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1、a Date: 30 March 2007 Origin: European Latest date for receipt of comments: 30 June 2007 Project no.: 2006/02936 Responsible committee: ACE/61/-/24 Light alloys Interested committees: ACE/61 Title: Draft BS EN 2116 Aerospace Series - Aluminium Alloy 2017A-T42 - wire for solid rivets D 10mm Supersess
2、ion information: If this document is published as a standard, the UK implementation of it will supersede NONE and partially supersede NONE . If you are aware of a current national standard which may be affected, please notify the secretary (contact details below). WARNING: THIS IS A DRAFT AND MUST N
3、OT BE REGARDED OR USED AS A BRITISH STANDARD. THIS DRAFT IS NOT CURRENT BEYOND 30 June 2007. This draft is issued to allow comments from interested parties; all comments will be given consideration prior to publication. No acknowledgement will normally be sent. See overleaf for information on commen
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7、ement International or European publications referred to in this draft may be found via the British Standards Online Service on the BSI web site http:/www.bsi-. Direct tel: 020 8996 7792 Responsible Committee Secretary: Mrs Sara Ansari (BSI) E-mail: sara.ansaribsi- Draft for Public Comment Head Offi
8、ce 389 Chiswick High Road London W4 4AL Telephone: +44(0)20 8996 9000 Fax: +44(0)20 8996 7001 Form 36 Version 7.0 DPC: 07/30157997 DC Licensed Copy: London South Bank University, London South Bank University, Mon May 07 12:39:35 GMT+00:00 2007, Uncontrolled Copy, (c) BSI b Introduction This draft st
9、andard is based on European discussions in which the UK took an active part. Your comments on this draft are welcome and will assist in the preparation of the consequent British Standard. If no comments are received to the contrary, then the UK will approve this draft and implement it as a British S
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15、e/ Note (e.g. Table 1) Type of com- ment Comment (justification for change) by the MB Proposed change by the MB Secretariat observations on each comment submitted 3.1 Definition 1 ed Definition is ambiguous and needs clarifying. Amend to read . so that the mains connector to which no connection . 6.
16、4 Paragraph 2 te The use of the UV photometer as an alternative cannot be supported as serious problems have been encountered in its use in the UK. Delete reference to UV photometer. Microsoft and MS-DOS are registered trademarks, and Windows is a trademark of Microsoft Corporation. Licensed Copy: L
17、ondon South Bank University, London South Bank University, Mon May 07 12:39:35 GMT+00:00 2007, Uncontrolled Copy, (c) BSI DRAFT prEN2116 Date : 05.12.06 Edition : P1 STUDY: DRAFT N : 11 STAGE : Ref. : Superseding Ref. : ENGLISH VERSION Aerospace series Aluminium alloy 2017A T42 wire for solid rivets
18、 D 10 mm Srie Arospatiale Alliage daluminium 2017A T42 fils pour rivets pleins D 10 mm Luft- und Raumfahrt Aluminiumlegierung 2017A T42 Nietdrhte fr Vollniete D 10 mm Master document : en fr de Sponsor : AIRBUS INDUSTRIE TF3/WG1 THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES - STANDARDIZATION Gull
19、edelle 94, B - 1200 Bruxelles Tel. : (32) 2 775 8110 Fax. : (32) 2 775 8111 Licensed Copy: London South Bank University, London South Bank University, Mon May 07 12:39:35 GMT+00:00 2007, Uncontrolled Copy, (c) BSI Page 2 prEN 2116 : 10/2006 Blank page Licensed Copy: London South Bank University, Lon
20、don South Bank University, Mon May 07 12:39:35 GMT+00:00 2007, Uncontrolled Copy, (c) BSI Page 3 prEN 2116 : 10/06 0 Introduction This standard is part of the series of EN metallic material standards for aerospace applications. The general organisation of this series is described in EN4258. This sta
21、ndard has been prepared in accordance with EN 4500-2. 1 Scope This specification defines 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 o
22、f 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 2070-6 Aerospace series Aluminium and aluminium alloy wrought products Technical Specification Part 2 Rivet wire EN 4258
23、 Aerospace series Metallic materials General organisation of standardization Links between types of EN standards and their use EN 4500-2 Aerospace series Metallic materials Rules for drafting and presentation of material standards Part 2: Specific rules for aluminium, aluminium alloys and magnesium
24、alloys1) EN 2032-2 Aerospace series Metallic materials Part 2: Coding of metallurgical condition in delivery condition ASTM E 112-96 Standard Test Methods for Determining Average Grain Size _ 1) Published as ASD-STAN Prestandard at the date of publication of this standard. Licensed Copy: London Sout
25、h Bank University, London South Bank University, Mon May 07 12:39:35 GMT+00:00 2007, Uncontrolled Copy, (c) BSI Page 4 prEN 2116 : 10/2006 1 Material designation Aluminium alloy 2017A-T42 others Element Si Fe Cu Mn Mg Cr Zn Ti + Zr each total Al min. 0,20- 3,5 0,400,40- - - - - 2 Chemical compositio
26、n %2) max. 0,8 0,7 4,5 1,0 0,8 0,100,25 0,25 0,05 0,15 Base 3 Method of melting - 4.1 Form Wire 4.2 Method of production Cold drawn 4.3 Limit dimension (mm) D 10 mm 5 Technical specification EN 2070-6 6.1 Delivery condition H143) 6.2 Delivery condition code4)F Use condition T42 7 heat treatment See
27、line 29 Characteristics 8.1 Test sample See EN2070-6 8.2 Test piece See EN2070-6 8.3 Heat treatment Delivery condition see line 6.1 Use condition T42 (see line 29) 9 Dimensions concerned D mm D 10 10 Thickness of cladding on each face % - 11 Direction of test piece L 12 Temperature - C Ambient 13 Pr
28、oof stress Rp0,2MPa - 14 Strength RmMPa 210 Rm 310 400 15 Elongation A50% - 16 T Reduction of area Z % - 17 Hardness HB - - 18 Shear strength RcMPa - 260 Rc 290 19 Bending k - - 20 Impact strength - 21 Temperature - C - 22 Time t h - 23 Stress aMPa - 24 Elongation a % - 25 Rupture stress RMPa - 26 C
29、 Elongation at rupture A % - 27 Notes (see line 98) 2) 3) 4) Licensed Copy: London South Bank University, London South Bank University, Mon May 07 12:39:35 GMT+00:00 2007, Uncontrolled Copy, (c) BSI Page 5 prEN 2116 : 10/06 29 Reference heat treatment - Delivery condition T42 see line 6.1 + (495 5)
30、C 30 min / WQ 40 C + ageing / t 5 d (120 h) Quench delay 10 s 1 ASTM E 112-96 2 - 5 - 34 Grain size 7 G 5 98 Notes - 2) In according with Handbook from Aluminium Association International Alloy Designation and Composition Limits and Wrought Aluminium and Wrought Aluminium Alloys. 3) Instead H14 it is also acceptable to use either H13 or H15. 4) See EN2032-2. 100 Typical use - - Licensed Copy: London South Bank University, London South Bank University, Mon May 07 12:39:35 GMT+00:00 2007, Uncontrolled Copy, (c) BSI