1、BRITISH STANDARDBS EN 3162:2007Aerospace series Steel FE-PM3801 (X5CrNiCu17-4) Air melted, solution treated and precipitation treated, sheet and strip a 6 k mm, Rm U 930 MPaICS 49.025.10g49g50g3g38g50g51g60g44g49g42g3g58g44g55g43g50g56g55g3g37g54g44g3g51g40g53g48g44g54g54g44g50g49g3g40g59g38g40g51g5
2、5g3g36g54g3g51g40g53g48g44g55g55g40g39g3g37g60g3g38g50g51g60g53g44g42g43g55g3g47g36g58BS EN 3162:2007This British Standard was published under the authority of the Standards Policy and Strategy Committee on 29 August 2008 BSI 2008ISBN 978 0 580 58057 4National forewordThis British Standard is the UK
3、 implementation of EN 3162:2007. The UK participation in its preparation was entrusted by Technical Committee ACE/61, Metallic materials for aerospace purposes, to Panel ACE/61/-/15, Steels.A list of organizations represented on this committee can be obtained on request to its secretary.This publica
4、tion does not purport to include all the necessary provisions of a contract. Users are responsible for its correct application.Compliance with a British Standard cannot confer immunity from legal obligations.Amendments/corrigenda issued since publicationDate CommentsEUROPEAN STANDARD NORME EUROPENNE
5、 EUROPISCHE NORM EN 3162 August 2007 ICS 49.025.10 English Version Aerospace series - Steel FE-PM3801 (X5CrNiCu17-4) - Air melted, solution treated and precipitation treated, sheet and strip a 6 mm, Rm 930 MPa Srie arospatiale - Acier FE-PM3801 (X5CrNiCu17-4) - labor lair, mis en solution et vieilli
6、, tles et bandes a 6 mm, Rm 930 MPa Luft- und Raumfahrt - Stahl FE-PM3801 (X5CrNiCu17-4) - Lufterschmolzen, lsungsgeglht und ausgelagert, Bleche und Bnder a 6 mm, Rm 930 MPa This European Standard was approved by CEN on 24 February 2007. CEN members are bound to comply with the CEN/CENELEC Internal
7、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 on application to the CEN Management Centre or to any CEN member.
8、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 CEN Management Centre has the same status as the official versions. CEN members a
9、re the national standards bodies of Austria, Belgium, Bulgaria, 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, Switz
10、erland and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG Management Centre: rue de Stassart, 36 B-1050 Brussels 2007 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No
11、. EN 3162:2007: E2 Contents Page Foreword3 Introduction .4 1 Scope 4 2 Normative references 4 BS EN 3162:20073 Foreword This document (EN 3162:2007) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). After enquiries and votes carried out in
12、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 by publicati
13、on of an identical text or by endorsement, at the latest by February 2008, and conflicting national standards shall be withdrawn at the latest by February 2008. Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. CEN and/or CENELEC sh
14、all 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, Cyprus, Czech Republic, Denmark, Es
15、tonia, 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 3162:20074 Introduction This standard is part of the series of
16、 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-PM3801 (X5CrNiCu17-4) Air melted, solution
17、 treated and precipitation treated, sheet and strip a 6 mm, Rm 930 MPa 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 lates
18、t edition of the referenced document (including any amendments) applies. EN 2043, Aerospace series Metallic materials General requirements for semi-finished product qualification (excluding forgings and castings)1)EN 4258, Aerospace series Metallic materials General organization of standardization L
19、inks between types of EN standards and their use EN 4436, Aerospace series Steel Test methods Determination of ferrite content1)EN 4500-5, Aerospace series Metallic materials Rules for drafting and presentation of material standards Part 5: Specific rules for steels1)EN 4700-1, Aerospace series Stee
20、l and heat resisting alloy Wrought products Technical specification Part 1: Plate, sheet and strip1)1) Published as ASD Prestandard at the date of publication of this standard. BS EN 3162:20075 1 Material designation Steel FE-PM3801 (X5CrNiCu17-4) Element C Si Mn P S Cr Mo Ni Cu Nb+Ta Fe min. 15,0 3
21、,0 3,0 5 x C 2 Chemical composition % max. 0,07 1,00 1,00 0,040 0,030 17,5 0,50 5,0 5,0 0,45 Base 3 Method of melting Air melted 4.1 Form Sheet and strip 4.2 Method of production 4.3 Limit dimension(s) mm a 6 5 Technical specification EN 4700-1 Delivery condition Solution treated Solution treated an
22、d precipitation treated 6.1 Heat treatment 1 025 C 1 055 C / t 1h / AC or OQ + cool to 30 C 1 025 C 1 055 C / t 1h / AC or OQ + cool to 30 C + 600 C 630 C / t 4 h / AC 6.2 Delivery condition code W U Use condition Solution treated and precipitation treated Delivery condition 7 Heat treatment Deliver
23、y condition + 600 C 630 C / t 4 h / AC Characteristics 8.1 Test sample(s) See EN 4700-1. 8.2 Test piece(s) See EN 4700-1. 8.3 Heat treatment Solution treated Use condition 9 Dimensions concerned mm a 6 a 6 10 Thickness of cladding on each face % 11 Direction of test piece L 12 Temperature C Ambient1
24、3 Proof stress Rp0,2 MPa 725 14 T Strength RmMPa Rm 930 15 Elongation A % A50 mm 8 16 Reduction of area Z % 17 Hardness 370 HV 29 HRC 35 280 HV 383 18 Shear strength RcMPa 19 Bending k 2; = 105 20 Impact strength 21 Temperature C 22 Time h 23 Stress aMPa 24 C Elongation a % 25 Rupture stress RMPa 26
25、 Elongation at rupture A % 27 Notes (see line 98) BS EN 3162:20076 See EN 4700-1. 1 EN 4436 30 Microstructure 7 The -ferrite content shall not exceed 5 % See EN 4700-1. 34 Grain size 7 G 4 44 External defects See EN 4700-1. See EN 4700-1. 50 Cleanliness/inclusion content (micro-cleanness) 7 Category
26、 2 95 Marking inspection See EN 4700-1. 96 Dimensional inspection See EN 4700-1. 98 Notes 99 Typical use BS EN 3162:20077 See EN 2043. 100 Product qualification Qualification programme to be agreed between manufacturer and purchaser. BS EN 3162:2007BS EN 3162:2007BSI Group Headquarters389 Chiswick H
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