1、BS EN 2116:2009ICS 49.025.20NO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBRITISH STANDARDAerospace series Aluminium alloy 2017A-T42 Wire for solid rivets D null 10 mmThis British Standardwas published underthe authority of theStandards Policy andStrategy Committee on 30Septe
2、mber 2009 BSI 2009ISBN 978 0 580 57868 7Amendments/corrigenda issued since publicationDate CommentsBS EN 2116:2009National forewordThis British Standard is the UK implementation of EN 2116:2009.The UK participation in its preparation was entrusted to TechnicalCommittee ACE/61/-/24, Light alloys.A li
3、st 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 confer immunityfrom legal o
4、bligations.BS EN 2116:2009EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 2116 February 2009 ICS 49.025.20 English Version Aerospace series - Aluminium alloy 2017A-T42 - Wire for solid rivets - D 10 mm Srie arospatiale - Alliage daluminium 2017A-T42 - Fils pour rivets pleins - D 10 mm Luft- und
5、 Raumfahrt - Aluminiumlegierung 2017A-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 Standard the status of a nation
6、al 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, German). A version in an
7、y 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, Czech Republic, Denmark, Es
8、tonia, 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 EUROPEN DE NORMALISATION EU
9、ROPISCHES 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 2116:2009: EBS EN 2116:2009EN 2116:2009 (E) 2 Foreword This document (EN 2116:2009) has been pre
10、pared 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 Services of the member count
11、ries 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 latest by August 2009. Atte
12、ntion 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 standards organizations of
13、 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, Portugal, Romania, Slov
14、akia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. BS EN 2116:2009EN 2116:2009 (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. This standard has been
15、prepared in accordance with EN 4500-2. 1 Scope This standard specifies the requirements relating to: Aluminium alloy 2017A-T42 Wire for solid rivets D 10 mm for aerospace applications. 2 Normative references The following referenced documents are indispensable for the application of this document. F
16、or 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 2070-6, Aerospace series Al
17、uminium 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 for drafting and present
18、ation 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)ASTM E112-96, Standard test methods for determining average grain size 3)1) Publi
19、shed as ASD Prestandard at the date of publication of this standard. 2) Published as ASD Technical Report at the date of publication of this standard. 3) Published by: American Society for Testing and Materials (ASTM), 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959 USA. BS EN 2
20、116:2009EN 2116:2009 (E) 4 1 Material designation Aluminium alloy 2017A-T42 2 Chemical composition % aElement Si Fe Cu Mn Mg Cr Zn Ti + Zr Others Al Each Total min. 0,20 3,5 0,40 0,40 Base max. 0,8 0,7 4,5 1,0 1,0 0,10 0,25 0,25 0,05 0,15 3 Method of melting 4.1 Form Wire 4.2 Method of production Co
21、ld drawn 4.3 Limit dimension(s) mm D 10 5 Technical specification EN 2070-6 6.1 Delivery condition H14 bHeat treatment 6.2 Delivery condition code F c7 Use condition T42 Heat treatment See line 29. Characteristics 8.1 Test sample(s) See EN 2070-6. 8.2 Test piece(s) See EN 2070-6. 8.3 Heat treatment
22、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 Rp0,2MPa 14 Strength RmMPa 210 Rm 310 400 15 Elongation A % 16 Reduction of area Z % 17 Har
23、dness 18 Shear strength RcMPa 260 Rc 290 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, b, cBS EN 2116:2009EN 2116:2009 (E) 5 29 Reference heat treatment Delivery condition +
24、(495 5) C = 30 min / WQ 40 C Quench delay = 10 s + = ambient / t 5 d 34 Grain size 1 ASTM E112-96 2 One sample per batch 4 Full cross-section taken transversely through the wire. 7 G 5 44 External defects See EN 2070-6. 95 Marking inspection See EN 2070-6. 96 Dimensional inspection See EN 2070-6. 1
25、Measuring equipment and procedures suitable 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 In accordance with Handbook from Aluminium Association International Alloy Designation and Co
26、mposition Limits and Wrought Aluminium and Wrought Aluminium Alloys. b Instead of H14 it is also acceptable to use either H13 or H15. c See EN 2032-2. 99 Typical use BS EN 2116:2009EN 2116:2009 (E) 6 100 Product qualification Qualifcation programe to be agred betwen manufacturer and purchaser. BS EN
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