AECMA PREN 3316-1995 Aerospace Series Titanium Alloy TI-P64 Annealed Rm Greater Than or Equal to 1070 MPa Sheet and Strip a Less Than or Equal to 6 mm Edition P 2 WITHDRAWN《航空航天系列..pdf

《AECMA PREN 3316-1995 Aerospace Series Titanium Alloy TI-P64 Annealed Rm Greater Than or Equal to 1070 MPa Sheet and Strip a Less Than or Equal to 6 mm Edition P 2 WITHDRAWN《航空航天系列..pdf》由会员分享，可在线阅读，更多相关《AECMA PREN 3316-1995 Aerospace Series Titanium Alloy TI-P64 Annealed Rm Greater Than or Equal to 1070 MPa Sheet and Strip a Less Than or Equal to 6 mm Edition P 2 WITHDRAWN《航空航天系列..pdf（4页珍藏版）》请在麦多课文档分享上搜索。

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 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or

6、 networking permitted without license from IHS-,-,-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 titanium alloy Scope and field of application TI-P64. Unless otherwise specified by the drawing, the order

7、 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, Aerospace series - Conventional designation for metal 1 ic materiais Aerospace series - Metallic materi

8、als - 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 - Inspection and testing requirements for sheets, strips and plates Aerospace series - Sheets - Titanium and

9、 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 the preparation and use of standards for metallic materiais - Part 4 - Titanium and titanium alloys 1) 3

10、mm - Dimensions Aerospace series - Designation of metallic semi-finished products - Rules 1). i) in preparation Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from

11、 IHS-,-,-AECMA PREN33Lb 88 U 10L23LL 0005387 3 B prEN 3316 Page 4 Al V Sn Cu Fe I I I I Element 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

12、strip a 1000 - 1000 Direction of sample I Temperature I 8 g: Proof W I stress IRQ MPa i 1 w I- 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 % - - MP

13、e W Stress aa UI - IE 0 Elongation 8 Ruptu re Stress IA Elongation nt rupture Notas see Ilne 98 % - *) 1 MPa = 1 N/mm2 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without licen

14、se from IHS-,-,-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

15、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 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-,-,-