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1、BRITISH STANDARD BS EN 4318:2007 Aerospace series Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) Solution treated and precipitation treated, bar and section De kk 100 mm, Rm UU 960 MPa ICS 49.025.05 ? Copyright British Standards Institution Provided by IHS under license with BSI - Uncontrolled Co
2、py Licensee=Boeing Co/5910770001 Not for Resale, 08/14/2008 20:33:21 MDTNo reproduction or networking permitted without license from IHS -,-,- BS EN 4318:2007 This British Standard was published under the authority of the Standards Policy and Strategy Committee on 31 March 2008 BSI 2008 ISBN 978 0 5
3、80 61220 6 National foreword This 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 resisting alloys. A list of organizations represente
4、d on this committee can be obtained on request to 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/co
5、rrigenda issued since publication DateComments Copyright British Standards Institution Provided by IHS under license with BSI - Uncontrolled Copy Licensee=Boeing Co/5910770001 Not for Resale, 08/14/2008 20:33:21 MDTNo reproduction or networking permitted without license from IHS -,-,- EUROPEAN STAND
6、ARD NORME EUROPENNE EUROPISCHE NORM EN 4318 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 De 100 mm, Rm 960 MPa Srie arospatiale - Alliage rsistant chaud FE-PA2601 (X6NiCrTi
7、MoV26-15) - Mis en solution et prcipit, barres et profils De 100 mm, Rm 960 MPa Luft- und Raumfahrt - 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 mem
8、bers 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 obtained on applicat
9、ion 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 Management Centre has
10、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, Norway, Poland, Port
11、ugal, 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 form and by any mea
12、ns reserved worldwide for CEN national Members. Ref. No. EN 4318:2007: E Copyright British Standards Institution Provided by IHS under license with BSI - Uncontrolled Copy Licensee=Boeing Co/5910770001 Not for Resale, 08/14/2008 20:33:21 MDTNo reproduction or networking permitted without license fro
13、m IHS -,-,- 2 Contents Page Introduction.4 1 Scope 4 2 Normative references4 EN 4318:2007 Copyright British Standards Institution Provided by IHS under license with BSI - Uncontrolled Copy Licensee=Boeing Co/5910770001 Not for Resale, 08/14/2008 20:33:21 MDTNo reproduction or networking permitted wi
14、thout license from IHS -,-,- 3 Foreword This document (EN 4318:2007) 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 has received the ap
15、proval 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 February 2008, and c
16、onflicting national standards shall be withdrawn at the latest by February 2008. 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. Accor
17、ding to the CEN/CENELEC Internal Regulations, the national standards organizations 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, Latvi
18、a, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. EN 4318:2007 Copyright British Standards Institution Provided by IHS under license with BSI - Uncontrolled Copy Licensee=Boeing Co/5910770001 Not fo
19、r Resale, 08/14/2008 20:33:21 MDTNo reproduction or networking permitted without license from IHS -,-,- 4 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
20、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 100 mm, Rm 960 MPa for aerospace applications. 2 Normative references The followi
21、ng 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) applies. EN 2043, Aerospace series Metallic materials General require
22、ments 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 4500-3, Aerospace series Metallic materials Rules for drafting and presentation
23、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 this standard. EN 4318:2007 Copyright
24、British Standards Institution Provided by IHS under license with BSI - Uncontrolled Copy Licensee=Boeing Co/5910770001 Not for Resale, 08/14/2008 20:33:21 MDTNo reproduction or networking permitted without license from IHS -,-,- 5 1 Material designation Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-
25、15) Element C Si Mn P S Al B Cr Mo Ni Ti V Pb Fe min. 30a13,51,00 24,0 1,90 0,10 2 Chemical composition % max. 0,080 1,002,000,020 0,0150,35100a16,01,50 27,0 2,30 0,5020a Base 3 Method of melting Consumable electrode remelted 4.1 Form Bar and section 4.2 Method of production Rolled, extruded 4.3 Lim
26、it dimension(s) mm De 100 5 Technical specification EN 4700-2 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
27、 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 8.2 Test piece(s) See EN 4700-2 See EN 4700-2 8.3 Heat treatment Solution treated Use condition 9 Dimension
28、s concerned mm De 100 De 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 655 14 T Strength Rm MPa 960 15 Elongation A % 10 16 Reduction of area Z % 15 17 Hardness 201 HB 277 HB 363 18 Shear strength Rc MPa 19 Ben
29、ding k 20 Impact strength 21 Temperature C 650 22 Time h tR 23 23 Stress a MPa 24 C Elongation a % 25 Rupture stress R MPa 450 26 Elongation at rupture A % 5 for tR 48 h 3 for tR 48 h 27 Notes (see line 98) a EN 4318:2007 Copyright British Standards Institution Provided by IHS under license with BSI
30、 - Uncontrolled Copy Licensee=Boeing Co/5910770001 Not for Resale, 08/14/2008 20:33:21 MDTNo reproduction or networking permitted without license from IHS -,-,- 6 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 def
31、ined 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 a p.p.m. 99 Typical use EN 4318:2007 Copyright British Standards Institution Provided by IHS under license with BSI - Uncontrolled Copy Licensee=Boeing C
32、o/5910770001 Not for Resale, 08/14/2008 20:33:21 MDTNo reproduction or networking permitted without license from IHS -,-,- 7 See EN 2043 100 Product qualification Qualification programme to be agreed between manufacturer and purchaser. EN 4318:2007 Copyright British Standards Institution Provided by
33、 IHS under license with BSI - Uncontrolled Copy Licensee=Boeing Co/5910770001 Not for Resale, 08/14/2008 20:33:21 MDTNo reproduction or networking permitted without license from IHS -,-,- BS EN 4318:2007 BSI 389 Chiswick High Road London W4 4AL BSI British Standards Institution BSI is the independen
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