1、BRITISH STANDARDBS EN 4315:2007Aerospace series Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) Solution treated and precipitation treated, bar and section a or D k 100 mm, Rm U 900 MPaICS 49.025.05g49g50g3g38g50g51g60g44g49g42g3g58g44g55g43g50g56g55g3g37g54g44g3g51g40g53g48g44g54g54g44g50g49g3g40
2、g59g38g40g51g55g3g36g54g3g51g40g53g48g44g55g55g40g39g3g37g60g3g38g50g51g60g53g44g42g43g55g3g47g36g58BS EN 4315:2007This British Standard was published under the authority of the Standards Policy and Strategy Committee on 31 March 2008 BSI 2008ISBN 978 0 580 61218 3National forewordThis British Stand
3、ard is the UK implementation of EN 4315:2007. The UK participation in its preparation was entrusted by Technical Committee ACE/61, Metallic materials for aerospace purposes, to Panel ACE/61/-/48, Heat resisting alloys.A list of organizations represented on this committee can be obtained on request t
4、o its secretary.This publication does not purport to include all the necessary provisions of a contract. Users are responsible for its correct application.Compliance with a British Standard cannot confer immunity from legal obligations.Amendments/corrigenda issued since publicationDate CommentsEUROP
5、EAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4315 August 2007 ICS 49.025.05 English Version Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section a or D 100 mm, Rm 900 MPa Srie arospatiale - Alliage rsistant chaud FE-PA2
6、601 (X6NiCrTiMoV26-15) - Mis en solution et prcipit, barres et profils a ou D 100 mm, Rm 900 MPa Luft- und Raumfahrt - Hochwarmfeste Legierung FE-PA2601 (X6NiCrTiMoV26-15) - Lsungsgeglht und ausgehrtet, Stangen und Profile a oder D 100 mm, Rm 900 MPa This European Standard was approved by CEN on 15
7、March 2007. 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 o
8、btained on application to the CEN 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 CEN Man
9、agement Centre has the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, N
10、orway, 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: rue de Stassart, 36 B-1050 Brussels 2007 CEN All rights of exploitation in any
11、form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4315:2007: E2 Contents Page Foreword3 Introduction .4 1 Scope 4 2 Normative references 4 EN 4315:20073 Foreword This document (EN 4315:2007) has been prepared by the Aerospace and Defence Industries Association of Europe
12、- 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 countries of ASD, prior to its presentation to CEN. This European Standar
13、d 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 2008. Attention is drawn to the possibility that some of the elements of t
14、his 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 organizations of the following countries are bound to implement this European St
15、andard: Austria, 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 the United Kingdo
16、m. EN 4315:20074 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 prepared in accordance with EN 4500-3. 1 Scope This standard specifies the requireme
17、nts relating to: Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) Solution treated and precipitation treated, bar and section a or D 100 mm, Rm 900 MPa for aerospace applications. 2 Normative references The following referenced documents are indispensable for the application of this document. For d
18、ated references, 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
19、2860-2, Aerospace series Heat resisting alloys Forging stock and forgings Technical specification Part 2: Forging stock1) EN 4258, Aerospace series Metallic materials General organization of standardization Links between types of EN standards and their use EN 4500-3, Aerospace series Metallic materi
20、als 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 prestandard at the date of publication of
21、this standard. EN 4315:20075 1 Material designation Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) Element C Si Mn PS Al B Cr Mo Ni Ti V Pb Fe min. 30a13,5 1,00 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
22、Consumable electrode remelted 4.1 Form Bar and section 4.2 Method of production Rolled, extruded 4.3 Limit dimension(s) mm a or D 100 5 Technical specification EN 4700-2 Delivery condition Solution treated Solution treated and precipitation treated 6.1 Heat treatment = 980 C 10 C / t 1 h / OQ or WQ
23、= 980 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 condition 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
24、.2 Test piece(s) See EN 4700-2 See EN 4700-2 8.3 Heat treatment Solution treated Use condition 9 Dimensions concerned mm a or D 100 a or D 100 10 Thickness of cladding on each face % 11 Direction of test piece See EN 4700-2 12 Temperature C Ambient 13 Proof stress Rp0,2 MPa 590 14 T Strength RmMPa 9
25、00 15 Elongation A % 13 16 Reduction of area Z % 20 17 Hardness 201 HB 248 HB 341 18 Shear strength RcMPa 19 Bending k 20 Impact strength 21 Temperature C 650b22 Time h tR 23 23 Stress aMPa 24 C Elongation a % 25 Rupture stress RMPa 480 26 Elongation at ruptureA % 5 for tR 48 h 3 for tR 48 h 27 Note
26、s (see line 98) a, b EN 4315:20076 See EN 4700-2 34 Grain size 7 G 3 See EN 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
27、EN 4700-2 98 Notes ap.p.m. bProportional round test piece.99 Typical use EN 4315:20077 See EN 2043 100 Product qualification Qualification programme to be agreed between manufacturer and purchaser. EN 4315:2007BS EN 4315:2007BSI389 Chiswick High RoadLondonW4 4ALBSI British Standards InstitutionBSI i
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