1、ASD STANDARD NORME ASD ASD NORM prEN 4683 Edition P1 December 2009 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: Descriptors: ENGLISH VERSION Aerospac
2、e series Steel FE-WM 3504 (X4CrNiMo16-5-1) Air melted Filler metal for welding Wire and rod Srie arospatiale Acier FE-WM 3504 X4CrNiMo16-5-1) labor lair Mtal dapport de soudage Fils et baguettes Luft- und Raumfahrt Stahl FE-WM 3504 (X4CrNiMo16-5-1) Lufterschmolzen Schweizuzatz This “Aerospace Series
3、“ Prestandard has been 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 mem
4、ber comments. Subsequent 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,
5、 it will be submitted 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
6、 by withdrawing any national standards conflicting with the EN. Edition approved for publication 15 December 2009 Comments should be sent within six months after the date of publication to ASD-STAN Metallic Material Domain Copyright 2009 by ASD-STAN prEN 4683:2009 (E) 2 Foreword This standard was re
7、viewed 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 Process Manual, this standard has received approval for Publication. prEN 4683:2009 (E) 3 Introduction This st
8、andard is part of the series of EN metallic material standards for aerospace applications. The general organization of this series is described in EN 4258. This standard has been prepared in accordance with EN 4500-5. 1 Scope This standard specifies the requirements relating to: Steel FE-WM 3504 (X4
9、CrNiMo16-5-1) Air melted Filler metal for welding Wire and rod for aerospace applications. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the edition cited applies. For undated references, the latest editio
10、n of the referenced document (including any amendments) applies. EN 3879, Aerospace series Metallic materials Filler Metal for welding technical specification EN 4258, Aerospace series Metallic materials General organization of standardization Links between types of EN standards and their use EN 450
11、0-5, Aerospace series Metallic materials Rules for drafting and presentation of material standards Part 5: Specific rules for steel 1) 1) Published as ASD-STAN Prestandard at the date of publication of this standard. prEN 4683:2009 (E) 4 1 Material designation Steel FE-WM 3504 (X4CrNiMo16-5-1) Eleme
12、nt C Si Mn P S Cr Mo Ni N2Fe 2 min. 15,00 0,80 4,00 0,02 Chemical composition % max. 0,06 0,70 1,50 0,025 0,005 17,00 1,50 6,00 0,08 Base3 Method of melting Air melted + AOD aor + VOD bor equivalent process 4.1 Form Filler wire or filler rods 4.2 Method of production Cold drawn 4.3 Limit dimension(s
13、) mm 5 Technical specification EN 3879 Delivery condition Cold drawn and annealed 6.1 Heat treatment 6.2 Delivery condition code U Use condition Delivery condition 7 Heat treatment Characteristics 8.1 Test sample(s) 8.2 Test piece(s) 8.3 Heat treatment 9 Dimensions concerned mm 10 Thickness of cladd
14、ing on each face % 11 Direction of test piece 12 Temperature C 13 Proof stress Rp0,2 MPa 14 Strength Rm MPa 15 Elongation A % 16 T Reduction of area Z % 17 Hardness 18 Shear strength Rc MPa 19 Bending k 20 Impact strength 21 Temperature C 22 Time h 23 Stress a MPa 24 Elongation a % 25 Rupture stress
15、 R MPa 26 C Elongation at rupture A % 27 Notes (see line 98) a, bprEN 4683:2009 (E) 5 44 External defects See EN 3879. 57 Residual stress See EN 3879. 61 Internal defects See EN 3879. 82 Batch uniformity (Material verification) See EN 3879. 95 Marking inspection See EN 3879. 96 Dimensional inspection See EN 3879. 98 Notes aAOD “Argon Oxygen Decarbonization”. bVOD “Vacuum Oxygen Decarbonization”. 99 Typical use prEN 4683:2009 (E) 6 100 Product qualification See EN 3879. Qualification programme to be agreed between manufacturer and purchaser.
