1、AECMA STANDARD NORME AECMA AECMA NORM prEN 3459 Edition P 2 May 1996 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA) Gulledelle 94 - B-1200 BRUXELLES - Tel. (32) 2 775 81 10 - Fax. (32) 2 775 81 11 ICs : ENGLISH VERSION Aerospace series Titanium alloy TLP63001 Solution treated
2、and aged Plate 6 mm a 5 50 mm Supersedes issue P1 March 1988 Srie arospatiale Alliage de titane TLP63001 Mis en solution et revenu Plaques 6 mm a I50 mm Luft- und Raumfahrt Titanlegierung TLP63001 Lsungsgeglht und ausgelagert Platten 6 mm a I 50 mm This “Aerospace Series“ Prestandard has been drawn
3、up under the responsibility of AECMA (The European Association of Aerospace Industries). 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 the pu
4、blication 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 the O
5、fficial 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 JeamJacques Rousseau - 921 38 ISSY-LES-MOULINEAUX CEDEX C5 Chairman
6、I Comments should be sent within six months after the date of oublication to I I Edition approved for publication 1996-05-31 AECMA Gulledelle 94 B-1200 BRUXELLES Mr Odorico aecma 1996 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANo
7、t for ResaleNo reproduction or networking permitted without license from IHS-,-,-AECMA PREN3459 96 = 1012311 0010462 OT4 D Page 3 prEN 3459 : 1996 O Introduction This standard is part of the series of EN metallic material standards for aerospace applications. The general organization of this series
8、is described in EN 4258. This standard has been prepared in accordance with EN 4500-4. I Scope This standard specifies the requirements relating to : Titanium alloy TLP63001 Solution treated and aged Plate 6 mm as 50 mm for aerospace applications. 2 Normative references This European Standard incorp
9、orates by 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 Europe
10、an Standard 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 qualific
11、ation (excluding forgings and castings) Aerospace series - Microstructure of (a + ) titanium alloy wrought products - Part 3 : Microstructure of plate Aerospace series - Titanium and titanium alloys - Wrought products - Technical specification - Part 1 : General requirements I) Aerospace series - Ti
12、tanium and 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 l) Aerospace series - Metallic materiais - Rules for drafting
13、and presentation of material standards - Part 4 : Specific rules for titanium and titanium alloys *) 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 Materi
14、el Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 4 prEN 3459 : 1996 6.2 AECMA PREN3459 96 m 3032333 O030463 T30 m + 500 “C f 10 “C It = 24 h /AC Delivery condition code U Heat treatment - L LT L LT ST 2 900
15、 1 030 R, 1 220 29 2 20 2 920 2 900 2 920 2900 1030Rm 1050R, 1030IR, 5 1 220 Il 220 I 1 220 1 050 R, 1 220 29 29 29 27 2 20 2 20 2 20 220 Form Plate Method of Droduction - Limit dimension(s) mm 6as50 Technical specification EN 3544-2 I Heat treatment I 900C ? lOC/t 2 20 min /AC 7 I Use condition I D
16、elivery condition I Characteristics Sample(s) rest piece(s) +eat treatment Delivery condition I 3imensions concerned rhickness of cladding on sach face Direction of test piece “C MPa - Ambient Temperature Strength T MPa 1 Elongation I A 1 % Pl% Reduction of I area Hardness Shear strength R, MPa Bend
17、ing k- Impact strength MPa % - Stress 1 Rupture stress I A I Mr Elongation at rupture Notes (see line 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-,
18、-,-AECflA PREP43459 96 1012311 OO104b4 977 icrostructure Memal defects itemal defects iurface contamination Marking inspection Dimensional inspection - Notes Typical use Page 5 prEN 3459 : 1996 See EN 3544-2 if incidence less than U incidence of 5 or me - See EN 3544-2 - See EN 3544-2 I -I See EN 35
19、44-2 - See EN 3544-2 1) Determination not required for routine acceptance - -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-,-,-Page 6 prEN 3459 : 1996
20、Product qualification See EN 2043 iualification 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-,-,-
