1、BS EN 4372:2009Aerospace series Heat resisting nickelalloy with copper NIPD9001 (NiCu31) Wire for solid rivets D 10 mmICS 49.025.15BRITISH STANDARDNO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWThis British Standard was published under the authority of the Standards Policy and
2、 Strategy Committee on 31 July2009. BSI 2009ISBN 978 0 580 67406 8Amendments/corrigenda issued since publicationDate CommentsBS EN 4372:2009National forewordThis British Standard is the UK implementation of EN 4372:2009. The UK participation in its preparation was entrusted to TechnicalCommittee ACE
3、/61/-/48, Heat resisting alloys.A list of organizations represented on this committee can be obtained onrequest to its secretary.This publication does not purport to include all the necessary provisionsof a contract. Users are responsible for its correct application. Compliance with a British Standa
4、rd cannot confer immunityfrom legal obligations.BS EN 4372:2009EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4372 February 2009 ICS 49.025.15 English Version Aerospace series - Heat resisting nickel alloy with copper NI-PD9001 (NiCu31) - Wire for solid rivets - D 10 mm Srie arospatiale - Alli
5、age de nickel corroy au cuivre rsistant chaud NI-PD9001 (NiCu31) - Fil pour rivets - D 10 mm Luft- und Raumfahrt - Hochwarmfeste Nickellegierung mit Kupfer NI-PD9001 (NiCu31) - Nietdrhte - D 10 mm This European Standard was approved by CEN on 11 July 2008. CEN members are bound to comply with the CE
6、N/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 CEN Management Centre or
7、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 the same status as the official vers
8、ions. 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, Portugal, Romania, Slovakia, Slovenia, S
9、pain, Sweden, Switzerland and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG Management Centre: Avenue Marnix 17, B-1000 Brussels 2009 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national
10、 Members. Ref. No. EN 4372:2009: EBS EN 4372:2009EN 4372:2009 (E) 2 Foreword This document (EN 4372:2009) 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 Associati
11、on, 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 or by endorsement,
12、at the latest by August 2009, and conflicting national standards shall be withdrawn at the latest by August 2009. 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
13、 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, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungar
14、y, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. BS EN 4372:2009EN 4372:2009 (E) 3 Introduction This standard is part of the series of EN metallic material standard
15、s 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 requirements relating to: Heat resisting nickel alloy with copper NI-PD9001 (NiCu31) Wire for solid rivets
16、D 10 mm 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 amendments)
17、 applies. EN 2002-001, Aerospace series Metallic materials Test methods Part 001: Tensile testing at ambient temperature EN 2032-2, Aerospace series Metallic materials Part 2: Coding of metallurgical condition in delivery condition EN 4258, Aerospace series Metallic materials General organization of
18、 standardization Links between types of EN standards and their use EN 4500-3, Aerospace series Metallic materials Rules for drafting and presentation of material standards Part 3: Specific rules for heat resisting alloys 1) EN 4700-4, Aerospace series Steel and heat resisting alloys Wrought products
19、 Technical specification Part 4: Wire 1) ASTM B565, Standard test method for shear testing of aluminum and aluminum-alloy rivets and cold-heading wire and rods 2)1) Published as ASD Prestandard at the date of publication of this standard. 2) Published by: American Society for Testing and Materials (
20、ASTM), 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959, USA. BS EN 4372:2009EN 4372:2009 (E) 4 1 Material designation Nickel alloy with copper NI-PD9001 (NiCu31) 2 Chemical composition % Element Ni+Co aAl C Cu Fe Mn S Si Others Ni Each Total min. 63 28 1 0,3 Base max. 0,5 0,15 3
21、4 2,5 2,0 0,024 0,5 0,60 b3 Method of melting 4.1 Form Wire 4.2 Method of production Cold drawn 4.3 Limit dimension(s) mm D 10 mm 5 Technical specification EN 4700-4 6.1 Delivery condition Recrystallized annealed 4 h, 780 C, furnace cool combined with gas quench to 50 C, subsequent air cool cHeat tr
22、eatment 6.2 Delivery condition code U d7 Use condition Delivery condition Heat treatment Characteristics 8.1 Test sample(s) EN 2002-001 8.2 Test piece(s) EN 2002-001 8.3 Heat treatment 9 Dimensions concerned mm D 10 mm 10 Thickness of cladding on each face % 11 Direction of test piece L 12 T Tempera
23、ture C Ambient 13 Proof stress Rp0,2MPa 14 Strength RmMPa 530 Rm 620 15 Elongation A % A50 mm 25 16 Reduction of area Z % 17 Hardness 18 Shear strength RcMPa 340 Rc e19 Bending k 20 Impact strength 21 C Temperature C 22 Time h 23 Stress aMPa 24 Elongation a % 25 Rupture stress RMPa 26 Elongation at
24、rupture A % 27 Notes (see line 98) a, b, c, d, eBS EN 4372:2009EN 4372:2009 (E) 5 36 Reverse torsion test for wires See EN 4700-4. 7 D 8 mm; 10 turns in each way 43 Wrapping test for wires See EN 4700-4. 44 External defects See EN 4700-4. 1 Only visual is required 7 No cracks, laps, folds 95 Marking
25、 inspection See EN 4700-4. 96 Dimensional inspection See EN 4700-4. 98 Notes a Mass content of max. 1,0 % Co is allowed. b (Zn, Sn, Pb), Ti 0,6 where (Zn, Sn, Pb) 0,3 Ti 0,3. c Tolerance according to EN 4700-4. d See EN 2032-2. e Testing of shear strength according to ASTM B565. 99 Typical use BS EN
26、 4372:2009EN 4372:2009 (E) 6 100 Product qualification Qualification programme to be agreed between manufacturer and purchaser. BS EN 4372:2009This page has been intentionally left blankBS EN4372:2009BSI GroupHeadquarters 389Chiswick High Road,London, W4 4AL, UKTel +44 (0)20 8996 9001Fax +44 (0)20 8
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