1、AECMA PREN3464 96 W LOL23LL OCIL0466 74T W AECMA STANDARD prEN 3464 NORME AECMA Edition P 2 AECMA NORM May 1996 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA) Gulledelle 94 - E-1 200 BRUXELLES - Tel. (32) 2 775 81 1 O - Fax. (32) 2 775 81 1 1 ICs : Supersedes issue P1 March 19
2、88 Descriptors : ENGLISH VERSION Aerospace series Titanium alloy TLP64001 Annealed Plate 6 mm a 5100 mm Srie arospatiale Alliage de titane TI-P64001 Recuit Plaques 6 mm a 5100 mm Luft- und Raumfahrt Titanlegierung TLP64001 G egl ht Platten 6 mm a 1100 mm This “Aerospace Series“ Prestandard has been
3、drawn up under the responsibility of AECMA (The European Association of Aerospace Industriesl. It is published on green paper for the needs of AECMA-Members. It has been technically approved by the experts of the concerned Technical Committee following comment by the Member countries. Subsequent to
4、the publication of this Prestandard, the technical content shall not be changed to an extent that interchangeability is affected, physically or functionally, without re-identification of the standard. After examination and signature of the AECMA Standard Checking Centre (NPS) and formal agreement of
5、 the Official Services of the Member countries it will be submitted as a draft European Standard to CEN (European Committee for Standardization) for formal vote. Nota - Extra copies can be supplied by B.N.A.E. - Technopolis 54 - 199, rue Jean-Jacques Rousseau - 921 38 ISSY-LEC-MOULINEAUX CEDEX I Edi
6、tion approved for publication Comments should be sent within six months after the date of publication to 1996-05-3 1 AECMA Gulledelle 94 B-1200 BRUXELLES C5 Chairman Mr Odorico I I aecrna 199 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with
7、 AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,- - AECMA PREN34b4 96 m LO12311 0010Yb8 512 m Page 3 prEN 3464 : 1996 O Introduction This standard is part of the series of EN metallic material standards for aerospace applications. The general organization of t
8、his series is described in EN 4258. This standard has been prepared in accordance with EN 4500-4. 1 Scope This standard specifies the requirements relating to : Titanium alloy TLP64001 Annealed Plate 6mma100mm for aerospace applications. 2 Normative references This European Standard incorporates -y
9、dated or undated reference provisions from other publications. These normative references are cited at the appropriate places in the text and the publications are listed hereafter. For dated references, subsequent amendments to or revisions of any of these publications apply to this European Standar
10、d only when incorporated in it by amendment or revision. For undated references the latest edition of the publication referred to applies. EN 2043 EN 3114-3 EN 3544-1 EN 3544-2 EN 4258 EN 4500-4 Aerospace series - Metallic materials - General requirements for semi-finished product qualification (exc
11、luding forgings and castings) Aerospace series - Microstructure of (a + ) titanium alloy wrought products - Part 3 : Microstructure of plate 2, Aerospace series - Titanium and titanium alloys - Wrought products - Technical specification - Part 1 : General requirements Aerospace series - Titanium and
12、 titanium alloys - Wrought products - Technical specification - Part 2 : Plate, sheet and strip Aerospace series - Metallic materials - General organization of standardization - Links between types of EN standards and their use Aerospace series - Metallic materials - Rules for drafting and presentat
13、ion of material standards - Part 4 : Specific rules for titanium and titanium alloys 2, 1) Published as AECMA Prestandard at the date of publication of this standard 2) In preparation at the date of publication of this standard Copyright Association Europeene des Constructeurs de Materiel Aerospatia
14、l Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 4 prEN 3464 : 1996 Matenal designation Titanium alloy TI-P64001 - Chemical Element com posit ion % min. max. Method of melting I See EN 3544-1 Others 1) AI V 02+2NZ N2 H2
15、 C Fe Ti 5,5 3,5 6,75 45 0,25 0,03 0,0125 0,08 0,30 0,lO 0,40 Each Total - - - - - - - Base - Form Method of production Limit dimension(s) I mm I 6as100 Plate - Technical specification I EN 3544-2 6.1 6.2 Delivery condition Annealed Heat treatment 690 “C I O 840 C / t 2 30 min I AC or inert atmosphe
16、re Delivery condition code U 7 I - I 8.1 I Sample(s) I Use condition Delivery condition Heat treatment - - I 8.2 1 Test piece) I I 8.3 9 Heat treatment Use condition imensionsconcerned I rnm 6as12 I 12a140 I 40as100 (%I Thickness of cladding on 101 each face - “C 11 12 13 14 15 16 17 - - - - - - See
17、 EN 3544-2 See EN 3544-2 See EN 3544-2 ST Ambient Temperature I Elongation I A 0 Hardness MPa MPa % 96 2 830 2 830 2 830 t 830 900 5 Rm 5 I 160 9001Rm1 160 900SRmSl 160 900SRm1 160 2 10 28 28 26 - 2 20 2 20 2 15 - 18 19 Shear strength Rc MPa - Bending k- - I 20 I Impact strength I - C 1 25 Time h -
18、Stress ea MPa - Elongation a% - Rupture stress oR MPa - i - I I Temperature 1 O I “C I - Elongation at rupture A % - Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license
19、 from IHS-,-,- AECkaA PREN34bY 96 W 1012311 0010Lt70 170 Page 5 prEN 3464 : 1996 icrostructure ixternal defects nternal defects Mace contamination Marking inspection I - 96 Dimensional inspection I if incidence less than if incidence of 5 or more if incidence less than 5 per cmz of the sampling sect
20、ion sampling section 3 T 200 to 3 T 202 if incidence of 5 or more per ern of the 3A1 to3AB - - See EN 3544-2 See EN 3544-2 See EN 3544-2 I See EN 3544-2 See EN 3544-2 1) Determination not required for routine acceptance I Copyright Association Europeene des Constructeurs de Materiel Aerospatial Prov
21、ided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,- AECMA PREN3464 96 m 1012311 0010471 007 m Page 6 prEN 3464 : 1996 roduct qualification See EN 2043 lualification programme to be agreed between manufacturer and purchaser 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-,-,-
