ASD-STAN PREN 3114-3-1997 Aerospace Series Test Method Microstructure of (a + b) Titanium Alloy Wrought Products Part 3 Microstructure of Plate (Edition P 1)《航空航天系列 (a+b)钛合金锻件的显微结构.pdf
《ASD-STAN PREN 3114-3-1997 Aerospace Series Test Method Microstructure of (a + b) Titanium Alloy Wrought Products Part 3 Microstructure of Plate (Edition P 1)《航空航天系列 (a+b)钛合金锻件的显微结构.pdf》由会员分享,可在线阅读,更多相关《ASD-STAN PREN 3114-3-1997 Aerospace Series Test Method Microstructure of (a + b) Titanium Alloy Wrought Products Part 3 Microstructure of Plate (Edition P 1)《航空航天系列 (a+b)钛合金锻件的显微结构.pdf(22页珍藏版)》请在麦多课文档分享上搜索。
1、 STD-AECMA PREN 3LLq-l-ENGL 1997 LOL23LL CIDL3115 207 AECMA STANDARD prEN 31 14-3 NORME AECMA Edition P 1 AECMA NORM July 1997 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA) Gulledelle 94 - B-1200 BRUXELLES - Tel. (+32) 2 775 81 1 O - Fax. (+32) 2 775 81 11 ICs : Descriptors :
2、 ENGLISH VERSION Aerospace series Test method Microstructure of (a + ) titanium alloy wrought products Part 3 : Microstructure of plate Srie arospatiale Mthode dessai Microstructure des produits corroys en alliage de titane (a + ) Partie 3 : Microstructure des plaques Luft- und Raumfahrt Prfverfahre
3、n Mikrogefge von Titanlegierung (a + ) Teil 3 : Mikrogefge Kneterzeugnisse von Platten This “Aerospace Series Prestandard has been drawn up under the responsibility of AECMA (The European Association of Aerospace Industries). It is published on green paper for the needs of AECMA-Members. It has been
4、 technically approved by the experts of the concerned Technical Committee following comment by the Member countries. 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-
5、identification of the standard. After examination and signature of the AECMA Standard Checking Centre INPSI and formal agreement of the Official Services of the Member countries it will be submitted as a draft European Standard to CEN (European Committee for Standardization) for formal vote. NOTE :
6、Images of higher quality for the prints in this standard are available from BNAE. Nota - Extra copies can be supplied by B.N.A.E. - Technopolis 54 - 199, rue Jean-Jacques Rousseau - 921 38 ICCY-LEC-MOULINEAUX CEDEX I C5 Chairman Comments should be sent within six months after the date of publication
7、 to I I Edition approved for publication 1997-07-31 AECMA Gulledelle 94 I B-1200 BRUXELLES Mr Odorico aecma 1997 1 Scope This standard contains pictures of the microstructure of (a +) titanium alloy plate. It shall be used in conjunction with EN 31 14-1. 2 Normative references This European Standard
8、 incorporates by dated or undated reference provisions from other publications. These normative references are cited at the appropriate places in the text and the publications are listed hereafter. For dated references, subsequent amendments to or revisions of any of these publications apply to this
9、 European Standard only when incorporated in it by amendment or revision. For undated references the latest edition of the publication referred to applies. EN 3114-1 Aerospace series - Microstructure of (a + ) titanium alloy wrought products - Part 1 : General requirements 1) 3 Micrographs Photo mic
10、rograph no 3T1 to 3T38 3T1 O0 to 3T106 3A1 to 3A8 3T200 to 3T202 Description (a + ) structure globular/lamellar, transverse section LT-ST (a + ) structure, with local blocky a and CI stringers, transverse section LT-ST. (a + ) structure, with lean a areas. transformed structure, transverse section L
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