EN 3114-003-2006 en Aerospace series - Test method - Microstructure of ( + ) titanium alloy wrought products - Part 003 Microstructure of plate《航空航天系列的试验方法 (α+β)钛合金锻制品的微观结构 第003部分 .pdf
《EN 3114-003-2006 en Aerospace series - Test method - Microstructure of ( + ) titanium alloy wrought products - Part 003 Microstructure of plate《航空航天系列的试验方法 (α+β)钛合金锻制品的微观结构 第003部分 .pdf》由会员分享,可在线阅读,更多相关《EN 3114-003-2006 en Aerospace series - Test method - Microstructure of ( + ) titanium alloy wrought products - Part 003 Microstructure of plate《航空航天系列的试验方法 (α+β)钛合金锻制品的微观结构 第003部分 .pdf(28页珍藏版)》请在麦多课文档分享上搜索。
1、BRITISH STANDARD BS EN 3114-003:2006 Aerospace series Test method Microstructure of ( ! + “) titanium alloy wrought products Part 003: Microstructure of plate The European Standard EN 3114-003:2006 has the status of a British Standard ICS 49.025.30 BS EN 3114-003:2006 This British Standard was publi
2、shed under the authority of the Standards Policy and Strategy Committee on 31 January 2007 BSI 2007 ISBN 978 0 580 50079 4 National foreword This British Standard was published by BSI. It is the UK implementation of EN 3114-003:2006. The UK participation in its preparation was entrusted by Technical
3、 Committee ACE/61, Metallic materials for aerospace purposes, to Panel ACE/61/-/49, Titanium and its alloys. A list of organizations represented on ACE/61/-/49 can be obtained on request to its secretary. This publication does not purport to include all the necessary provisions of a contract. Users
4、are responsible for its correct application. Compliance with a British Standard cannot confer immunity from legal obligations. Amendments issued since publication Amd. No. Date Comments EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 3114-003 December 2006 ICS 49.025.30 English Version Aerospac
5、e series - Test method - Microstructure of ( + ) titanium alloy wrought products - Part 003: Microstructure of plate Srie arospatiale - Mthode dessai - Microstructure des produits corroys en alliage de titane ( + ) - Partie 003 : Microstructure des plaques Luft- und Raumfahrt - Prfverfahren - Mikrog
6、efge Kneterzeugnisse von Titanlegierung ( + ) - Teil 003: Mikrogefge von Platten This European Standard was approved by CEN on 18 October 2006. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standard the status of a n
7、ational standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the Central Secretariat or to any CEN member. This European Standard exists in three official versions (English, French, German). A version in
8、 any other language made by translation under the responsibility of a CEN member into its own language and notified to the Central Secretariat has the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Fi
9、nland, 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 STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES
10、 KOMITEE FR NORMUNG Management Centre: rue de Stassart, 36 B-1050 Brussels 2006 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 3114-003:2006: E2 Contents Page Foreword3 1 Scope4 2 Normative references4 3 Micrographs.4 EN 3114-003:
11、20063 Foreword This document (EN 3114-003:2006) 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 Nationa
12、l Associations 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 June 2007, and conflicting national stand
13、ards shall be withdrawn at the latest by June 2007. 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 Inter
14、nal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Nether
15、lands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. EN 3114-003:20064 1 Scope This standard contains pictures of the microstructure of ( + ) titanium alloy plate. It shall be used in conjunction with EN 3114-001. 2 Normative references The
16、 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 3114-001, Aerospace series Microstructure of ( +
17、) titanium alloy wrought products Part 00 1: General requirements. 3 Micrographs See Table 1. Table 1 Photo micrograph No. Description 3T1 to 3T38 ( + ) structure, globular/lamellar, transverse section LT-ST. 3T100 to 3T106 ( + ) structure, with local blocky and stringers, transverse section LT-ST.
18、3A1 to 3A8 ( + ) structure, with lean areas. 3T200 to 3T202 transformed structure, transverse section LT-ST. EN 3114-003:20065 ( + + + + ) structure, globular/lamellar, transverse section LT-ST 100 : 1 500 : 1 3T1 100 : 1 500 : 1 3T2 100 : 1 500 : 1 3T3 EN 3114-003:20066 ( + + + + ) structure, globu
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