1、ASD-STAN STANDARD NORME ASD-STAN ASD-STAN NORM prEN 3813 Edition P 2 June 2010 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATIONAvenue de Tervuren, 270 - B-1150 Brussels - Tel. 32 2 775 8126 - Fax. 32 2 775 8131 - www.asd-stan.orgICS: Supersedes Edition P 1 of
2、 April 2002 Descriptors: ENGLISH VERSION Aerospace series Titanium alloy TI-P64001 (Ti-6Al-4V) Annealed Bar and wire for forged fasteners De 50 mm Srie arospatiale Alliage de titane TI-P64001 (Ti-6Al-4V) Recuit Barre et fil pour lments de fixations forges De 50 mm Luft- und Raumfahrt Titanlegierung
3、TI-P64001(Ti-6Al-4V) Geglht Stangen und Drhte zum Warmstauchschmied fr Verbindungselemente De 50 mm This “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
4、 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 Prestandard, the technical content shall not be changed to an extent that interchangeability is affected, physically or functi
5、onally, 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 (prEN) to CEN (European Committee for Standardization) for formal vote and transformation to full European Standard (EN). The C
6、EN 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 with the EN. Edition approved for publication 30 June 2010 Comments should be sent within six months after the date of publicat
7、ion to ASD-STAN Metallic Material Domain Copyright 2010 by ASD-STAN prEN 3813:2010 (E) 2 White page prEN 3813:2010 (E) 3 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. Thi
8、s standard has been prepared in accordance with EN 4500-4. 1 Scope This standard specifies the requirements relating to: Titanium alloy TI-P64001 (Ti-6Al-4V) Annealed Bar and wire for forged fasteners De 50 mm for aerospace applications. 2 Normative references The following referenced documents are
9、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 condition
10、 in delivery condition EN 3114-002, Aerospace series Test method Microstructure of ( ) titanium alloy wrought products Part 002: Microstructure of bars, sections, forging stock and forgings EN 4050-4, Aerospace series Test method for metallic materials Ultrasonic inspection of bars, plates, forging
11、stock and forgings Part 4: Acceptance criteria 1)EN 4258, Aerospace series Metallic materials General organization of standardization Links between types of EN standards and their useEN 4500-4, Aerospace series Metallic materials Rules for drafting and presentation of material standards Part 4: Spec
12、ific rules for titanium and titanium alloys 1) EN 4800-004, Aerospace series Titanium and titanium alloys Technical specification Part 004: Wire 1)1) Published as ASD-STAN Standard at the date of publication of this standard by Aerospace and Defence Industries Association of Europe-Standardization (
13、ASD-STAN), (www.asd-stan.org). prEN 3813:2010 (E) 4 1 Material designation Titanium alloy TI-P64001 (Ti-6Al-4V) Others Element Al V O N H Fe C Y Each Total Ti min. 5,50 3,50 2 Chemical composition % max. 6,75 4,50 0,20 0,03 0,0080 0,30 0,08 0,0050 0,10 0,40 Base 3 Method of melting See EN 4800-004.
14、4.1 Form Bar and wire 4.2 Method of production Wrought 4.3 Limit dimension(s) mm De 50 5 Technical specification EN 4800-004 Delivery condition Annealed 6.1 Heat treatment 700 C 790 C / 1 h t 2 h / AC in inert atmosphere 6.2 Delivery condition code U aUse condition Delivery condition 7 Heat treatmen
15、t Characteristics 8.1 Test sample(s) See EN 4800-004. Location for test sample b8.2 Test piece(s) See EN 4800-004. 8.3 Heat treatment Use condition See line 29. 9 Dimensions concerned mm De 50 De25 mm, location of test specimen shall be the mid-radius. 99 Typical use Forged fasteners prEN 3813:2010 (E) 6 100 Product qualification Qualification programme to be agreed between manufacturer and purchaser.
