1、ASD STANDARD NORME ASD ASD NORM prEN 2115 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 2117-T42 Wire for solid rivets D 10 mm Srie arospatiale Alliage daluminium 2117-T42 Fils pour rivets pleins D 10 mm Luft- und Raumfahrt Aluminiumlegierung 2117-T42 Nietdrhte fr Vollniete D 10 mm This “Aerospace Series“ Prestandard has been drawn up under the responsibili
3、ty 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. Subsequent to the publication of this Pr
4、estandard, 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 submitted as a draft European Standard (pr
5、EN) 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 any national standards conflicting wit
6、h 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 2115:20072 Foreword This standard was reviewed by the Domain Technical Coordinator of ASD-STANs Meta
7、llic 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 2115:20073 Introduction This standard is part of the series of EN metallic material standards fo
8、r aerospace applications. The general organization 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 2117-T42 Wire for solid rivets D 10 mm for aerospace applications. 2
9、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 any amendments) applies. EN 2032-2, Aerospace series
10、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 General organization of standardization Links betwee
11、n 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 Prestandard at the date of publication of this standard.p
12、rEN 2115:20074 1 Material designation Aluminium alloy 2117-T42 Others Element Si Fe Cu Mn Mg Cr Zn Each Total Al min. 2,2 0,20 2 Chemical composition % max. 0,8 0,7 3,0 0,20 0,50 0,10 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(s) mm
13、D 10 5 Technical specification EN 2070-6 Delivery condition H14 a6.1 Heat treatment 6.2 Delivery condition code F bUse condition T42 7 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 Delivery condition (see line 6.1) U
14、se 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 Temperature C Ambient 13 Proof stress Rp0,2MPa 14 Strength RmMPa 175 Rm 245 15 Elongation A % 16 T Reduction of area Z % 17 Hardness 18 Shear strength RcMPa 195 19 Be
15、nding 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 2115:20075 29 Reference heat treatment Delivery condition + (495 5) C 30 min / WQ 40 C + ageing / t 5 d (120 h) Quench delay 10 s 98 Notes a Instead H14 it is also acceptable to use either H13 or H15. b See EN 2032-2. 99 Typical use prEN 2115:20076 100 Product qualification Qualification programme to be agreed between manufacturer and purchaser.
