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 2011BS EN 2482:2010 BRITISH STANDA
2、RDNational 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.A list of organizations represented on this committee can beobtained on request to its secretary.Th
3、is 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 British Standard cannot confer immunity fromlegal obligations.This British Standard was published under
4、 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 Implementation of CEN corrected text to change the title of the standardEUROPEAN STANDARD NORME EUROPEN
5、NE EUROPISCHE NORM EN 2482 December 2010 ICS 49.025.10 English Version Aerospace series - Steel FE-PL2108 (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 (36NiC
6、rMo16) - 1 100 MPa Rm 1 300 MPa - Stangen - De 100 mm This European Standard was approved by CEN on 2 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 al
7、teration. 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 versions (English, French, German). A version in any other language m
8、ade 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, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Est
9、onia, 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 COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUR
10、OPISCHES KOMITEE FR NORMUNG Management Centre: Avenue Marnix 17, B-1000 Brussels 2010 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 2482:2010: EBS EN 2482:2010EN 2482:2010 (E) 2 Contents Foreword 3Introduction .41 Scope 52 Normat
11、ive references 5BS 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 enquiries and votes carried out in accordance with the rules of this Association, this Standard
12、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 publication of an identical text or by endorsement, at the latest by J
13、une 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 rights. CEN and/or CENELEC shall not be held responsible for identifying any or all such patent ri
14、ghts. 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 Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, I
15、reland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. BS EN 2482:2010EN 2482:2010 (E) 4 Introduction This standard is part of the series of EN metallic material standards for aerospa
16、ce applications. The general organization of this series is described in EN 4258. This standard has been prepared in accordance with EN 4500-5. BS 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
17、100 mm 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)
18、applies. 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,
19、 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 steels 1)EN 4700-002, Aerospace series St
20、eel and 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). BS EN 2482:2010 E
21、N 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 0,60 4,20 3 Method of melting Air melted 4.1 Form Bars 4.2 Method of production 4.3 Limit dimens
22、ion(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 and tempered Delivery condition Heat treatment Delivery condition + 860 C 890 C / AQ + 560 C C
23、haracteristics 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 % 11 Direction of test piece 12 T Temperature C Ambient 13 Proof stress Rp0,2MPa 900 14 Stren
24、gth 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 22 Time h 23 Stress aMPa 24 Elongation a % 25 Rupture stress RMPa 26 Elongation at rupture A
25、% 27 Notes (see line 98) aBS EN 2482:2010EN 2482:2010 (E) 7 34 Grain size See EN 4700-002. 7 G 5 44 External 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 b
26、e tested either on the product or at an earlier stage of manufacturing 7 Class 2 95 Marking inspection See EN 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. BS EN 2482:2010 EN 2482:2010 (E) 8 100 Product qualification Q
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