ASD-STAN PREN 4632-004-2010 Welded and brazed assemblies for aerospace constructions Weldability and brazeability of materials Part 004 Homogeneous assemblies highly alloyed steels.pdf
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1、ASD STANDARD NORME ASD ASD NORM prEN 4632-004 Edition P 1 February 2010 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATIONAvenue de Tervuren, 270 - B-1150 Brussels - Tel. 32 2 775 8126 - Fax. 32 2 775 8131 - www.asd-stan.orgICS: 25.160.40; 49.025.20; 49.035 Des
2、criptors: ENGLISH VERSION Welded and brazed assemblies for aerospace constructions Weldability and brazeability of materials Part 004: Homogeneous assemblies highly alloyed steels Assemblages souds et brass pour constructions arospatiales Soudabilit et brasabilit des matriaux Partie 004 : Assemblage
3、s homognes daciers fortement allis Schwei- und Ltverbindungen fr die Luft- und Raumfahrt Schweibarkeitsgrad und Ltbarkeitsgrad von Werkstoffen Teil 004: Gleichartige Verbingungen This “Aerospace Series“ Prestandard has been drawn up under the responsibility of ASD-STAN (The AeroSpace and Defence Ind
4、ustries 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. Subsequent to the publication of this Prestandard, the technical content shall not be
5、 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 submitted as a draft European Standard (prEN) to CEN (European Committee for Standardiz
6、ation) 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 national standards conflicting with the EN. Edition approved for publication 28
7、 February 2010 Comments should be sent within six months after the date of publication to ASD-STAN Metallic Material Domain Copyright 2010 by ASD-STAN prEN 4632-004:2010 (E) 2 Contents Page Foreword2 1 Scope 3 2 Normative references 3 3 Terms and definitions .8 4 Use of this standard 8 5 Updating of
8、 this standard .8 6 Index of steel sheets .9 7 Material sheets 10 Bibliography. 34 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 Genera
9、l Process Manual, this standard has received approval for Publication. prEN 4632-004:2010 (E) 3 1 Scope This standard specifies the weldability and brazeability of materials or material families used in the aerospace industry. It comprises a series of sheets, by materials or material family, which:
10、indicate the main titles, the typical chemic al composition and the main characteristics, contain recommendations for welding and brazing, indicate a degree of weldability or brazeability for a given process under defined conditions. indicate a value for the welded joint mechanical resistance coeffi
11、cient for each welding process when extracted from relevant bibliographical references. Joint coefficient is the ratio of stress resistance transversally to welded joint over tensile strength of parent alloy. It recommends ISO/TR 17671-3 and EN 1011-3 recommendations for pre-heating conditions speci
12、ally for the welding of martensitic steels. These conditions depend on the line energy of welding, thickness, arc welding process and of hydrogen rate in filler metal. It applies unreservedly to the manufacturing of new parts or for repair. 2 Normative references The following referenced documents a
13、re indispensable for the application of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the reference document (including any amendments) applies. EN 1011-3, Welding Recommendations for welding of metallic materials Part 3: Arc weldi
14、ng of stainless steels EN 1045, Brazing Fluxes for brazing Classification and technical delivery conditions EN 2174, Aerospace series Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) Solution treated and precipitation treated - Forgings De 100 mm Rm 850 MPa 1)EN 2175, Aerospace series Heat resistin
15、g alloy FE-PA2602 (X4NiCrTiMoV26-15) Solution treated and precipitation treated Sheet, strip and plate a 10 mm Rm 850 MPa 1)EN 2177, Aerospace series Heat resisting alloy FE-PA2501 (X4NiCrMoTi43-13) Solution treated and precipitation treated Forgings De 100 mm 1)EN 2178, Aerospace series Heat resist
16、ing alloy FE-PA2501 (X4NiCrMoTi43-13) Solution treated and precipitation treated Bar and section De 200 mm 1)EN 2278, Steel FE-PM37 900 MPa Rm 1 100 MPa Bars De 150 mm Aerospace series 2)EN 2279, Steel FE-PM37 900 MPa Rm 1 100 MPa Forgings De 150 mm Aerospace series 2)1) Published as ASD-STAN Presta
17、ndard at the date of publication of this standard. 2) Published as ASD-STAN Standard at the date of publication of this standard. prEN 4632-004:2010 (E) 4 EN 2280, Steel FE-PM37 900 MPa Rm 1 100 MPa Sheets a 6 mm Aerospace series 2)EN 2465, Aerospace series Steel FE-PA3901 (X2CrNi18-9) Softened 450
18、MPa Rm 680 MPa Bar for machining 4 mm De 100 mm EN 2466, Aerospace series Steel FE-PA3901 (X2CrNi19-11) Softened Forgings De 100 mm EN 2467, Aerospace series Steel FE-PA3901 (X2CrNi18-9) Air melted Softened Plate, sheet and strip 0,4 mm a 20 mm 520 MPa Rm 670 MPa EN 2468, Steel FE-PA11 Softened Tube
19、s 0,5 mm a 5 mm Aerospace series 2)EN 2469, Aerospace series Steel FE-PA3901 (X1CrNi18-10) Air melted Softened Wires 0,4 mm D 12,5 mm 450 MPa Rm 650 MPa EN 2815, Aerospace series Steel FE-PM1802 (X5CrNiCu15-5) Consumable electrode remelted - Solution treated and precipitation treated - Bar for machi
20、ning a or D 200 mm Rm 965 MPa 1)EN 2816, Aerospace series Steel FE-PM1802 (X5CrNiCu15-5) Consumable electrode remelted Solution treated and precipitation treated Forgings a or D 200 mm Rm 965 MPa 1)EN 2817, Aerospace series Steel FE-PM1802 (X5CrNiCu15-5) Consumable electrode remelted Solution treate
21、d and precipitation treated Bar for machining a or D 200 mm Rm 1 070 MPa 1)EN 2818, Aerospace series Steel FE-PM1802 (X5CrNiCu15-5) Consumable electrode remelted Solution treated and precipitation treated Forgings a or D 200 mm Rm 1 070 MPa 1)EN 2821, Aerospace series Steel FE-PM1802 (X5CrNiCu15-5)
22、Consumable electrode remelted Solution treated and precipitation treated Bar for machining a or D 200 mm Rm 1 310 MPa EN 3160, Aerospace series Steel FE-PM3801 (X5CrNiCu17-4) Air melted Solution treated and precipitation treated Bar a or D 200 mm Rm 1 310 MPa EN 3161, Aerospace series Steel FE-PM380
23、1 (X5CrNiCu17-4) Air melted Solution treated and precipitation treated Bar - a or D 200 mm Rm 930 MPa EN 3162, Aerospace series Steel FE-PM3801 (X5CrNiCu17-4) Air melted Solution treated and precipitation treated Sheet and strip a 6 mm Rm 930 MPa EN 3357, Aerospace series Steel FE-PM1503 (X3CrNiMoAl
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