1、ASD STANDARD NORME ASD ASD NORM prEN 2117 Edition P 1 October 2007 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATIONAvenue de Tervuren, 270 - B-1150 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 763 3565 - www.asd-stan.orgICS: Descriptors: ENGLISH VERSION Aero
2、space series Aluminium alloy AL-P5056A (5056A)-H32 Wire for solid rivets D 10 mm Srie arospatiale Alliage daluminium AL-P5056A (5056A)-H32 Fils pour rivets pleins D 10 mm Luft- und Raumfahrt Aluminiumlegierung AL-P5056A (5056A)-H32 Nietdrhte fr Vollniete D 10 mm This “Aerospace Series“ Prestandard h
3、as been drawn up under the responsibility of ASD-STAN (The AeroSpace and Defence Industries Association of Europe - Standardization). It is published for the needs of the European Aerospace Industry. It has been technically approved by the experts of the concerned Domain following member comments. S
4、ubsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that interchangeability is affected, physically or functionally, without re-identification of the standard. After examination and review by users and formal agreement of ASD-STAN, it will be sub
5、mitted as a draft European Standard (prEN) to CEN (European Committee for Standardization) for formal vote and transformation to full European Standard (EN). The CEN national members have then to implement the EN at national level by giving the EN the status of a national standard and by withdrawing
6、 any national standards conflicting with the EN. Edition approved for publication 31 October 2007 Comments should be sent within six months after the date of publication to ASD-STAN Metallic Material Domain Copyright 2007 by ASD-STAN prEN 2117:20072 Foreword This standard was reviewed by the Domain
7、Technical Coordinator of ASD-STANs Metallic Material Domain. After inquiries and votes carried out in accordance with the rules of ASD-STAN defined in ASD-STANs General Process Manual, this standard has received approval for Publication. prEN 2117:20073 Introduction This standard is part of the seri
8、es of EN metallic material standards for aerospace applications. The general organisation of this series is 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
9、 solid rivets 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 a
10、ny amendments) applies. EN 2032-2, Aerospace series Metallic materials Part 2: Coding of metallurgical condition 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
11、General organization 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 alloys. 1)1) Published as ASD Prest
12、andard at the date of publication of this standard.prEN 2117:20074 1 Material designation Aluminium alloy AL-P5056A (5056A)-H32 a2 Others Element Si Fe Cu Mn Mg Cr Zn Ti Cr + Mn Each Total Al min. 0,10 4,50 0,10 Chemical composition % max. 0,40 0,50 0,10 0,60 5,60 0,20 0,20 0,20 0,60 0,05 0,15 Base
13、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 Delivery condition H32 6.1 Heat treatment 6.2 Delivery condition code UbUse condition H32 7 Heat treatment Delivery condition Characteristics 8.1 Test sample(s) Se
14、e 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 Temperature C Ambient 13 Proof stress Rp0,2MPa 14 Strength RmMPa 280 Rm 360 15 Elongation A % 16 T Reduction of area Z % 17 Hardness
15、 18 Shear strength RcMPa 170 19 Bending k 20 Impact strength 21 Temperature C 22 Time h 23 Stress aMPa 24 Elongation a % 25 Rupture stress RMPa 26 C Elongation at rupture A % 27 Notes (see line 98) a, bprEN 2117:20075 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 prEN 2117:20076 100 Product qualification Qualification programme to be agreed between manufacturer and purchaser.
