AECMA PREN 3458-2002 Aerospace Series Titanium Alloy TI-P63 Annealed 900 Less Than or Equal to Rm Less Than or Equal to 1160 MPa Bar and Wire for Fasteners Machined De Less Than or.pdf

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1、AECMA STANDARD NORME AECMA AECMA NORM Declassification approved 2002-04-30 prEN 3458 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: Srie arospatiale Alliage de titane TI-P63 Recuit 900 5 R, 5 1160 MPa Barres et fils pour fixations usines De 5 25 mm ENGLISH

3、VERSION Aerospace series Titanium alloy TI-P63 Ann ea1 ed 900 I R, I1160 MPa Bar and wire for fasteners machined De I25 mm Luft- und Raumfahrt Titanlegierung TI-P63 geglht 900 5 R, 5 1160 MPa Stangen und Draht fr Verbindungselemente De 5 25 mm This Yerospace Series“ Presfandard has been dra needs of

4、 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 Sfandardizafion) for formal vofe. I Replace page

5、 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 3458 Page 3 1 Scope and field of application This standard

6、 specifies for the aerospace appl properties for bar and wire for fasteners mach annealed, iri titanium alloy TI-P63. cation, the mechanical ned, De - 830 900 10 - 25 - Shear Strength RC - k - K MPa Eendlng Impact e oc t h Time Stress w U o Elongatton Rupture Stress Elongatton at rupture Notes (Ja M

7、Pa a % MPa * (JR A - % - *I 1 MPa = 1 N/mm2 see Ilne 98 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 3458 Page 5 1 Ultrasonic test Designation

8、Notes Typical use 2 EN 2003-8 _ _ - 1) Material shall be ultrasonically tested at the nearest practicable diameter to finished size. 2) Class 5. The rules governing the designation of semi-finished products are indicated in standard EN 2600. When the codified designation is used, the identification

9、code shall be as foIlows : Material standard number Letter code (see 6.2) Appropriate dimensional standard code (see 5.3) Data concerning dimension (see EN 2600) I) Determination not required for routine acceptance 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-,-,-