AECMA PREN 3114-2-1997 Aerospace Series Test Method Microstructure (a + b) Titanium Alloy Wrought Products Part 2 Microstructure of Bars Sections Forging Stock and Forgings Edition.pdf
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1、STD*AECMA PREN 3114-2-ENGL 1777 9 1012311 0013075 by7 Edition approved for publication AECMA STANDARD NORME AECMA AECMA NORM Comments should be sent within six months after the date of publication to C5 Chairman prEN 31 14-2 Edition P 1 July 1997 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE IN
2、DUSTRIES (AECMA) Guiledelle 94 - B-1200 BRUXELLES - Tel. (+32) 2 775 81 1 O - Fax. (+32) 2 775 81 11 ICs : Descriptors : ENGLISH VERSION Aerospace series Test method Microstructure of (a + ) titanium alloy wrought products Part 2 : Microstructure of bars, sections, forging stock and forgings Srie ar
3、ospatiale Luft- und Raumfahrt Mthode dessai Prfverfahren Microstructure des produits corroys en alliage de titane (o1 + ) Partie 2 : Microstructure des barres, des profils, des produits destins la forge et des pices forges Mikrogefge von Titanlegierung (a + ) Teil 2 : Mikrogefge Kneterzeugnisse von
4、Stangen, Profilen, Schmiedevormaterial und Schmiedestcken 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 technically approved by the
5、 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, ph ysicaily or functionally, without re-identification of the stand
6、ard. After examination and signature of the AECMA Standard Checking Centre (NPS) 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 : Images of higher quality fo
7、r the prints in this standard are available from BNAE. 1997-07-31 AECMA Guiiedelie 94 B-1200 BRUXELLES Mr Odorico aecma 199 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without
8、license from IHS-,-,-Page 3 prEN 31 14-2 : 1997 STD-AECMA PREN II,I,-ENGL 1,777 m I,OLZI,I, ouixm 525 rn 1 Scope This standard contains pictures of the microstructure of bars, sections, forging stock and forgings for (a + ) titanium alloy. It shall be used in conjunction with EN 31 14-1. 2 Normative
9、 references This European Standard 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 o
10、f these publications apply to this European Standard only when incorporated in it by amendment or revision. For undated references the latest edition of the publication referred to applies. EN 31 14-1 Aerospace series - Microstructure of (a + ) titanium alloy wrought products - Part 1 General requir
11、ements 1) 3 Micrographs Photo micrograph no 2T1 to 2T15 2L1 to 2L15 2T1 O0 to 2T117 2A1 and 2A2 2T200 and 2T201 Description (a + ) structure, globular/lamellar, transverse section. (a + ) structure, globular/lamellar, longitudinal section. (a + ) structure with local blocky a and a stringers, transv
12、erse section. (a + ) structure with lean a areas, longitudinal or transverse section. transformed structure, transverse section. 1 ) Published as AECMA Prestandard at the date of publication of this standard Previous page is blank Copyright Association Europeene des Constructeurs de Materiel Aerospa
13、tial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-STD-AECMA PREN 3LLq-Z-ENGL 3777 m 3032333 0033077 Lib1 m Page 4 prEN 31 14-2 : 1997 (a + i structure, globular/lamellar, transverse section 200 : 1 2T 1 200: 1 2T2 200 : 1
14、2T3 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-STD-AECMA PREN ILLi-Z-ENGL 1777 LO12311 OOL3D98 3TB Page 5 prEN 31 14-2 : 1997 (a + l structure, gl
15、obular/lamellar, transverse section 200 : 1 2T4 200: 1 2T5 200: 1 2T6 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-STD-AECMA PREN 3114-2-ENGL 1777 m
16、 1012311 0033097 234 m Page 6 prEN 3114-2: 1997 (a + i structure, globular/lameilar, transverse section 200 : 1 2T7 200: 1 2T8 200 : 1 2T9 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking per
17、mitted without license from IHS-,-,-STD-AECMA PREN 3LL4-2-ENGL 1777 = LOL23Ll OOL3LOO BBb Page 7 prEN 31 14-2 : 1997 (a + ) structure, globularllamellar, transverse section 200: 1 2T1 O 200 : 1 2T11 200: 1 2T12 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS
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