AECMA PREN 4632-003-2008 Aerospace series Weldability and brazeability of materials in aerospace constructions Part 003 Homogeneous assemblies of unalloyed and low alloy steels Edi.pdf
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1、ASD STANDARD NORME ASD ASD NORM prEN 4632-003 Edition P 1 December 2008 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATIONAvenue de Tervuren, 270 - B-1150 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 763 3565 - www.asd-stan.orgICS: Descriptors: ENGLISH VERSION
2、 Aerospace series Weldability and brazeability of materials in aerospace constructions Part 003: Homogeneous assemblies of unalloyed and low alloy steels Srie arospatiale Soudabilit et brasabilit des matriaux pour constructions arospatiales Partie 003 : Assemblages homognes des aciers non allis et f
3、aiblement allis Luft- und Raumfahrt Schweibarkeit und Ltbarkeit von Werkstoffen im Luft und Raumfahrzeugbau Teil 003: GleicharGTAW e Verbindungen unlegierten und niedriglegierten Stlhen This “Aerospace Series“ Prestandard has been drawn up under the responsibility of ASD-STAN (The AeroSpace and Defe
4、nce 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. Subsequent to the publication of this Prestandard, the technical content shall
5、 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 submitted as a draft European Standard (prEN) to CEN (European Committee for Sta
6、ndardization) 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 publica
7、tion 31 December 2008 Comments should be sent within six months after the date of publication to ASD-STAN Metallic Material Domain Copyright 2008 by ASD-STAN Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,
8、-prEN 4632-003:20082 Contents Page Foreword2 1 Scope 3 2 Normative references3 3 Terms and definitions .6 4 Use of this standard 6 5 Updating this standard7 6 Index of steel sheets .7 7 Material sheets.8 Bibliography30 Foreword This standard was reviewed by the Domain Technical Coordinator of ASD-ST
9、ANs Metallic Material Domain. 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. Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or
10、networking permitted without license from IHS-,-,-prEN 4632-003:2008 3 1 Scope This standard defines degrees 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 families, which: indicate t
11、he 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 conditions, indicate a value of the mechanical strength coefficient of the welded joint f
12、or 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 base alloy. To define preheating conditions, it recommends ISO TR 17671-2 recomm
13、endations. These conditions depend on the calculation of carbon equivalent, welding energy per unit length, thickness, arc welding process and hydrogen rate in filler metal. It is applicable without restriction for the manufacturing of new parts or for repair. 2 Normative references The following re
14、ferenced documents are indispensable for the application 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. ISO 636, Welding consumables Rods, wires and deposits for tungste
15、n inert gas welding of non-alloy and unalloyed and low alloy steels Classification. EN ISO 4063, Welding and allied processes Nomenclature of processes and reference numbers. ISO/TR 17671-2, Welding Recommendations for welding of metallic materials Part 2: Arc welding of ferritic steels. EN 439, Wel
16、ding consumables Shielding gases for arc welding and cutting. EN 440, Welding consumables Wire electrodes and deposits for gas shielded metal arc welding of non alloy and fine grain steels Classification. EN 499, Welding consumables Covered electrodes for manual metal arc welding of non alloy and fi
17、ne grain steels Classification. EN 758, Welding consumables Tubular cored electrodes for metal arc welding with and without a gas shield of non alloy and fine grain steels Classification. EN 1045, Brazing Fluxes for brazing Classification and technical delivery conditions. EN 1599, Welding consumabl
18、es Covered electrodes for manual metal arc welding of creep-resisting steels Classification. Copyright ASD-STAN Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 4632-003:20084 EN 2135, Aerospace series Steel FE-PL61 Carb
19、urized, hardened and tempered Bar De 40 mm. 1)EN 2213, Steel FE-PL52 S 980 MPa Rm 1 180 MPa Bars De 16 mm Aerospace series. 1) EN 2218, Steel FE-PL52 S 980 MPa Rm 1 180 MPa Tubes for structures a 4 mm d 5 a Aerospace series. 1)EN 2220, Steel FE-PL52 S 1 080 MPa Rm 1 250 MPa Tubes for structures 2 mm
20、 a 20 mm d 5 a Aerospace series. 1)EN 2767, Aerospace series Steel FE-PL79 Carburized, hardened and tempered 1180 Rm 1550 MPa Bar for machining De 150 mm. 1)EN 2768, Aerospace series Steel FE-PL79 Carburized, hardened and tempered 1180 Rm 1550 MPa Forgings De 150 mm. EN 2779, Aerospace series Steel
21、FE-PL56 Hardened and tempered 1250 Rm 1400 MPa Bars De 70 mm. EN 2780, Aerospace series Steel FE-PL56 Hardened and tempered 1250 Rm 1400 MPa Forgings De 70 mm. EN 3522, Aerospace series Steel FE-PL79 Softened Reference heat treatment: carburized, hardened and tempered Forging stock De 200 mm. EN 352
22、3, Aerospace series Steel FE-PL1505 (15CrMoV6) Air melted Hardened and tempered Bar for machining De 100 mm 1 080 MPa Rm 1 280 MPa. 1)EN 3524, Aerospace series Steel FE-PL1505 (15CrMoV6) Air melted Hardened and tempered Bar for machining 2 mm a 6 mm 1 080 MPa Rm 1 280 MPa. EN 3525, Aerospace series
23、Steel FE-PL1505 (15CrMoV6) Air melted Hardened and tempered Plate 6 mm 12 Normalized Stress relieving if necessary 1 Basic covered electrodes E 42B according to EN 499 4 Normalized 1 1 Filler metal: Steel for GTAW with Si + Mn(type G3Si1 according to EN 440) GTAW 141 4 (1strun) Normalized none 1 Dit
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