AECMA PREN 3353-2002 Aerospace Series Titanium Alloy TI-P63 Solution Treated and Aged Rm Greater Than or Equal to 1100 MPa Bar and Wire for Fasteners Machined De Less Than or Equal.pdf
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1、AECMA STANDARD NORME AECMA AECMA NORM Declassification approved 2002-04-30 prEN 3353 Edition P 2 April 2002 Comments should be sent within six months after the date of publication to Gulledelle 94 Material Domain AECMA-STAN Mr Evetts 8-1200 BRUXELLES PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPAC
2、E INDUSTRIES - STANDARDIZATION (AECMA-STAN) Gulledelle 94 - 8-1200 BRUXELLES - Tel. (+32) 2 775 8110 - Fax. (+32) 2 775 8111 Supersedes issue P 1 March 1988 ICs: Descriptors: ENGLISH VERSION Aerospace series Titanium alloy TI-P63 Solution treated and aged R, 2 1100 MPa Bar and wire for fasteners mac
3、hined De I25 mm Srie arospatiale Alliage de titane TI-P63 Mis en solution et revenu R, 2 1100 MPa Barres et fils pour fixations usines De 5 25 mm Luft- und Raumfahrt Titanlegierung TI-P63 Isungsgeglht und ausgelagert R, 2 1100 MPa Stangen und Draht fr Verbindungselemente De 5 25 mm This Yerospace Se
4、ries“ Presfandard has been dra needs of fhe Euro concerned Domain pproved by fhe experts of fhe confenf shall nof be changed fo an ally, wifhouf re-idenfificafion of fhe agreemenf of AECMA-STAN if will be submiffed as a Affer examinafi draff European Sfandard fo CEN (European Commiffee for Sfandardi
5、zafion) for formal vofe. I Replace page 1 of the previous issue by this page I 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-,-,-prEN 3353 Page 3 1 This
6、standard specifies for the aerospace application, the mechanical properties for bar and wire for fasteners machined, De 5 25 mm, solution treated and aged, in titanium alloy TI-P63, Scope and field of application Line 7 specifies the heat treatment for the fasteners. Unless otherwise specified by th
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