1、raising standards worldwideNO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBSI Standards PublicationBS EN 2483:2010Aerospace series Steel FE-PL2108 (36NiCrMo16) 1 100 MPa null Rm null 1 300 MPa Forgings De null 100 mmIncorporating corrigendum June 2011BS EN 2483:2010 BRITISH ST
2、ANDARDNational forewordThis British Standard is the UK implementation of EN 2483:2010,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 secretar
3、y.This publication does not purport to include all the necessaryprovisions of a contract. Users are responsible for its correctapplication. BSI 2011ISBN 978 0 580 7 ICS 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 issued since publicationDate Text affected5051 9incorporating corrigendum December 2010.30 June 2011 Implementation of CEN corrected text to change the title of the standardEUROPEAN STANDARD NORME EUROPENNE EUR
5、OPISCHE NORM EN 2483 December 2010 ICS 49.025.10 English Version Aerospace series - Steel FE-PL2108 (36NiCrMo16) - 1 100 MPa Rm 1 300 MPa - Forgings - De 100 mm Srie arospatiale - Acier FE-PL2108 (36NiCrMo16) - 1 100 MPa Rm 1 300 MPa - Pices forges et matrices - De 100 mm Luft- und Raumfahrt - Stahl
6、 FE-PL2108 (36NiCrMo16) - 1 100 MPa Rm 1 300 MPa - Gesenk- und Freiformschmiedestcke - 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 s
7、tatus 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 versions (English, French,
8、 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, Belgium, Bulgaria, Cr
9、oatia, 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 COMMITTEE FOR STANDAR
10、DIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES 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 2483:2010: EBS EN 2483:2010 EN 2483:2010 (E) 2 Content
11、s Foreword 3Introduction . 41Scope 42Normative references 4BS EN 2483:2010EN 2483:2010 (E) 3 Foreword This document (EN 2483:2010) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). After enquiries and votes carried out in accordance with th
12、e 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 publication of an identical
13、 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 rights. CEN and/or CENELEC shall not be held responsibl
14、e 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 Republic, Denmark, Estonia, Finland, F
15、rance, 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 2483:2010 EN 2483:2010 (E) 4 Introduction This standard is part of the series o
16、f 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-PL2108 (36NiCrMo16) 1 100 MPa Rm 1 300 MP
17、a Forgings De 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 an
18、y amendments) applies. 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, Aerospace series Metallic materials General organization of standardization Links between types of EN standar
19、ds 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 4700-006, Aerospace series Steel and heat resisting alloys Wrought products Technical specification Part 006: Pre-production and production
20、 forgings 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 2483:2010EN 2483:2010 (E) 5 1 Material designation Steel FE-PL2108 (36NiCrMo16) 2 Chemical composi
21、tion % 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 Forgings 4.2 Method of production Forged from forging stock EN xxxx 2)4.3 Limit dimension(s) mm De 100 5 Technical specification EN 47
22、00-006 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 Characteristics 8.1 Test sample(s) See EN 4700-00
23、6. 8.2 Test piece(s) See EN 4700-006. 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 Strength RmMPa 1 100 Rm 1 300 15 Elongation A % 10 16
24、 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 % 27 Notes (see line 98) a2) In preparation at t
25、he date of publication of this standard. BS EN 2483:2010 EN 2483:2010 (E) 6 34 Grain size See EN 4700-006. 7 G 5 44 External defects See EN 4700-006. 50 Cleanliness/inclusion content (micro-cleanness) See EN 4700-006. 61 Internal defects See EN 4700-006. 1 EN 4050-4 7 Class 2 95 Marking inspection S
26、ee EN 4700-006. 96 Dimensional inspection See EN 4700-006. 98 Notes a HV for De 5 mm. 99 Typical use Low alloy general purpose steel. BS EN 2483:2010EN 2483:2010 (E) 7 100 Product qualification Qualification programme to be agreed between manufacturer and purchaser. This page deliberately left blank
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