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本文(ASD-STAN PREN 4632-002-2007 Aerospace series Welded and brazed assemblies for aerospace constructions Weldability and brazeability of materials Part 002 Homogeneous assemblies alum.pdf)为本站会员(李朗)主动上传,麦多课文库仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文库(发送邮件至master@mydoc123.com或直接QQ联系客服),我们立即给予删除!

ASD-STAN PREN 4632-002-2007 Aerospace series Welded and brazed assemblies for aerospace constructions Weldability and brazeability of materials Part 002 Homogeneous assemblies alum.pdf

1、ASD STANDARD NORME ASD ASD NORM prEN 4632-002 Edition P 1 January 2007 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATIONGulledelle 94 - B-1200 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 763 3565 - www.asd-stan.orgICS: Descriptors: ENGLISH VERSION Aerospace

2、series Welded and brazed assemblies for aerospace constructions Weldability and brazeability of materials Part 002: Homogeneous assemblies aluminium and aluminium alloys Srie arospatiale Assemblages souds et brass pour constructions arospatiales Soudabilit et brasabilit des matriaux Partie 002 : Ass

3、emblages homognes de laluminium et des alliages daluminium Luft- und Raumfahrt Schwei- und Ltverbindungen fr die Luft- und Raumfahrt Schweibarkeitsgrad und Ltbarkeitsgrad von Werkstoffen Teil 002: Gleichartige Verbingungen Aluminium und Aluminiumlegierungen This “Aerospace Series“ Prestandard has be

4、en drawn up under the responsibility of ASD-STAN (The AeroSpace and Defence Industries Association of Europe - Standardization). It is published for the needs of the European Aerospace Industry. It has been technically approved by the experts of the concerned Domain following member comments. Subseq

5、uent to the publication of this Prestandard, the technical content shall not be changed to an extent that interchangeability is affected, physically or functionally, without re-identification of the standard. After examination and review by users and formal agreement of ASD-STAN, it will be submitte

6、d as a draft European Standard (prEN) to CEN (European Committee for Standardization) for formal vote and transformation to full European Standard (EN). The CEN national members have then to implement the EN at national level by giving the EN the status of a national standard and by withdrawing any

7、national standards conflicting with the EN. Edition approved for publication 31 January 2007 Comments should be sent within six months after the date of publication to ASD-STAN Metallic Material Domain Copyright 2007 by ASD-STAN prEN 4632-002:20072 Contents Page Foreword2 1 Scope 3 2 Normative refer

8、ences 3 3 Terms, definitions, symbols and abbreviations .4 4 Use of this standard 4 5 Updating this standard4 6 Index of aluminium and aluminium alloy sheets5 7 Material sheets.6 Bibliography. 30 Foreword This standard was reviewed by the Domain Technical Coordinator of ASD-STANs Metallic Material D

9、omain. After inquiries and votes carried out in accordance with the rules of ASD-STAN defined in ASD-STANs General Process Manual, this standard has received approval for Publication. prEN 4632-002:20073 1 Scope This standard defines degrees of weldability and brazeability for materials or families

10、of materials used in the aerospace industry. 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 recommendations for welding and brazing, indicate a degree of weldability or brazea

11、bility for a given process under defined conditions. 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 o

12、f the welded joint to the tensile strength of the 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 editio

13、n cited applies. For undated references, the latest 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 a

14、nd plate Part 2: Mechanical properties. EN 515, Aluminium 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 C

15、hemical composition and form of wrought products Part 3: Chemical composition. 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 Casting Chemical composition and mechanical properties. E

16、N 2032-1, Aerospace series Metallic materials Part 1: Conventional designation. EN 2726, Aerospace series Aluminium alloy AL-C42201 T6 Sand casting a 20 mm. 1)EN 2728, Aerospace series Aluminium alloy AL-C42101 T6 Sand casting a 20 mm. 1)EN 4632-001, Welded and brazed assemblies for aerospace constr

17、uctions Weldability and brazeability of materials Part 001: General requirements. 1)EN ISO 18273, Welding consumables Wire electrodes, wires and rods for welding of aluminium and aluminium alloys Classification. 1) Published as ASD Prestandard at the date of publication of this standard. prEN 4632-0

18、02:20074 ANSI/AWS A5.10, Specification for Bare Aluminum and Aluminum-Alloy Welding Electrodes and Rods. 2)ASTM/ANSI B209, Standard Specification for Aluminum and Aluminum-Alloy Sheet and Plate. SAE-AMS 4031, Aluminum alloy, sheet and plate 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-0) annealed.

19、 3)SAE-AMS 4191, Aluminum Alloy, Welding Wire 6.3Cu - 0.30Mn - 0.18Zr - 0.15Ti - 0.10V (2319). 3)SAE-AMS-QQ-A-250/30, Aluminium alloy 2219, plate and sheet. 3)SAE-AMS-A-21180, Aluminum-alloy castings, high strength. 3)3 Terms, definitions, symbols and abbreviations For the purposes of this document,

20、 the terms and definitions given in EN 4632-001 apply. PWHT: Post-Welding Heat Treatment F: Foil p: powder w: wire AFB: Air Furnace Brazing FLB: Flame Brazing VFB: Vacuum Furnace Brazing 4 Use of this standard The index of material sheets contained in this standard, classified by family based on the

21、 main element used in the chemical composition and on the alloy structure, is given in Clause 6 in this standard. The degree of weldability or brazeability to be used is the value indicated by the material sheet considered for the process chosen. In the operating cycle, choose thermal states that gi

22、ve the lowest degree in preference. If two degrees are indicated, the responsible person must select the degree that is most appropriate for the definition of the assembly. 5 Updating this standard See EN 4632-001. 2) Published by: AWS, 550 N.W. LeJeune Road, Miami, Florida 33126. 3) Published by: S

23、ociety of Automotive Engineers, Inc. (SAE), 400 Commonwealth Drive, Warrendale, PA 15096-0001, USA. prEN 4632-002:20075 6 Index of aluminium and aluminium alloy sheets 6.1 Index by material family family 1000: sheet 7.1 family 2000: sheets 7.2 to 7.7 family 5000: sheets 7.8 and 7.9 family 6000: shee

24、t 7.10 family 7000: sheets 7.11 and 7.12 foundry alloys family: sheet 7.13 6.2 Numeric index Sheet Material 7.1 1050A - 1060 7.2 7.3 7.4 7.5 7.6 7.7 2001 2014 2017A 2024 2219 2618A 7.8 7.9 5056A, 5083, 5086, 5182, 5456 5754 7.10 6005A, 6013, 6016, 6056, 6060, 6061, 6063, 6081, 6082, 6181 7.11 7.12 7

25、020, 7051 7050, 7075, 7175, 7475 7.13 Al Si 7 Mg 0,3 and Al Si 7 Mg 0,6 prEN 4632-002:20076 7 Material sheets 7.1 Designation: EN 573-2 : EN AW-1050A; EN AW-1060 Old designation : A5, A6 EN 2032-1 : AL-P1050A; AL-P1060 ISO : Al 99,5; Al 99,6 Other standards : Typical composition: See EN 573-3. Grade

26、 Al Si Fe Cu Mn Mg Zn Ti 1050A base 0,25 0,40 0,05 0,05 0,05 0,07 0,05 1060 base 0,25 0,35 0,05 0,03 0,03 0,05 0,05 Structure: Without structural hardening Particular characteristics: Recommendations for welding and filling with EN AW-1050A and EN AW-1060 Process Thickness range in mm State before w

27、elding PWHT Degree of weldabilityJoint coefficientComments and bibliographic references OA O or H111 none 1 TIG 2 O or H111 none 1 1 Filler metal same grade 1050 or 1080 45 EBW O or H111 none 1 1 RSEW, RSW O or H111 or H24 none 2 prEN 4632-002:20077 7.2 Designation: EN 573-2 : EN AW-2001 Old designa

28、tion : AU6 MGT EN 2032-1 : AL-P2001- ISO : Al Cu 5,5 Mg Mn Other standards : Typical composition: See EN 573-3. Grade Al Si Fe Cu Mn Mg Cr Zn Ti Ni Zr 2001- base 0,20 0,20 5,2 to6,0 0,15 to 0,50 0,20 to 0,45 0,10 0,10 0,20 0,05 0,05 Structure: With structural hardening Particular characteristics: Re

29、commendations for welding and filling with EN AW-2001 Process Thickness range in mm State before welding PWHT Degree of weldabilityJoint coefficient Comments and bibliographic references T4 T 2 Micro-porosity in the weld 49 1 T6 none 2 No porosity Area with large grains in the base metal T4 T 2 Micr

30、o-porosity in the weld 49 8 T6 none 2 No porosity EBW 30 T4 T6 T none 2 2 No porosity 49 RSEW, RSW T6 2 prEN 4632-002:20078 7.3 Designation: EN 573-2 : EN AW-2014 Old designation : AU4 SG EN 2032-1 : AL-P2014- ISO : Al Cu 4 Si Mg Other standards: Typical composition: See EN 573-3. Grade Al Si Fe Cu

31、Mn Mg Cr Zn Ti Ni 2014- base 0,50 to 1,2 0,7 3,9 to 5,0 0,40 to 1,2 0,20 to 0,8 0,10 0,25 0,15 0,10 Al Ti + Zr base 0,20 only for extruded or forged products with agreement between supplier and customer Structure: With structural hardening Particular characteristics: prEN 4632-002:20079 Recommendati

32、ons for welding and filling with EN AW-2014 Process Thickness range in mm State before welding PWHT Degree of weldabilityJoint coefficient Comments and bibliographic references OA 4 TIG 4 T4 T4 2 Porosity in the weld 1 T6 none 2 No porosity and area with large grains in the base metal 50 T4 T6 Micro

33、-porosity 8 T6 none 2 No porosity 50 EBW 30 T4 T6 T6 none 2 to 3 2 to 3 No porosity 50 RSEW, RSW T6 2 FSW 22 6,35 T6 T651 none none 2 2 0,68 43 44 prEN 4632-002:200710 7.4 Designation: EN 573-2 : EN AW-2017A Old designation : AU4G EN 2032-1 : AL-P2017A ISO : Al Cu 4 Mg 1 Other standards : Typical co

34、mposition: See EN 573-3. Grade Al Si Fe Cu Mn Mg Cr Zn Ti + Zr 2017A base 0,2 to 0,8 0,7 3,5 to 4,5 0,4 to 1,0 1,2 to 1,8 0,10 0,25 0,25 Structure: With structural hardening Particular characteristics: Recommendations for welding and filling with EN AW-2017A Process Thickness range in mm State befor

35、e welding PWHT Degree of weldabilityJoint coefficientComments and bibliographic references CDFW 10 T4 none 2 0,87 3 DW 10 T4 none 2 0,65 11 Diffusion temperature starting from 550 C prEN 4632-002:200711 7.5 Designation: EN 573-2 : EN AW-2024 Old designation : AU4 G1 EN 2032-1 : AL-P2024- ISO : Al Cu

36、 4 Mg 1 Other standards : Typical composition: See EN 573-3. Grade Al Si Fe Cu Mn Mg Cr Zn Ti 2017A base 0,50 0,50 3,8 to 4,9 0,30 to 0,9 1,2 to 1,8 0,10 0,25 0,15 Al Ti + Zr base 0,20 Only for extruded or forged products with agreement between supplier and customer Structure: With structural harden

37、ing Particular characteristics: prEN 4632-002:200712 Recommendations for welding and filling with EN AW-2024 Process Thickness range in mm State before welding PWHT Degree of weldabilityJoint coefficientComments and bibliographic references TIG T3 none 4 C.A 1,6 T3 none 2 0,78 Filler metal 2219 55 5

38、 30 T4 T4 none T4 0,65 to 0,8 EBW 100 T351 none 2 to 3 0,82 Micro-cracks (liquation cracking) along the grain boundaries in the heat affected zone metal 79 SLW continuous 3 2 T351 T4 none 2 0,72 0,53 Filler metal 5356 68 Filler metal 5356 14 SLW Pulsed frequency 100 Hz to 500 Hz 2 T4 none 2 0,8 Fill

39、er metal 4043 14 SLW pulsed frequency 60 C and exposed in a corrosive environment. b24 h desensitization treatment at 250 C if parts must be exposed to a corrosive environment and if welding conditions (very high energies) or forming conditions (hot) could have made them sensitive to corrosion. cEle

40、ctron beam welds are not sensitive to stress corrosion for magnesium contents of the order of 4,1 % Mg 76 prEN 4632-002:200718 7.9 Designation: EN 573-2 : EN AW-5754 Old designation : AG3M EN 2032-1 : AL-P5754- ISO : Al Mg 3 Other standards : Typical composition: See EN 573-3. Grade Al Si Fe Cu Mg M

41、n Cr Zn Ti Mn + Cr 5754 base 0,40 0,40 0,10 2,6 to 3,6 0,50 0,30 0,20 0,15 0,10 to 0,6Structure: Particular characteristics: Recommendations for welding and filling with EN AW-5754 Process Thickness range in mm State before welding PWHT Degree of weldabilityJoint coefficientComments and bibliographi

42、c references OA 1 TIG C.A Man. 6 O or H111 1 1 C.C Auto He 12 O or H111 2 1 Filler metal: 5154 or 5854 or 5183 or 5356 MIG 30 O or H111 2 PAW 2,5 O or H111 2 1 EBW 40 O or H111 2 1 RSEW, RSW O or H111 2 prEN 4632-002:200719 7.10 Designation: EN 485-1 : EN AW-6005A, EN AW-6013, EN AW-6016, EN AW-6056

43、, EN AW-6060, EN AW-6061, EN AW-6063, EN AW-6081, EN AW-6082, EN AW-6181 Old designation : AGS (6060); AGSU (6061); ASGM 0,9 (6081); ASGM 1 (6082) EN 2032-1 : AL-P6005A, AL-P6013-, AL-P6016-, AL-P6056-, AL-P6060-, AL-P6061-, AL-P6063-, AL-P6081-, AL-P6082-, AL-P6181-, AL-P6063 ISO : Al Si Mg; Al Mg

44、15.0,8 Cu Mn; ; Al Si Mg Cu Mn; Al Mg Si; Al Mg 1 Si Cu; Al Si 0,9 Mg Mn; Al Si 1 Mg Mn; Al Si 1 Mg 0,8; Al Mg 0,7 Si Other standards : Typical composition: See EN 573-3. Grade Al Si Fe Cu Mn Mg Cr Zn Ti Mn + Cr 6005A base 0,50 to 0,9 0,35 0,30 0,50 0,40 to 0,7 0,30 0,20 0,10 0,12 to 0,50 6013 base

45、0,6 to 1,0 0,50 0,6 to 1,1 0,2 to 0,8 0,8 to 1,2 0,10 0,25 0,10 6016 base 1,0 to 1,5 0,50 0,2 0,2 0,25 to 0,6 0,1 0,2 0,15 6056 base 0,7 to 1,3 0,50 0,5 to 1,1 0,4 to 1,0 0,6 to 1,2 0,25 0,1 to 1,7 0,2 6060 base 0,30 to 0,60,10 to 0,30 0,10 0,10 0,35 to 0,6 0,05 0,15 0,10 6061 base 0,40 to 0,8 0,7 0

46、,15 to 0,40 0,15 0,8 to 1,2 0,04 to 0,34 0,25 0,15 6063 base 0,2 to 0,6 0,35 0,1 0,1 0,45 to 0,9 0,1 0,1 0,1 6081 base 0,8 to 1,2 0,45 0,10 0,15 0,6 to 1,0 0,10 0,20 0,10 6082 base 0,7 to 1,3 0,50 0,10 0,40 to 1,0 0,6 to 1,2 0,25 0,20 0,10 6181 base 0,7 to 1,1 0,45 0,10 0,1 to 0,45 0,6 to 1,0 0,10 0

47、,20 0,10 Structure: With structural hardening Particular characteristics: Preferably to weld 6082, 6081, 6060, 6005, 6016 alloys rather than 6061 alloy prEN 4632-002:200720 Recommendations for welding and filling with EN AW-6005A Process Thickness range in mm State before welding PWHT Degree of weld

48、abilityJoint coefficientComments and bibliographic references TIG T4 1 C.A Man. 0,6 H111 or O C.C Auto He 12 T4 T6 T6 none 2 3 Ditto for the MIG process MIG 20 T6 2 to 3 0,45 to 0,5 depending on the filler metal grade (51) PAW 2,5 2 Filler metal for TIG and MIG: - 5183 and 5356 for high mechanical properties (better elongations with 5

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