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

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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 Copyright European Association of Aerospace Industries Provided by IHS

8、under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4632-002:20072 Contents Page Foreword2 1 Scope 3 2 Normative references 3 3 Terms, definitions, symbols and abbreviations .4 4 Use of this standard 4 5 Updating this standard4 6 Index of

9、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 Domain. After inquiries and votes carried out in accordance with the rules of ASD-STAN defined in ASD-STANs General Proces

10、s Manual, this standard has received approval for Publication. Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4632-002:20073 1 Scope This standard defines degrees

11、of weldability and brazeability for materials or families 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 weldi

12、ng and brazing, indicate a degree of weldability or brazeability 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 coe

13、fficient is expressed as a ratio of the tensile strength of 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 applicati

14、on of this document. For dated references, only the edition 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 deliver

15、y. EN 485-2, Aluminium and aluminium alloys Sheet, strip and 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 desi

16、gnation system. EN 573-3, Aluminium and aluminium alloys Chemical 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

17、 Casting Chemical composition and mechanical properties. EN 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 4

18、632-001, Welded and brazed assemblies for aerospace constructions 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 Prestandar

19、d at the date of publication of this standard. Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4632-002:20074 ANSI/AWS A5.10, Specification for Bare Aluminum and Al

20、uminum-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. 3)SAE-AMS 4191, Aluminum Alloy, Welding Wire 6.3Cu - 0.30Mn -

21、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, the terms and definitions given in EN 4632-001 apply. PWHT: Po

22、st-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 main element used in the chemical composition and on the alloy

23、 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 give the lowest degree in preference. If two degrees are indicate

24、d, 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: Society of Automotive Engineers, Inc. (SAE), 400 Commonwealth Dr

25、ive, Warrendale, PA 15096-0001, USA. Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4632-002:20075 6 Index of aluminium and aluminium alloy sheets 6.1 Index by mat

26、erial family family 1000: sheet 7.1 family 2000: sheets 7.2 to 7.7 family 5000: sheets 7.8 and 7.9 family 6000: sheet 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

27、 7.9 5056A, 5083, 5086, 5182, 5456 5754 7.10 6005A, 6013, 6016, 6056, 6060, 6061, 6063, 6081, 6082, 6181 7.11 7.12 7020, 7051 7050, 7075, 7175, 7475 7.13 Al Si 7 Mg 0,3 and Al Si 7 Mg 0,6 Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo

28、 reproduction or networking permitted without license from IHS-,-,-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 Al S

29、i 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 weldin

30、g 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 Copyright European Association of Aerospace Industries Provided by IHS unde

31、r license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4632-002:20077 7.2 Designation: EN 573-2 : EN AW-2001 Old designation : 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

32、 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: Recommendations for welding and filling with EN AW-2001 Process Thickness range in mm State before welding PWHT Degree of weldab

33、ilityJoint 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 Micro-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 Copyright European Ass

34、ociation of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-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:

35、Typical composition: See EN 573-3. Grade Al Si Fe Cu 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 Particu

36、lar characteristics: Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4632-002:20079 Recommendations for welding and filling with EN AW-2014 Process Thickness range

37、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-porosity 8 T6 none 2 No porosity 50 EBW 30 T4 T6 T6 none 2 to 3 2 t

38、o 3 No porosity 50 RSEW, RSW T6 2 FSW 22 6,35 T6 T651 none none 2 2 0,68 43 44 Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4632-002:200710 7.4 Designation: EN 5

39、73-2 : EN AW-2017A Old designation : AU4G EN 2032-1 : AL-P2017A ISO : Al Cu 4 Mg 1 Other standards : Typical composition: 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 char

40、acteristics: Recommendations for welding and filling with EN AW-2017A Process Thickness range in mm State before 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 Copyrig

41、ht European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-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 4 Mg 1 Ot

42、her 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 hardening Partic

43、ular characteristics: Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4632-002:200712 Recommendations for welding and filling with EN AW-2024 Process Thickness rang

44、e 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 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 hea

45、t 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 Filler metal 4043 14 SLW pulsed frequency 60 C and exposed in a corrosive environment. b24 h desensitization treatment at 250 C if part

46、s 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. cElectron beam welds are not sensitive to stress corrosion for magnesium contents of the order of 4,1 % Mg 76 Copyright European Associ

47、ation of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-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 Mn 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