EN 2115-2009 en Aerospace series - Aluminium alloy 2117-T42 - Wire for solid rivets - D less than or equal to 10 mm《航空航天系列 铝合金2117-T42 实心铆钉用线材 D≤10 mm》.pdf

1、BS EN 2115:2009ICS 49.025.20NO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBRITISH STANDARDAerospace series Aluminium alloy 2117-T42 Wire for solid rivets D null 10 mmThis British Standardwas published underthe authority of theStandards Policy andStrategy Committee on 30Septem

2、ber 2009 BSI 2009ISBN 978 0 580 57867 0Amendments/corrigenda issued since publicationDate CommentsBS EN 2115:2009National forewordThis British Standard is the UK implementation of EN 2115:2009.The UK participation in its preparation was entrusted to TechnicalCommittee ACE/61/-/24, Metallic materials

3、 for aerospace purposes.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 Standard cannot

4、 confer immunityfrom legal obligations.BS EN 2115:2009EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 2115 February 2009 ICS 49.025.20 English Version Aerospace series - Aluminium alloy 2117-T42 - Wire for solid rivets - D 10 mm Srie arospatiale - Alliage daluminium 2117-T42 - Fils pour rivets

5、pleins - D 10 mm Luft- und Raumfahrt - Aluminiumlegierung 2117-T42 - Nietdrhte fr Vollniete - D 10 mm This European Standard was approved by CEN on 16 August 2008. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standa

6、rd 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 official versions (English, French,

7、 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, Belgium, Bulgaria, Cyprus, Cz

8、ech 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 COMMITTEE FOR STANDARDIZATION COMIT EU

9、ROPEN 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 Members. Ref. No. EN 2115:2009: EBS EN 2115:2009EN 2115:2009 (E) 2 Foreword This document (E

10、N 2115:2009) 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 Association, this Standard has received the approval of the National Associations and the Official Ser

11、vices 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 August 2009, and conflicting national standards shall be withdrawn at the la

12、test 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 or all such patent rights. According to the CEN/CENELEC Internal Regulations, the national s

13、tandards 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, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland

14、, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. BS EN 2115:2009EN 2115:2009 (E) 3 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

15、. This standard has been prepared in accordance with EN 4500-2. 1 Scope This standard specifies the requirements relating to: Aluminium alloy 2117-T42 Wire for solid rivets D 10 mm for aerospace applications. 2 Normative references The following referenced documents are indispensable for the applica

16、tion 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 2032-2, Aerospace series Metallic materials Part 2: Coding of metallurgical condition in delivery condition EN 207

17、0-6, Aerospace series Aluminium and aluminium alloy wrought products Technical specification Part 6: Rivet wire EN 4258, Aerospace series Metallic materials General organization of standardization Links between types of EN standards and their use EN 4500-2, Aerospace series Metallic materials Rules

18、for drafting and presentation of material standards Part 2: Specific rules for aluminium, aluminium alloys and magnesium alloys 1)TR 2410, Aerospace series Metallic materials Relationship between dimensional standards and material standards 2)1) Published as ASD Prestandard at the date of publicatio

19、n of this standard. 2) Published as ASD Technical Report at the date of publication of this standard. BS EN 2115:2009EN 2115:2009 (E) 4 1 Material designation Aluminium alloy 2117-T42 2 Chemical composition % Element Si Fe Cu Mn Mg Cr Zn Others Al Each Total min. 2,2 0,20 Base max. 0,8 0,7 3,0 0,20

20、0,50 0,10 0,25 0,05 0,15 3 Method of melting 4.1 Form Wire 4.2 Method of production Cold drawn 4.3 Limit dimension(s) mm D 10 5 Technical specification EN 2070-6 6.1 Delivery condition H14 aHeat treatment 6.2 Delivery condition code F b7 Use condition T42 Heat treatment See line 29. Characteristics

21、8.1 Test sample(s) See EN 2070-6. 8.2 Test piece(s) See EN 2070-6. 8.3 Heat treatment Delivery condition (see line 6.1) Use condition T42 (see line 29) 9 Dimensions concerned mm D 10 10 Thickness of cladding on each face % 11 Direction of test piece L 12 T Temperature C Ambient 13 Proof stress Rp0,2

22、MPa 14 Strength RmMPa 175 Rm 245 15 Elongation A % 16 Reduction of area Z % 17 Hardness 18 Shear strength RcMPa 195 19 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 rupture A % 27 Notes (see line 98) a, bBS EN 2115:

23、2009EN 2115:2009 (E) 5 29 Reference heat treatment Delivery condition + (495 5) C = 30 min / WQ 40 C Quench delay = 10 s + = ambient / t 5 d 44 External defects See EN 2070-6. 95 Marking inspection See EN 2070-6. 96 Dimensional inspection See EN 2070-6. 1 Measuring equipment and procedures suitable

24、for the tolerances shall be used. 7 Dimensions and tolerances shall conform to the requirements of the order or the relevant standard given in TR 2410. 98 Notes a Instead of H14 it is also acceptable to use either H13 or H15. b See EN 2032-2. 99 Typical use BS EN 2115:2009EN 2115:2009 (E) 6 100 Prod

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