1、BRITISH STANDARD AEROSPACE SERIES Steel FE-WM1502 (X1 lCrNiMoVN12-3) Filler metal for welding The European Standard EN 3890:2001 has the status of a British Standard ICs 49.025.10; 25.160.20 BS EN 3890:2002 Wk present to the responsible European committee any enquiries on the interpretation, or prop
2、osals for change, and keep the UK interests informed; monitor related international and European developments and promulgate them in the UK. - A list of organizations represented on this committee can be obtained on request to its secretary. Cr oss-r e fer enc e s The British Standards which impleme
3、nt international or European publications referred to in this document may be found in the BSI Standards Catalogue under the section entitled “International Standards Correspondence Index”, or by using the “Find” facility of the BSI Standards Electronic Catalogue. A British Standard does not purport
4、 to include all the necessary provisions of a contract. Users of British Standards are responsible for their correct application. Compliance with a British Standard does not of itself confer immunity from legal obligations. Summary of pages This document comprises a front cover, an inside front cove
5、r, the EN title page, pages 2 to 6, an inside back cover and a back cover. The BSI copyright date displayed in this document indicates when the document was last issued. O BSI 11 January 2002 ISBN0 580 38193 5 EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 3890 December 2001 ICs 49.025.1 O Eng
6、lish version Aerospace series - Steel FE-WM1502 (XI ICrNiMoVN12-3) - Filler metal for welding Seri arospatiale - Acier FE-WM1502 (XI 1CrNiMoVN12- 3) - Mtal dapport de soudage Luft- und Raumfahrt - Stahl FE-WM1502 (XI 1 CrNiMoVN12-3) - Schweizusatz This European Standard was approved by CEN on 2 May
7、2001 CEN members are bound to comply with the CENKENELEC Internal Regulations which stipulate the conditions for giving this European Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained
8、on application to the Management Centre or to any CEN member. This European Standard exists in three official versions (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 Management Centre h
9、as the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and United Kingdom. EUROPEAN COMMI
10、TTEE FOR STANDARDIZATION EUROPISCHES KOMITEE FR NORMUNG COMIT EUROPEN DE NORMALISATION Management Centre: rue de Stassart, 36 B-1050 Brussels O 2001 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 3890:2001 E EN 3890:2001 (E) Forew
11、ord This European Standard has been prepared by the European Association of Aerospace Manufacturers (AECMA) . After inquiries and votes carried 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
12、member countries of AECMA, prior to its presentation to CEN. This European Standard shall be given the status of a national standard, either by publication of an identical text or by endorsement, at the latest by June 2002, and conflicting national standards shall be withdrawn at the latest by June
13、2002. According to the CENKENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway
14、, Portugal, Spain, Sweden, Switzerland and the United Kingdom. 2 EN 3890:2001 (E) O Introduction This standard is part of the series of EN metallic material standards for aerospace applications. The general organisation of this series is described in EN 4258. This standard has been prepared in accor
15、dance with EN 4500-5. 1 Scope This standard specifies the requirements relating to: Steel FE-WM1502 (XI 1CrNiMoVN12-3) Filler metal for welding for aerospace applications. 2 Normative references This European Standard incorporates by dated or undated reference provisions from other publications. The
16、se normative references are cited at the appropriate places in the text and the publications are listed hereafter. For dated references, subsequent amendments to or revisions of any of these publications apply to this European Standard only when incorporated in it by amendment or revision. For undat
17、ed references the latest edition of the publication referred to applies. EN 2043 Aerospace series - Metallic materials - General requirements for semi-finished product qualification (excluding forgings and castings) 1) EN 3879 Aerospace series - Metallic materials - Filler metals for welding - Techn
18、ical specification 1) EN 4258 Aerospace series - Metallic materials - General organization of standardization - Links between types of EN standards and their use EN 4500-5 Aerospace series - Metallic materials - Rules for drafting and presentation of material standards - Part 5: Specific rules for s
19、teels 1) 1) Published as AECMA Prestandard at the date of publication of this standard 3 EN 3890:2001 (E) Limit dimension(s) mm Technical specification Material designation I Steel FE-WM1502 (XIlCrNiMoVN12-3) - EN 3879 I Element Chemical 6.2 7 % Heat treatment - Delivery condition code U Use conditi
20、on Delivery condition Heat treatment - 0,08 - 0,50 - 11,O 1,50 2,OO - 0,020 0,25 0,13 0,35 0,90 0,030 0,025 12,5 2,OO 3,OO 0,50 0,040 0,40 - Base 3.1 3.2 3.3 9 Method of melting I Air melted Test sample(s) - Test piece(s) - Heat treatment - Dimensions concerned mm - each face Thickness of cladding o
21、n % - Form I Filler wire and filler rods Strength Elongation Reduction ofarea Method of production R, MPa - A% - Z % - Cold drawn Time Stress O= Elongation Rupture stress OR - h MPa - a% - MPa - 6.1 I Delivery condition I Cold drawn and annealed I Elongation at rurAure A % - Characteristics - I 11 I
22、 Direction of test piece 12 I ITemperature I ,9 I “C I - 13 I I Proof stress I Rp0,2 I MPa I - I I I - I 17 I Hardness 18 I Shear strength I R, I MPa I - 19 I Bending 1kl-l - - 20 I Impact strength I Temperature I ,9 I “C I - - I 27 I Notes (see line 98) 4 ixternal defects - - iesidual stress See EN
23、 3879 - nternal defects 3atch uniformity :Material verification) Marking inspection 3imensional inspection Votes rypical use EN 3890:2001 (E) See EN 3879 See EN 3879 See EN 3879 See EN 3879 -I See EN 3879 -I - 5 100 6 EN 3890:2001 (E) - Product qualification BS EN 3890:2002 BSI 389 Chiswick High Roa
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