1、ASD STANDARD NORME ASD ASD NORM prEN 2573 Edition P 2 October 2006 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATION Gulledelle 94 - B-1200 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 763 3565 - www.asd-stan.orgICS: Supersedes issue P 1 April 1986 Descriptor
2、s: ENGLISH VERSION Aerospace series Steel FE-PA3601 (X6CrNiTi18-10) Softened Rm 780 MPa Wire 0,25 mm De 3 mm Srie arospatiale Acier FE-PA3601 (X6CrNiTi18-10) Adouci Rm 780 MPa Fils 0,25 mm De 3 mm Luft- und Raumfahrt Stahl FE-PA3601 (X6CrNiTi18-10) Weichgeglht Rm 780 MPa Drhte 0,25 mm De 3 mm This “
3、Aerospace Series“ Prestandard has 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 Doma
4、in following member comments. Subsequent 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 agreem
5、ent of ASD-STAN, it will be submitted 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 natio
6、nal standard and by withdrawing any national standards conflicting with the EN. Edition approved for publication 31 October 2006 Comments should be sent within six months after the date of publication to ASD-STAN Metallic Material Domain Copyright 2006 by ASD-STAN Copyright Association Europeene des
7、 Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 2573:20062 Foreword This standard was reviewed by the Domain Technical Coordinator of ASD-STANs Metallic Material Domain. After inqu
8、iries 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. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo r
9、eproduction or networking permitted without license from IHS-,-,-prEN 2573:20063 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 prepared in accordan
10、ce with EN 4500-5. 1 Scope This standard specifies the requirements relating to: Steel FE-PA3601 (X6CrNiTi18-10) Softened Rm 780 MPa Wire 0,25 mm De 3 mm for aerospace applications. 2 Normative references The following referenced documents are indispensable for the application of this document. For
11、dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 4258, Aerospace series Metallic materials General organization of standardization Links between types of EN standards and their use. EN 4500-
12、5, Aerospace series Metallic materials Rules for drafting and presentation of material standards Part 5: Specific rules for steels. 1) EN 4700-4, Aerospace series Steel and heat resisting alloys Wrought products Technical specification Part 4: Wire.1) 1) Published as ASD Prestandard at the date of p
13、ublication of this standard. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 2573:20064 1 Material designation Steel FE-PA3601 (X6CrNiTi18-10) El
14、ement C Si Mn S P Cr Ni Ti Fe min. 17 9 5 x C 2 Chemical composition % max. 0,08 1 2 0,030 0,045 19 12 0,70 Base 3 Method of melting Air melted 4.1 Form Wire 4.2 Method of production Drawn 4.3 Limit dimension(s) mm 0,25 De 3 5 Technical specification EN 4700-4 Delivery condition Softened 6.1 Heat tr
15、eatment 1 050 C q 1 100 C AC or WQ 6.2 Delivery condition code U Use condition Delivery condition 7 Heat treatment Characteristics 8.1 Test sample(s) See EN 4700-4. 8.2 Test piece(s) See EN 4700-4. 8.3 Heat treatment Delivery condition 9 Dimensions concerned mm 0,25 De 3 10 Thickness of cladding on
16、each face % 11 Direction of test piece L 12 Temperature q C Ambient 13 Proof stress Rp0,2MPa 14 Strength RmMPa 780 15 T Elongation A % 40 16 Reduction of area Z % 17 Hardness 18 Shear strength RcMPa 19 Bending k 20 Impact strength 21 Temperature q C 22 Time h 23 Stress aMPa 24 Elongation a % 25 Rupt
17、ure stress RMPa 26 C Elongation at rupture A % 27 Notes (see line 98) Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 2573:20065 37 Reverse bend
18、EN 4700-4 7 9 bend minimum 95 Marking inspection See EN 4700-4. 96 Dimensional inspection See EN 4700-4. 98 Notes Maximum temperature using: 600 C 99 Typical use Locking wire Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for Re
19、saleNo reproduction or networking permitted without license from IHS-,-,-prEN 2573:20066 100 Product qualification See EN 4700-4. Qualification programme to be agreed between manufacturer and purchaser. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-
