BS EN 4318-2007 Aerospace series - nHeat resisting alloy nFE-PA2601 n(X6NiCrTiMoV26-15) - nSolution treated and nprecipitation treated nbar and section nDe ≤ 100 mm nRm ≥ 960 MPa《航.pdf

1、Licensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 13/05/2008 01:52, Uncontrolled Copy, (c) BSIg49g50g3g38g50g51g60g44g49g42g3g58g44g55g43g50g56g55g3g37g54g44g3g51g40g53g48g44g54g54g44g50g49g3g40g59g38g40g51g55g3g36g54g3g51g40g53g48g44g55g55g40g39g3g37g60g3g38g50g51g60g53g44g42g43g55g3g47g36g58(

2、X6NiCrTiMoV26-15) Solution treated and precipitation treated, bar and section De k 100 mm, Rm U 960 MPaICS 49.025.05Aerospace series Heat resisting alloy FE-PA2601 BRITISH STANDARDBS EN 4318:2007BS EN 4318:2007Licensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 13/05/2008 01:52, Uncontrolled Copy

3、, (c) BSIThis British Standard was published under the authority of the Standards Policy and Strategy Committee on 31 March 2008 BSI 2008ISBN 978 0 580 61220 6Amendments/corrigenda issued since publicationDate Commentscontract. Users are responsible for its correct application.Compliance with a Brit

4、ish Standard cannot confer immunity from legal obligations.National forewordThis British Standard is the UK implementation of EN 4318:2007. The UK participation in its preparation was entrusted by Technical Committee ACE/61, Metallic materials for aerospace purposes, to Panel ACE/61/-/48, Heat resis

5、ting alloys.A list of organizations represented on this committee can be obtained on request to its secretary.This publication does not purport to include all the necessary provisions of a EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4318 August 2007 ICS 49.025.05 English Version Aerospace s

6、eries - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section De 100 mm, Rm 960 MPa Srie arospatiale - Alliage rsistant chaud FE-PA2601 (X6NiCrTiMoV26-15) - Mis en solution et prcipit, barres et profils De 100 mm, Rm 960 MPa Luft- und Raumfah

7、rt - Hochwarmfeste Legierung FE-PA2601 (X6NiCrTiMoV26-15) - Lsungsgeglht und ausgehrtet, Stangen und Profile De 100 mm, Rm 960 MPa This European Standard was approved by CEN on 15 February 2007. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions

8、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. This European Standard exists in three offi

9、cial 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 are the national standards bodies of Austria

10、, 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, Switzerland and United Kingdom. EUROPEAN COMMITT

11、EE 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. EN 4318:2007: ELicensed Copy: Wang Bin, I

12、SO/EXCHANGE CHINA STANDARDS, 13/05/2008 01:52, Uncontrolled Copy, (c) BSI2 Contents Page Introduction .4 1 Scope 4 2 Normative references 4 EN 4318:2007Licensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 13/05/2008 01:52, Uncontrolled Copy, (c) BSI3 Foreword This document (EN 4318:2007) has been

13、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 has received the approval of the National Associations and the Official Services of the member co

14、untries 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 February 2008, and conflicting national standards shall be withdrawn at the latest by February 200

15、8. 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 rights. According to the CEN/CENELEC Internal Regulations, the national standards organizat

16、ions of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romani

17、a, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. EN 4318:2007Licensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 13/05/2008 01:52, Uncontrolled Copy, (c) BSI4 Introduction This standard is part of the series of EN metallic material standards for aerospace applications. Th

18、e general organization of this series is described in EN 4258. This standard has been prepared in accordance with EN 4500-3. 1 Scope This standard specifies the requirements relating to: Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) Solution treated and precipitation treated, bar and section De

19、100 mm, Rm 960 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 latest edition of the referenced document (including any

20、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 Links between types of EN standards and their use EN

21、4500-3, Aerospace series Metallic materials Rules for drafting and presentation of material standards Part 3: Specific rules for heat resisting alloys1)EN 4700-2, Aerospace series Steel and heat resisting alloys Wrought products Technical specification Part 2: Bar and section1)1) Published as ASD pr

22、estandard at the date of publication of this standard. EN 4318:2007Licensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 13/05/2008 01:52, Uncontrolled Copy, (c) BSI5 1 Material designation Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) Element C Si Mn P S Al B Cr Mo Ni Ti V Pb Fe min. 30a13,5 1

23、,00 24,0 1,90 0,10 2 Chemical composition % max. 0,080 1,00 2,00 0,020 0,015 0,35 100a16,0 1,50 27,0 2,30 0,50 20a Base 3 Method of melting Consumable electrode remelted 4.1 Form Bar and section 4.2 Method of production Rolled, extruded 4.3 Limit dimension(s) mm De 100 5 Technical specification EN 4

24、700-2 Delivery condition Solution treated Solution treated and precipitation treated 6.1 Heat treatment = 900 C 10 C / t 1 h / OQ or WQ = 900 C 10 C / t 1 h / OQ or WQ + = 720 C 10 C / t = 16 h / AC 6.2 Delivery condition code W U Use condition Solution treated and precipitation treated Delivery con

25、dition 7 Heat treatment Delivery condition + = 720 C 10 C / t = 16 h / AC Characteristics 8.1 Test sample(s) See EN 4700-2 See EN 4700-2 8.2 Test piece(s) See EN 4700-2 See EN 4700-2 8.3 Heat treatment Solution treated Use condition 9 Dimensions concerned mm De 100 De 100 10 Thickness of cladding on

26、 each face % 11 Direction of test piece See EN 4700-2 12 Temperature C Ambient 13 Proof stress Rp0,2 MPa 655 14 T Strength RmMPa 960 15 Elongation A % 10 16 Reduction of area Z % 15 17 Hardness 201 HB 277 HB 363 18 Shear strength RcMPa 19 Bending k 20 Impact strength 21 Temperature C 650 22 Time h t

27、R 23 23 Stress aMPa 24 C Elongation a % 25 Rupture stress RMPa 450 26 Elongation at ruptureA % 5 for tR 48 h 3 for tR 48 h27 Notes (see line 98) aEN 4318:2007Licensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 13/05/2008 01:52, Uncontrolled Copy, (c) BSI6 See EN 4700-2 34 Grain size 7 G 3 See EN

28、4700-2 44 External defects 1 Only visual is required See EN 4700-2 51 Macrostructure 7 To be defined on the order See EN 4700-2 61 Internal defects 7 Class 2 96 Marking inspection See EN 4700-2 97 Dimensional inspection See EN 4700-2 98 Notes ap.p.m. 99 Typical use EN 4318:2007Licensed Copy: Wang Bi

29、n, ISO/EXCHANGE CHINA STANDARDS, 13/05/2008 01:52, Uncontrolled Copy, (c) BSI7 See EN 2043 100 Product qualification Qualification programme to be agreed between manufacturer and purchaser. EN 4318:2007Licensed Copy: Wang Bin, ISO/EXCHANGE CHINA STANDARDS, 13/05/2008 01:52, Uncontrolled Copy, (c) BS

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