1、BS EN 4683:2011Aerospace series Steel FE-WM 3504 (X4CrNiMo16-5-1) Air melted Filler metal forwelding Wire and rodBS EN 4683:2011 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of EN 4683:2011.The UK participation in its preparation was entrusted to TechnicalCommittee
2、 ACE/61/-/15, Steels for Aerospace Purposes.A list of organizations represented on this committee can beobtained on request to its secretary.This publication does not purport to include all the necessaryprovisions of a contract. Users are responsible for its correctapplication. BSI 2011ISBN 978 0 58
3、0 66259 1ICS 49.025.10Compliance with a British Standard cannot confer immunity fromlegal obligations.This British Standard was published under the authority of theStandards Policy and Strategy Committee on 31 July 2011.Amendments issued since publicationDate Text affectedBS EN 4683:2011EUROPEAN STA
4、NDARD NORME EUROPENNE EUROPISCHE NORM EN 4683 June 2011 ICS 49.025.10 English Version Aerospace 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 bague
5、ttes Luft- und Raumfahrt - Stahl FE-WM 3504 (X4CrNiMo16-5-1) - Lufterschmolzene - Schweizusatz - Draht und StangeThis European Standard was approved by CEN on 27 November 2010. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this Eu
6、ropean Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the CEN-CENELEC Management Centre or to any CEN member. This European Standard exists in three official versi
7、ons (English, French, German). A version in any other language made by translation under the responsibility of a CEN member into its own language and notified to the CEN-CENELEC Management Centre has the same status as the official versions. CEN members are the national standards bodies of Austria,
8、Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom. EUROPEAN
9、COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG Management Centre: Avenue Marnix 17, B-1000 Brussels 2011 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4683:2011: EBS EN 4683:2011EN 468
10、3:2011 (E) 2 Contents Page Foreword 3 Introduction . 4 1 Scope 4 2 Normative references 4 BS EN 4683:2011EN 4683:2011 (E) 3 Foreword This document (EN 4683:2011) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). After enquiries and votes ca
11、rried out in accordance with the rules of this Association, this Standard has received the approval of the National Associations and the Official Services of the member countries of ASD, prior to its presentation to CEN. This European Standard shall be given the status of a national standard, either
12、 by publication of an identical text or by endorsement, at the latest by December 2011, and conflicting national standards shall be withdrawn at the latest by December 2011. Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. CEN and/
13、or CENELEC shall not be held responsible for identifying any or all such patent rights. According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech
14、 Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. BS EN 4683:2011EN 4683:2011 (E) 4 Introduction
15、 This European Standard 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 European Standard specifies the requirements relatin
16、g to: Steel FE-WM 3504 (X4CrNiMo16-5-1) 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 ref
17、erences, the latest edition of the referenced document (including any amendments) applies. EN 3879, Aerospace series Metallic materials Filler Metal for welding technical specification1)EN 4258, Aerospace series Metallic materials General organization of standardization Links between types of EN sta
18、ndards and their use EN 4500-5, 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. BS EN 4683:2011EN 4683:2011 (E) 5 1 Material designation
19、Steel FE-WM 3504 (X4CrNiMo16-5-1) 2 Chemical composition % Element C Si Mn P S Cr Mo Ni N2Fe min. 15,00 0,80 4,00 0,02 Basemax. 0,06 0,70 1,50 0,025 0,005 17,00 1,50 6,00 0,08 3 Method of melting Air melted + AOD aor + VOD bor equivalent process 4.1 Form Filler wire or filler rods 4.2 Method of prod
20、uction Cold drawn 4.3 Limit dimension(s) mm 5 Technical specification EN 3879 6.1 Delivery condition Cold drawn and annealed Heat treatment 6.2 Delivery condition code U 7 Use condition Delivery condition Heat treatment Characteristics 8.1 Test sample(s) 8.2 Test piece(s) 8.3 Heat treatment 9 Dimens
21、ions concerned mm 10 Thickness of cladding on each face % 11 Direction of test piece 12 T Temperature C 13 Proof stress Rp0,2 MPa 14 Strength Rm MPa 15 Elongation A % 16 Reduction of area Z % 17 Hardness 18 Shear strength Rc MPa 19 Bending k 20 Impact strength 21 C Temperature C 22 Time h 23 Stress
22、a MPa 24 Elongation a % 25 Rupture stress R MPa 26 Elongation at rupture A % 27 Notes (see line 98) a, bBS EN 4683:2011EN 4683:2011 (E) 6 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 Mark
23、ing inspection See EN 3879. 96 Dimensional inspection See EN 3879. 98 Notes aAOD = “Argon Oxygen Decarbonization”. bVOD = “Vacuum Oxygen Decarbonization”. 99 Typical use BS EN 4683:2011EN 4683:2011 (E) 7 100 Product qualification See EN 3879. Qualification programme to be agreed between manufacturer and purchaser. This page deliberately left blank
