1、AECMA STANDARD NORME AECMA AECMA NORM prEN 331 6 Edition P 2 May 1995 EDITE PAR LASSOCIATION EUROPEENNE DES CONSTRUCTEURS DE MATERIEL AhOSPATIAL Technopolis - 175, rue Jean-Jacques Rousseau - F-92138 Issy-les-Moulineaux Cedex - Tl. (1) 47.36.98.76 ICs : Descriptors : Supersedes Issue P 1 March 1988
2、ENGLISH VERSION Aerospace series Titanium alloy TI-P64 Annealed Rm 2 1070 MPa Sheet and strip a16mm Srie arospatiale Alliage de titane TI-P64 Recuit R, 2 1070 MPa Tles et bandes aI6mm Luft- und Raumfahrt Titanlegierung TI-P64 geglht R, 2 1070 MPa Bleche und Bnder al6mm This “Aerospace Series Prestan
3、dard has b (Association Europenne des Constructeurs de concerned Technical Com e Member countries. tandard, the technical content shall not be changed to ed, ph ysically or functionally, without re-identification ture of the AECMA Standard Checking Centre (NPS) and formal rd to CEN (European Committ
4、ee for Standardization) for formal vote. Replace page 1 of the previous issue by this page Nota Extra copies can be supplied by E.N.A.E. - Technopolis 54 - 199. rue Jean-Jacques Rousseau - 921 38 ISSY-LES-MLINEAUX CEDEX Withdrawal approved 1995-05-3 1 Comments should be sent within six months after
5、the date of publication to AECMA Technopolis - 175, rue Jean-Jacques Rousseau 921 38 Issy-les-Moulineaux Cedex - FRANCE C5 Chairman M. Odorico aecma 1995 prEN 3316 Page 3 1 This standard specifies for the aerospace application, the mechanical properties for sheet and strip a 5 6 mm, annealed, in tit
6、anium alloy Scope and field of application TI-P64. Unless otherwise specified by the drawing, the order or the inspection schedule, the present standard shall be used in conjunction with the referenced EN standards. 2 References EN 2032-1, EN 2032-2, EN 2098-2, EN 2338, EN 2339, EN 2500-4, EN 2600,
7、Aerospace series - Conventional designation for metal 1 ic materiais Aerospace series - Metallic materials - Part 2 - Coding of material in delivery heat treatment coriditions Aerospace series - Inspection and testing requirements for titanium and heat resisting alloys wrought product - Part 2 - Ins
8、pection and testing requirements for sheets, strips and plates Aerospace series - Sheets - Titanium and titanium alloys - Hot rolled - Thickness 0,8 5 a 5 6 mm - Dimensions Aerospace series - Sheets - Titanium and titanium alloys - Cold rolled - Thickness 0,2 5 a Aerospace series - Guidelines for th
9、e preparation and use of standards for metallic materiais - Part 4 - Titanium and titanium alloys 1) 3 mm - Dimensions Aerospace series - Designation of metallic semi-finished products - Rules 1). i) in preparation AECMA PREN33Lb 88 U 10L23LL 0005387 3 B prEN 3316 Page 4 Al V Sn Cu Fe I I I I Elemen
10、t Chem bai Composition I min. 5,O 5,O 1,5 0,35 0,35 6,O 6,O 2,5 3,O 1,0 1 2 3 Multiple melting. At least the final melt shall be in vacuum using consumable stages may use non-consumable electrode Sheet and strip a 1000 - 1000 Direction of sample I Temperature I 8 g: Proof W I stress IRQ MPa i 1 w I-
11、 E Strength WPa *: - % - 1070 1070 Elongation ASc I I = - 8 - 7 % - - a2mn: k=4 2 a 6 m : k = 4,5 - MPa c( -A O! - - Hardness HE Shear Strength Rc Bending k impect K le I Temperature oc h l -I- MPa % - - MPe W Stress aa UI - IE 0 Elongation 8 Ruptu re Stress IA Elongation nt rupture Notas see Ilne 9
12、8 % - *) 1 MPa = 1 N/mm2 AECMA PREN3316 ._ - 88 W 1012311 0005388 - O _ - h prBN 3316 Page 5 1 Designation Noter Typical use - 2 The rules governing the designation of semi-finished products are indicated in standari EN 2600. When the codified designation is used, the identification code shall be as follows I Material standard number code (see 6.2) dimensional standard code (see 5.3) Data concerning dimension (see EN 2600) 1) Determination not required for routine acceptance
