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
7、e drawing, the order or the inspection schedule, the present standard shall be used in conjunction with the referenced EN standards. 2 References EN 2003-8, EN 2032-1, EN 2032-2, EN 2098-6, EN 2340, EN 2500-4, EN 2600, EN 3502, Aerospace series - Test methods - Ultrasonic test for titanium and titan
8、ium alloys, steel and steel alloys and heat resisting alloys 1) Aerospace series - Conventional designation for metallic materials Aerospace series - Metallic materials - Part 2 - Coding of material in delivery heat treatment conditions Aerospace series - Inspection and testing requirements for tita
9、nium and titanium alloys wrought products - Part 6 - Inspection and testing requirements for bar and wire for fasteners Aerospace series - Round bars - Titanium and titanium alloys - Diameter 10 irection of sample - O I Temperature O e Proof Stress i 1 Strength 4 erdness Elongation Reduction of area
10、 MPa *) - 1030 Rm A5 - WPa 1 - % - 8 - 20 - Z % HE ;hear Strength MPa *I 675 3ending k mpect Y Temperature Time Stress Elongation % WPa *I - Rupture Stress E longat ion at rupture A % - 0s line 98 1) *) 1 MPa= 1 N/mm2 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided
11、 by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3353 Page 5 1 Ultrasonic test Designation Notes Typical use 2 EN 2003-8 1) Material shall be ultrasonically tested at the nearest practicable diameter 2) Class 5. to finished size
12、in accordance with EN 2003-8. The rules governing the designation of semi-finished products are indicated in standard EN 2600, When the codified designation is used, the identification code shall be as follows : ,EN 33531, FI ,XX, 1- Material standard- number Data concerning dimension (see EN 2600)
13、1 II I /Letter code (see 6.2) I I Appropriate dimensional standard code (see 5.3) 1) 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-,-,-
