN 4632-006:2013EN 4632-006:2013 (E) 4 1 Scope This European Standard

21、defines degrees of weldability and brazeability for materials or families of materials used in the aerospace applications. It comprises a series of sheets, by materials or by material family, which: indicate the main titles, the typical chemical composition and the main characteristics, contain reco

22、mmendations for welding and brazing, indicate a degree of weldability or brazeability for a given process under defined conditions. It is applicable without restriction for the manufacturing of new parts or for repair. 2 Normative references The following documents, in whole or in part, are normativ

23、ely referenced in this document and are indispensable for its application. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 3120, Aerospace series Titanium alloy TI-P64003 Cold worked an

24、d stress relieved Seamless tube for pressure systems 4 mm D 51 mm 690 MPa Rm 1 030 MPa EN 3310, Aerospace series Titanium alloy TI-P64001 (Ti-6Al-4V) Not heat treated Forging stock, for annealed forgings De 360 mm EN 3311, Aerospace series Titanium alloy TI-P64001 (Ti-6Al-4V) Annealed Bar for machin

25、ing D 110 mm EN 3312, Aerospace series Titanium alloy Ti-6Al-4V Annealed Forgings De 150 mm EN 3313, Aerospace series Titanium alloy TI-P64001 Not heat treated Grade 2 forging stock, for solution treated and aged forgings a or D 360 mm 1)EN 3314, Aerospace series Titanium alloy TI-P64001 Solution tr

26、eated and aged Bar for machining D 75 mm 1)EN 3315, Aerospace series Titanium alloy TI-P64001 Solution treated and aged Forgings De 75 mm 1)EN 3321, Aerospace series Titanium alloy TI-P65001 As forged Grade 1 forging stock, for solution treated and aged forgings a or D 360 mm 1)EN 3322, Aerospace se

27、ries Titanium alloy TI-P65001 Solution treated and aged Grade 1 Forgings De 75 mm 1)EN 3354, Aerospace series Titanium alloy TI-P64001 (Ti-6Al-4V) Annealed Sheet for superplastic forming a 6 mm 1)1) Published as ASD-STAN Prestandard at the date of publication of this standard (www.asd-stan.org). BS

28、EN 4632-006:2013EN 4632-006:2013 (E) 5 EN 3355, Aerospace series Titanium alloy TI-P64001 (Ti-6Al-4V) Annealed Extruded section De 150 mm 900 MPa Rm 1 160 MPa EN 3442, Aerospace series Titanium TI-P99002 Annealed Sheet and strip, hot rolled a 6 mm 390 MPa Rm 540 MPa 1)EN 3443, Aerospace series Titan

29、ium TI-P99003 Annealed Sheet and strip, hot rolled a 6 mm 570 MPa Rm 730 MPa 1)EN 3451, Aerospace series Titanium TI-P99002 Not heat treated Grade 2 forging stock, for annealed forgings a or D 300 mm 1)EN 3453, Aerospace series Titanium TI-P99003 Not heat treated Grade 2 forging stock, for annealed

30、forgings a or D 300 mm 1)EN 3454, Aerospace series Titanium alloy TI-P19001 Not heat treated Grade 2 forging stock, for annealed forgings a or D 300 mm 1)EN 3455, Aerospace series Titanium alloy TI-P19001 Not heat treated Grade 2 forging stocks, for solution treated and aged forgings a or D 300 mm 1

31、)EN 3456, Aerospace series Titanium alloy TI-P64001 (Ti-6Al-4V) Annealed Sheet and strip, hot rolled a 6 mm EN 3460, Aerospace series Titanium TI-P99002 Annealed Bar for machining a or D 150 mm Rm 390 MPa 1)EN 3461, Aerospace series Titanium TI-P99003 Annealed Bar for machining D 150 mm 540 MPa Rm 7

32、40 MPa 1)EN 3462, Aerospace series Titanium alloy TI-P19001 Annealed Bar for machining D 150 mm 1)EN 3463, Aerospace series Titanium alloy TI-P19001 Solution treated and aged Bar for machining D 75 mm 1)EN 3464, Aerospace series Titanium alloy TI-P64001 (Ti-6Al-4V) Annealed Plate 6 mm a 100 mm EN 34

33、94, Aerospace series Titanium alloy TI-P19001 Grade 2 Solution treated and aged Forgings De 75 mm 1)EN 3495, Aerospace series Titanium alloy TI-P19001 Grade 2 Annealed Forgings De 150 mm 1)EN 3496, Aerospace series Titanium TI-P99003 Grade 2 Annealed Forgings De 150 mm 1)EN 3498, Aerospace series Ti

34、tanium TI-P99002 Annealed Sheet and strip, cold rolled a 6 mm 390 MPa Rm 540 MPa 1)EN 3499, Aerospace series Titanium TI-P99003 Annealed Sheet and strip, cold rolled a 6 mm 570 MPa Rm 730 MPa 1)EN 3735, Aerospace series Titanium alloy TI-P65002 Solution treated and aged Bar for machining D 75 mm 1)E

35、N 3736, Aerospace series Titanium alloy TI-P65002 Grade 2 Solution treated and aged Forgings De 75 mm 1)BS EN 4632-006:2013EN 4632-006:2013 (E) 6 EN 3737, Aerospace series Titanium alloy TI-P65002 Not heat treated Grade 2 forging stock, for solution treated and aged forgings a or D 360 mm 1)EN 3859,

36、 Aerospace series Titanium alloy TI-P19001 Annealed Sheet and strip, hot rolled a 6 mm 1)EN 3860, Aerospace series Titanium alloy TI-P19001 Annealed Sheet and strip, cold rolled a 6 mm 1)EN 3870, Aerospace series Titanium alloy TI-P19001 Solution treated and aged Sheet and strip, hot rolled a 6 mm 1

37、)EN 3871, Aerospace series Titanium alloy TI-P19001 Solution treated and aged Sheet and strip, cold rolled a 6 mm 1)EN 3892, Aerospace series Titanium alloy TI-W64001 Filler metal for welding EN 3965, Aerospace series Titanium alloy TI-B17001 Filler metal for brazing Rolled foil EN 4632-001:2008, Ae

38、rospace series Welded and brazed assemblies for aerospace constructions Weldability and brazeability of materials Part 001: General requirements EN 4632-007, Aerospace series Weldability and brazeability of materials in aerospace constructions Part 007: Homogeneous assemblies of miscellaneous alloys

39、 2)EN 10052, Vocabulary of heat treatment terms for ferrous products EN ISO 4063:2009, Welding and allied processes Nomenclature of processes and reference numbers (ISO 4063:2009) EN ISO 24034, Welding consumables Solid wires and rods for fusion welding of titanium and titanium alloys Classification

40、 (ISO 24034:2010) AMS 4897, Titanium alloy, sheet, strip, and plate 77 Ti 15Mo - 3.0AI - 2.8Cb - 0.20Si 3)AMS 4911, Titanium alloy, sheet, strip, and plate 6Al - 4V annealed 3)AMS 4920, Titanium alloy, forgings 6Al - 4V alpha-beta or beta processed, annealed 3)AMS 4928, Titanium alloy bars, wire, fo

41、rgings, rings, and drawn shapes, 6Al - 4V, annealed 3)AMS 4930, Titanium alloy bars, wire, forgings, and rings, 6Al - 4V, extra low interstitial, annealed 3)AMS 4934, Titanium alloy, extrusions and flash welded rings, 6Al - 4V, solution heat treated and aged 3)AMS 4935, Titanium alloy, extrusions an

42、d flash welded rings 6Al - 4V annealed beta processed 3)AMS 4965, Titanium alloy, bars, wire, forgings, and rings 6.0Al - 4.0V solution heat treated and aged 3)AMS 4966, Titanium alloy, forgings 5Al - 2.5Sn annealed, 110 ksi (758 MPa) yield strength 3)AMS 4967, Titanium alloy, bars, wire, forgings,

43、and rings, 6.0Al - 4.0V, annealed, heat treatable 3)2) In preparation at the date of publication. 3) Published by: SAE National (US) Society of Automotive Engineers http:/www.sae.org/. BS EN 4632-006:2013EN 4632-006:2013 (E) 7 AMS 4981, Titanium alloy bars, wire, and forgings 6.0Al - 2.0Sn - 4.0Zr -

44、 6.0Mo solution and precipitation heat treated 3)AMS 4985, Titanium alloy, investment castings 6Al 4V 130 Uts, 120 Ys, 6 % El hot isostatically pressed anneal optional or when specified 3)AMS 4991, Titanium alloy castings, investment 6Al - 4V hot isostatic pressed, annealed optional 3)AMS 4995, Bill

45、ets and preforms 5Al - 2Sn - 2Zr - 4Cr - 4M - 0.100 premium quality, powder-metallurgy product 3)ASTM B 265, Standard specification for titanium and titanium alloy strip, sheet, and plate 4)AWS A5.16, Specification for titanium and titanium alloy welding electrodes and rods 5)3 Terms, definitions, s

46、ymbols and abbreviations For the purposes of this document, the terms, definitions, symbols and abbreviations given in EN 4632-001:2008 and EN ISO 4063:2009 apply. PJHT : Post joining (brazing or diffusion brazing) heat treatment PWHT : Post welding heat treatment FSW : Friction stir welding 15 : Pl

47、asma arc welding 21 : Resistance spot welding 22 : Resistance seam welding 24 : Resistance flash welding 42 : Inertia friction welding 45 : Diffusion welding 51 : Electron beam welding 522 : Gas laser welding 91 : Brazing 111 : Shielded metal arc welding 131 : Gas metal arc welding 141 : Gas tungste

48、n arc welding 919 : Diffusion brazing 924 : Vacuum brazing 4) Published by: ASTM National (US) American Society for Testing and Materials http:/www.astm.org/. 5) Published by: AWS, 550 N.W. LeJeune Road, Miami, Florida 33126. BS EN 4632-006:2013EN 4632-006:2013 (E) 8 4 Use of this standard The index of material sheets contained in this standard, classified by family based on the main element used in the ch