BS EN 2213-2012 Aerospace series Steel FE-PL1505 (15CrMoV6) Air melted Hardened and tempered Bars De 16 mm 980 MPa Rm 1180 MPa《航空航天系列 FE-PL1505 (15CrMoV6)钢制 气融 淬火与回火 钢筋 De 16 mm 98.pdf

《BS EN 2213-2012 Aerospace series Steel FE-PL1505 (15CrMoV6) Air melted Hardened and tempered Bars De 16 mm 980 MPa Rm 1180 MPa《航空航天系列 FE-PL1505 (15CrMoV6)钢制 气融 淬火与回火 钢筋 De 16 mm 98.pdf》由会员分享，可在线阅读，更多相关《BS EN 2213-2012 Aerospace series Steel FE-PL1505 (15CrMoV6) Air melted Hardened and tempered Bars De 16 mm 980 MPa Rm 1180 MPa《航空航天系列 FE-PL1505 (15CrMoV6)钢制 气融 淬火与回火 钢筋 De 16 mm 98.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 2213:2012Aerospace series Steel FE-PL1505 (15CrMoV6) Air melted Hardened and tempered Bars De 16 mm 980 MPa Rm 1 180 MPaBS EN 2213:2012 BRITISH STANDARDNational forewordThi

2、s British Standard is the UK implementation of EN 2213:2012.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.This publication does no

3、t purport to include all the necessaryprovisions of a contract. Users are responsible for its correctapplication. The British Standards Institution 2012. Published by BSI StandardsLimited 2012ISBN 978 0 580 76574 2ICS 49.025.10Compliance with a British Standard cannot confer immunity fromlegal oblig

4、ations.This British Standard was published under the authority of theStandards Policy and Strategy Committee on 31 March 2012.Amendments issued since publicationDate Text affectedBS EN 2213:2012EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 2213 March 2012 ICS 49.025.10 English Version Aerospa

5、ce series - Steel FE-PL1505 (15CrMoV6) - Air melted - Hardened and tempered - Bars - De 16 mm - 980 MPa Rm 1 180 MPa Srie arospatiale - Acier FE-PL1505 (15CrMoV6) - labor lair - Tremp et revenu - Barres - De 16 mm - 980 MPa Rm 1 180 MPa Luft- und Raumfahrt - Stahl FE-PL1505 (15CrMoV6) - Lufterschmol

6、zen - Gehrtet und angelassen - Stangen - De 16 mm - 980 MPa Rm 1 180 MPa This European Standard was approved by CEN on 23 December 2011. 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

7、 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, German). A version

8、 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, Croatia, Cyprus, Czec

9、h 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, Turkey and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION CO

10、MIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG Management Centre: Avenue Marnix 17, B-1000 Brussels 2012 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 2213:2012: EBS EN 2213:2012EN 2213:2012 (E) 2 Contents Page Forew

11、ord 3Introduction .41 Scope 52 Normative references 5BS EN 2213:2012EN 2213:2012 (E) 3 Foreword This document (EN 2213:2012) 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 rule

12、s 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 text

13、or by endorsement, at the latest by September 2012, and conflicting national standards shall be withdrawn at the latest by September 2012. 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 respon

14、sible 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, Finlan

15、d, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the United Kingdom. BS EN 2213:2012EN 2213:2012 (E) 4 Introduction This standard is part of t

16、he series of 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. BS EN 2213:2012EN 2213:2012 (E) 5 1 Scope This European Standard specifies the requirements relating

17、to: Steel FE-PL1505 (15CrMoV6) Air melted Hardened and tempered Bars De 16 mm 980 MPa Rm 1 180 MPa for aerospace applications. 2 Normative references The following documents, in whole or in part, are normatively referenced in this document and are indispensable for its application. For dated referen

18、ces, only the edition cited applies. For undated references, the latest 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 2951, Aerosp

19、ace 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 EN 4258, Aerospace series M

20、etallic 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 and heat resist

21、ing alloys Wrought products Technical specification Part 002: Bar and section EN ISO 642, Steel Hardenability test by end quenching (Jominy test) (ISO 642) 1) Published as ASD-STAN pre-standard at the date of publication of this standard by Aerospace and Defence Industries Association of Europe-Stan

22、dardization (ASD-STAN), (www.asd-stan.org). BS EN 2213:2012EN 2213:2012 (E) 6 1 Material designation Steel FE-PL1505 (15CrMoV6) 2 Chemical composition % Element C Si Mn P S Cr Mo V Fe min. 0,12 0,80 1,25 0,80 0,20 Base max. 0,18 0,20 1,10 0,020 0,015 1,50 1,00 0,30 3 Method of melting Air melted 4.1

23、 Form Bars 4.2 Method of production 4.3 Limit dimension(s) mm De 16 5 Technical specification EN 4700-002 6.1 Delivery condition Annealed Hardened and tempered Heat treatment 955 C 995 C / AC + 615 C 655 C a6.2 Delivery condition code A U 7 Use condition Hardened and tempered Delivery condition Heat

24、 treatment Delivery condition 955 C 995 C / AC + 615 C 655 C a 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 16 10 Thickness of cladding on each face % 11 Direction of test piece L

25、 12 T Temperature C Ambient 13 Proof stress Rp0,2 MPa 780 14 Strength Rm MPa 980 Rm 1 180 15 Elongation A % 12 b16 Reduction of area Z % 17 Hardness HB 197 291 HB 350 18 Shear strength Rc MPa 19 Bending k 20 Impact strength KV J 30 21 C Temperature C 22 Time h 23 Stress a MPa 24 Elongation a % 25 Ru

26、pture stress R MPa 26 Elongation at rupture A % 27 Notes (see line 98) a, bBS EN 2213:2012EN 2213:2012 (E) 7 31 Hardenabilty (Jominy test) See EN 4700-002. 1 EN ISO 642 7 The “capability clause“ applies Distance in mm 1,5 5 9 15 25 40 HRC min. 38 37 35 32 31 29 34 Grain size See EN 4700-002. 7 G 5 4

27、4 External defects See EN 4700-002. 1 Visual 50 Cleanliness/inclusion content See EN 4700-002. (Micro cleanness) 1 EN 29517 Category 1 51 Macrostructure (Grain flow) See EN 4700-002. 61 Internal defects See EN 4700-002. 7 Class 3, see EN 4050-4. 95 Marking inspection See EN 4700-002. 96 Dimensional

28、inspection See EN 4700-002. 98 Notes a The range of temperature of tempering shall be adjusted on the wire rod if the bar is made from cold working b In case of cold working transformation, elongation could be 10 % minimum. 99 Typical use BS EN 2213:2012EN 2213:2012 (E) 8 100 Product qualification S

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