1、AECMA STANDARD NORME AECMA I AECMA NORM prEN 4005 Edition P 2 July 2002 Edition approved for publication 31 July 2002 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES - STANDARDIZATION 1 k Gulledelle 94 - B-1200 Brussels - Tel. + 32 2 775 81 10 - Fax. + 32 2 775 81 11 - www.aecma-stan.o
2、rg Comments should be sent within six months after the date of publication to Gulledeile 94 AECMA-STAN 8-1200 BRUXELLES ICs: Descriptors: Supersedes edition P 1 August 1993 ENGLISH VERSION Aerospace series Al umin i um alloy AL-P5052- O Sheet and strip 0,3 mm I a I6 mm Srie arospatiale Alliage dalum
3、inium AL-P5052- O Tles et bandes 0,3 mm las 6 mm Luft- und Raumfahrt Aluminiumlegierung AL-P5052- O Bleche und Bnder 03 mm I a I6 mm This “Aerospace Series“ Prestandard has been drawn up under the responsibility of AECMA-STAN (The European Association of Aerospace Industries - Standardization). It i
4、s published on green paper for the needs of the European Aerospace Industry. It has been technically approved by the experts of the concerned Domain following member comments. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that interchangea
5、bility is affected, physically or functionally, without re-identification of the standard. After examination and review by users and formal agreement of AECMA-STAN it will be submitted as a draft European Standard to CEN (European Committee for Standardization) for formal vote. Nota - Extra copies c
6、an be supplied by B.N.A.E. - Technopolis 54 - 199, nie Jean-Jacques Rousseau - 92138 ISSY-LES-MOULINEAUX CEDEX I I Material Domain I l I Copyright 2002 O by AECMA-STA Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo re
7、production or networking permitted without license from IHS-,-,-Page 2 prEN 4005: 2002 Blank page 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
8、3 prEN 4005: 2002 O I n troducti o n This standard is part of the series of EN metallic material standards for aerospace applications. The general organization of this series is described in EN 4258. This standard has been prepared in accordance with EN 4500-2. 1 Scope This standard specifies the re
9、quirements relating to: Aluminium alloy AL-P5052- O Sheet and strip 0,3 mm Sa I6 mm for aerospace applications. 2 Norma tive references This European Standard incorporates by dated or undated reference provisions from other publications. These normative references are cited at the appropriate places
10、 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 Standard only when incorporated in it by amendment or revision. For undated references the latest edition of the publication referre
11、d to applies. EN 4258 Aerospace series - Metallic materials - General organization of standardization - Links between types of EN standards and their use EN 4400-2 Aerospace series - Aluminium and aluminium alloy wrought products - Technical specification - Part 2: Sheet and strip 1) EN 4500-2 Aeros
12、pace series - Metallic materials - Rules for drafting and presentation of material standards - Part 2: Specific rules for aluminium, aluminium alloys and magnesium alloys 1) I) Published as AECMA Prestandard at the date of publication of this standard Copyright Association Europeene des Constructeur
13、s de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 4 prEN 4005: 2002 Form Method of production 2 9 J Sheet and strip Rolled 6.1 Delivery condition Heat treatment I 0,3 I a I 6 Limit dimension(s) I
14、mm I O - Technical specification 6.2 7 EN 4400-2 Delivery condition code U Use condition O Heat treatment Delivery condition Il I 8.1 Test sample(s) 8.2 Test piece(s) See EN 4400-2. See EN 4400-2. Characteristics 9 10 Dimensions concerned mm 0,3 I a I 0,8 0,8 a I6 Thickness of cladding on % - - each
15、 face I Use condition I 8.3 I Heat treatment 11 12 - - -. . . - - - I Direction of test piece LT LT Temperature I eloc Ambient Ambient dl I I I I 13 I I Proof stress I Rmo.z I MPa I 2 65 I 165 I _ 15 Elongation A% As mm 2 16 Aso mm 2 19 16 Reduction of area 2 % - 17 Hardness - -, I 170 I i?, I215 14
16、 I T I Strength I Rm 1MPal 170 5 Rm I215 I 20 Impact strength - 21 Temperature 0 “C - - 22 Time h - 27 Notes (see line 98) - I I 18 I Shear strength I R, 1 MPa I - I I 19 1 Bending lkl-1 - I Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with
17、AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Ixternal defects - - - - - Varking inspection Dimensional inspection See EN 4400-2. See EN 4400-2. - - Notes Typical use Page 5 prEN 4005: 2002 See EN 4400-2. Copyright Association Europeene des Constructeurs de
18、Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 6 prEN 4005: 2002 roduct qualification See EN 4400-2. _ hJaiification 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-,-,-
