EN 2119-2017 Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated - Wires for rivets - 2 mm D 10 mm.pdf

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1、BSI Standards PublicationWB11885_BSI_StandardCovs_2013_AW.indd 1 15/05/2013 15:06Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated - Wires for rivets - 2 mm D 10 mm - Rm 960 MPaBS EN 2119:2017EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE

2、 NORM EN 2119 December 2017 ICS 49.025.05 English Version Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated - Wires for rivets - 2 mm D 10 mm - Rm 960 MPa Srie arospatiale - Acier rsistant chaud FE-PA2601 (X6NiCrTiMoV26-15) - Mis en sol

3、ution et prcipit - Fils pour rivets - 2 mm D 10 mm - Rm 960 MPa Luft- und Raumfahrt - Hochwarmfeste Legierung FE-PA2601 (X6NiCrTiMoV26-15) - Lsungsgeglht und ausgehrtet - Drahte fr Niete - 2 mm D 10 mm - Rm 960 MPa This European Standard was approved by CEN on 11 September 2017. CEN members are boun

4、d 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 application to the CE

5、N-CENELEC 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-CENELEC Management Centre h

6、as the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, L

7、uxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Serbia, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG CEN-CENELEC Management Centre: Avenue Marnix 17, B

8、-1000 Brussels 2017 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 2119:2017 ENational forewordThis British Standard is the UK implementation of EN 2119:2017.The UK participation in its preparation was entrusted to Technical Commi

9、ttee ACE/61/-/48, Heat Resisting Alloys for Aerospace Purposes.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 contract. Users are responsible for its correct application.

10、 The British Standards Institution 2018 Published by BSI Standards Limited 2018ISBN 978 0 580 98674 1ICS 49.025.05Compliance with a British Standard cannot confer immunity from legal obligations.This British Standard was published under the authority of the Standards Policy and Strategy Committee on

11、 31 January 2018.Amendments/corrigenda issued since publicationDate Text affectedBRITISH STANDARDBS EN 2119:2017EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 2119 December 2017 ICS 49.025.05 English Version Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treate

12、d and precipitation treated - Wires for rivets - 2 mm D 10 mm - Rm 960 MPa Srie arospatiale - Acier rsistant chaud FE-PA2601 (X6NiCrTiMoV26-15) - Mis en solution et prcipit - Fils pour rivets - 2 mm D 10 mm - Rm 960 MPa Luft- und Raumfahrt - Hochwarmfeste Legierung FE-PA2601 (X6NiCrTiMoV26-15) - Lsu

13、ngsgeglht und ausgehrtet - Drahte fr Niete - 2 mm D 10 mm - Rm 960 MPa This European Standard was approved by CEN on 11 September 2017. 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

14、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

15、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, Czech

16、 Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Serbia, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and United King

17、dom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG CEN-CENELEC Management Centre: Avenue Marnix 17, B-1000 Brussels 2017 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 2119:20

18、17 EBS EN 2119:2017EN 2119:2017 (E) 2 Contents Page European foreword 3 Introduction 4 1 Scope 5 2 Normative references 5 3 Requirements . 5 BS EN 2119:2017EN 2119:2017 (E) 3 European foreword This document (EN 2119:2017) has been prepared by the Aerospace and Defence Industries Association of Europ

19、e - 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 Stand

20、ard shall be given the status of a national standard, either by publication of an identical text or by endorsement, at the latest by June 2018 and conflicting national standards shall be withdrawn at the latest by June 2018. Attention is drawn to the possibility that some of the elements of this doc

21、ument may be the subject of patent rights. CEN 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 Standard: Austria, Belgi

22、um, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Serbia, Slovakia, Slovenia, Spain, Sweden,

23、 Switzerland, Turkey and the United Kingdom. BS EN 2119:2017EN 2119:2017 (E) 4 Introduction This European 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 European Standard has been prep

24、ared in accordance with EN 4500-003. BS EN 2119:2017EN 2119:2017 (E) 5 1 Scope This European Standard specifies the requirements relating to: Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) Solution treated and precipitation treated Wires for rivets 2 mm D 10 mm Rm 960 MPa for aerospace applicatio

25、ns. 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 references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any a

26、mendments) applies. EN 2043, Aerospace series Metallic materials General requirements for semi-finished product qualification (excluding forgings and castings) EN 3238, Aerospace series Metallic materials Test method Shear test for wires and rivets EN 4258, Aerospace series Metallic materials Genera

27、l organization of standardization Links between types of EN standards and their use EN 4500-003, Aerospace series Metallic materials Rules for drafting and presentation of material standards Part 003: Specific rules for heat resisting alloys EN 4700-002, Aerospace series Steel and heat resisting all

28、oys Wrought products Technical specification Part 002: Bar and section EN 4700-004, Aerospace series Steel and heat resisting alloys Wrought products Technical specification Part 004: Wire 3 Requirements See Table 1. BS EN 2119:2017EN 2119:2017 (E) 6 Table 1 Requirements for heat resisting alloy FE-

29、PA2601 1 Material designation Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) 2 Chemical Composition % Element C Si Mn P S Al B Cr Mo Ni Ti V Pb Fe min. 30 * 13,5 1,00 24,0 1,90 0,10 Base max. 0,080 1,00 2,00 0,020 0,015 0,35 100 * 16,0 1,50 27,0 2,30 0,50 20 * 3 Method of melting Consumable elect

30、rode remelted 4.1 Form Wire 4.2 Method of production 4.3 Limit dimension(s) mm 2 D 10 5 Technical specification EN 4700-004 6.1 Delivery condition Solution treated Heat treatment 900 C 930 C a/t 15 min/OQ or WQ 6.2 Delivery condition code W 7 Use condition Solution treated and precipitation treated

31、Heat treatment Delivery condition + 680 C 780 C/t 30 min/AC Characteristics 8.1 Test sample(s) See EN 4700-002. 8.2 Test piece(s) See EN 4700-002. 8.3 Heat treatment Delivery condition Use condition 9 Dimensions concerned mm 2 D 10 2 D 10 10 Thickness of cladding on each face % 11 Direction of test

32、piece See EN 4700-004. See EN 4700-004. 12 T Temperature C Ambient Ambient 13 Proof stress Rp0,2 MPa 14 Strength Rm MPa 720 960 15 Elongation A % 16 Reduction of area Z % 17 Hardness 205 HV 260 HV 18 Shear strength Rc MPa 550 Rc 650 b19 Bending k 20 Impact strength 21 C Temperature C 22 Time h 23 St

33、ress a MPa 24 Elongation a % 25 Rupture stress R MPa 26 Elongation at rupture A % 27 Notes (see line 98) *, a, bBS EN 2119:2017EN 2119:2017 (E) 7 34 Grain size See EN 4700-004. 2 One per batch 3 L and LT 7 G 5 - No duplex structure 36 Reverse torsion test for wires See EN 4700-004. 7 6 turns in each

34、 direction 37 Bending of wires (Reverse bend) See EN 4700-004. 7 5 times without failure 44 External defects External imperfections See EN 4700-004. 1 Only visual testing is required 95 Marking inspection See EN 4700-004. 96 Dimensional inspection See EN 4700-004. 98 Notes *p.p.m. aHeat treatment at

35、 = 980 C 10 C may be used by agreement between manufacturer and purchaser. bSee EN 3238. 99 Typical use BS EN 2119:2017EN 2119:2017 (E) 8 100 Product qualification See EN 2043. Qualification programme to be agreed between manufacturer and purchaser. BS EN 2119:2017This page deliberately left blankTh

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