1、BS EN 2117:2009ICS 49.025.20NO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBRITISH STANDARDAerospace series Aluminium alloy ALP5056A (5056A)-H32 Wire for solid rivets D null 10 mmThis British Standardwas published underthe authority of theStandards Policy andStrategy Committee
2、 on 30September 2009 BSI 2009ISBN 978 0 580 57869 4Amendments/corrigenda issued since publicationDate CommentsBS EN 2117:2009National forewordThis British Standard is the UK implementation of EN 2117:2009.The UK participation in its preparation was entrusted to TechnicalCommittee ACE/61/-/24, Light
3、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 Standard cannot confer immunityf
4、rom legal obligations.BS EN 2117:2009EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 2117 February 2009 ICS 49.025.20 English Version Aerospace series - Aluminium alloy AL-P5056A (5056A)-H32 - Wire for solid rivets - D 10 mm Srie arospatiale - Alliage daluminium AL-P5056A (5056A)-H32 - Fils pou
5、r rivets pleins - D 10 mm Luft- und Raumfahrt - Aluminiumlegierung AL-P5056A (5056A)-H32 - 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 givin
6、g 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 to any CEN member. This European Standard exists in three official vers
7、ions (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 versions. CEN members are the national standards bodies of Austria, Belgium
8、, 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, Spain, Sweden, Switzerland and United Kingdom. EUROPEAN COMMITTEE FOR ST
9、ANDARDIZATION 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 Members. Ref. No. EN 2117:2009: EBS EN 2117:2009EN 2117:2009 (E) 2 For
10、eword This document (EN 2117:2009) 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 Association
11、s 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, at the latest by August 2009, and conflicting national standards shall
12、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 or all such patent rights. According to the CEN/CENELEC Internal Regul
13、ations, 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, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Nethe
14、rlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. BS EN 2117:2009EN 2117:2009 (E) 3 Introduction This standard is part of the series of EN metallic material standards for aerospace applications. The general organization of this series i
15、s described in EN 4258. This standard has been prepared in accordance with EN 4500-2. 1 Scope This standard specifies the requirements relating to: Aluminium alloy AL-P5056A (5056A)-H32 Wire for solid rivets D 10 mm for aerospace applications. 2 Normative references The following referenced document
16、s 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) applies. EN 2032-2, Aerospace series Metallic materials Part 2: Coding of metallurgical con
17、dition in delivery condition EN 2070-6, 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, Aerospa
18、ce series Metallic materials Rules 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 Pr
19、estandard at the date of publication of this standard. 2) Published as ASD Technical Report at the date of publication of this standard. BS EN 2117:2009EN 2117:2009 (E) 4 1 Material designation Aluminium alloy AL-P5056A (5056A)-H32 a2 Chemical composition % Element Si Fe Cu Mn Mg Cr Zn Ti Cr + Mn Ot
20、hers Al Each Total min. 0,10 4,50 0,10 Base max. 0,40 0,50 0,10 0,60 5,60 0,20 0,20 0,20 0,60 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 H32 Heat treatment 6.2 Delivery cond
21、ition code Ub7 Use condition H32 Heat treatment Delivery condition Characteristics 8.1 Test sample(s) See EN 2070-6. 8.2 Test piece(s) See EN 2070-6. 8.3 Heat treatment 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 P
22、roof stress Rp0,2MPa 14 Strength RmMPa 280 Rm 360 15 Elongation A % 16 Reduction of area Z % 17 Hardness 18 Shear strength RcMPa 170 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
23、) a, bBS EN 2117:2009EN 2117:2009 (E) 5 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 for the tolerances shall be used. 7 Dimensions and tolerances shall conform to the requirements of th
24、e order or the relevant standard given in TR 2410. 98 Notes a The material designation of AL-P5056A (5056A) is per Aluminium Association (AA) is 5019. b See EN 2032-2. 99 Typical use BS EN 2117:2009EN 2117:2009 (E) 6 100 Product qualification Qualifcation programe to be agred betwen manufacturer and
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