BS EN 2482-2010 Aerospace series Steel nFE-PL2108 (36NiCrMo16) n1 100 MPa ≤ Rm ≤ 1 300 MPa n Bars De ≤ 100 mm《航空航天系列 FE-PL2108 (35NiCrMo16)型钢 1100 MPa小于或等于Rm小于或等于1300 MPa 钢筋 De小于或.pdf

《BS EN 2482-2010 Aerospace series Steel nFE-PL2108 (36NiCrMo16) n1 100 MPa ≤ Rm ≤ 1 300 MPa n Bars De ≤ 100 mm《航空航天系列 FE-PL2108 (35NiCrMo16)型钢 1100 MPa小于或等于Rm小于或等于1300 MPa 钢筋 De小于或.pdf》由会员分享，可在线阅读，更多相关《BS EN 2482-2010 Aerospace series Steel nFE-PL2108 (36NiCrMo16) n1 100 MPa ≤ Rm ≤ 1 300 MPa n Bars De ≤ 100 mm《航空航天系列 FE-PL2108 (35NiCrMo16)型钢 1100 MPa小于或等于Rm小于或等于1300 MPa 钢筋 De小于或.pdf（12页珍藏版）》请在麦多课文档分享上搜索。

1、raising standards worldwideNO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBSI Standards PublicationBS EN 2482:2010Aerospace series Steel FE-PL2108 (36NiCrMo16) 1 100 MPa null Rm null 1 300 MPa Bars De null 100 mmIncorporating corrigendum June 2011Licensed Copy: Wang Bin, ISO/E

2、XCHANGE CHINA STANDARDS, 09/10/2011 03:39, Uncontrolled Copy, (c) BSIBS EN 2482:2010 BRITISH STANDARDNational forewordThis British Standard is the UK implementation of EN 2482:2010,The UK participation in its preparation was entrusted to TechnicalCommittee ACE/61/-/15, Steels for Aerospace Purposes.

3、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 0 580 75050 2ICS 49.025.10Compliance with a Brit

4、ish Standard cannot confer immunity fromlegal obligations.This British Standard was published under the authority of theStandards Policy and Strategy Committee on 31 January 2011.Amendments/corrigenda issued since publicationDate Text affectedincorporating corrigendum December 2010.30 June 2011 Impl

5、ementation of CEN corrected text to change the title of the standardLicensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 09/10/2011 03:39, Uncontrolled Copy, (c) BSIEUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 2482 December 2010 ICS 49.025.10 English Version Aerospace series - Steel FE-PL2

6、108 (36NiCrMo16) - 1 100 MPa Rm 1 300 MPa - Bars - De 100 mm Srie arospatiale - Acier FE-PL2108 (36NiCrMo16) - 1 100MPa Rm 1 300 MPa - Barres - De 100 mm Luft- und Raumfahrt - Stahl FE-PL2108 (36NiCrMo16) - 1 100 MPa Rm 1 300 MPa - Stangen - De 100 mm This European Standard was approved by CEN on 2

7、July 2010. CEN members are bound to comply with the CEN/CENELEC 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 ob

8、tained on application to the CEN-CENELEC 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

9、CEN-CENELEC Management Centre has the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembour

10、g, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG Management Centre: Avenue Marnix 17, B-1000 Brussels 2010 CEN All rights o

11、f exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 2482:2010: ELicensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 09/10/2011 03:39, Uncontrolled Copy, (c) BSIBS EN 2482:2010EN 2482:2010 (E) 2 Contents Foreword 3Introduction .41 Scope 52 Normative

12、 references 5Licensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 09/10/2011 03:39, Uncontrolled Copy, (c) BSIBS EN 2482:2010EN 2482:2010 (E) 3 Foreword This document (EN 2482:2010) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). After

13、enquiries 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 member countries of ASD, prior to its presentation to CEN. This European Standard shall be given the status of a nat

14、ional standard, either by publication of an identical text or by endorsement, at the latest by June 2011, and conflicting national standards shall be withdrawn at the latest by June 2011. Attention is drawn to the possibility that some of the elements of this document may be the subject of patent ri

15、ghts. CEN and/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,

16、 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 the United Kingdom. Licensed Copy: Wang Bin, ISO/EXC

17、HANGE CHINA STANDARDS, 09/10/2011 03:39, Uncontrolled Copy, (c) BSIBS EN 2482:2010EN 2482:2010 (E) 4 Introduction This 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

18、prepared in accordance with EN 4500-5. Licensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 09/10/2011 03:39, Uncontrolled Copy, (c) BSIBS EN 2482:2010EN 2482:2010 (E) 5 1 Scope This standard specifies the requirements relating to: Steel FE-PL2108 (36NiCrMo16) 1 100 MPa Rm 1 300 MPa Bars De 100 mm

19、 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 edition of the referenced document (including any amendments) applie

20、s. EN 2951, Aerospace series Metallic materials Test method Micrographic determination of content of non-metallic inclusions 1)EN 4050-4, Aerospace series Test method for metallic materials Ultrasonic inspection of bars, plates, forging stock and forgings Part 4: Acceptance criteria 1)EN 4258, Aeros

21、pace 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 steels 1)EN 4700-002, Aerospace series Steel an

22、d heat resisting alloys Wrought products Technical specification Part 002: Bar and section 1) Published as ASD-STAN Prestandard at the date of publication of this standard by Aerospace and Defence Industries Association of Europe-Standardization (ASD-STAN) (www.asd-stan.org). Licensed Copy: Wang Bin

23、, ISO/EXCHANGE CHINA STANDARDS, 09/10/2011 03:39, Uncontrolled Copy, (c) BSIBS EN 2482:2010 EN 2482:2010 (E) 6 1 Material designation Steel FE-PL2108 (36NiCrMo16) 2 Chemical composition % Element C Si Mn P S Cr Mo Ni Fe min. 0,30 0,15 0,30 1,60 0,25 3,50 Base max. 0,40 0,40 0,60 0,025 0,020 2,00 0,6

24、0 4,20 3 Method of melting Air melted 4.1 Form Bars 4.2 Method of production 4.3 Limit dimension(s) mm De 100 5 Technical specification EN 4700-002 6.1 Delivery condition Annealed Hardened and tempered Heat treatment 860 C 890 C / AQ + 560 C 6.2 Delivery condition code A U 7 Use condition Hardened a

25、nd tempered Delivery condition Heat treatment Delivery condition + 860 C 890 C / AQ + 560 C Characteristics 8.1 Test sample(s) See EN 4700-002. 8.2 Test piece(s) See EN 4700-002. 8.3 Heat treatment Annealed Hardened and tempered 9 Dimensions concerned mm De 100 10 Thickness of cladding on each face

26、% 11 Direction of test piece 12 T Temperature C Ambient 13 Proof stress Rp0,2MPa 900 14 Strength RmMPa 1 100 Rm 1 300 15 Elongation A % 10 16 Reduction of area Z % 40 17 Hardness HB 293 HV 309 a331 HB 388 350 HV 410 a18 Shear strength RcMPa 19 Bending k 20 Impact strength KV J 25 21 C Temperature C

27、22 Time h 23 Stress aMPa 24 Elongation a % 25 Rupture stress RMPa 26 Elongation at rupture A % 27 Notes (see line 98) aLicensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 09/10/2011 03:39, Uncontrolled Copy, (c) BSIBS EN 2482:2010EN 2482:2010 (E) 7 34 Grain size See EN 4700-002. 7 G 5 44 External

28、 defects See EN 4700-002. 1 Visual 50 Cleanliness/inclusion content See EN 4700-002. (micro-cleanness) 1 EN 2951 7 Category 2 61 Internal defects See EN 4700-002. 1 EN 4050-4 6 A or D 35 may be tested either on the product or at an earlier stage of manufacturing 7 Class 2 95 Marking inspection See E

29、N 4700-002. 96 Dimensional inspection See EN 4700-002. 98 Notes a HV for De 5 mm. 99 Typical use Low alloy general purpose steel. Licensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 09/10/2011 03:39, Uncontrolled Copy, (c) BSIBS EN 2482:2010 EN 2482:2010 (E) 8 100 Product qualification Qualificat

30、ion programme to be agreed between manufacturer and purchaser. Licensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 09/10/2011 03:39, Uncontrolled Copy, (c) BSIThis page deliberately left blankLicensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 09/10/2011 03:39, Uncontrolled Copy, (c) BSIBSI is

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