AECMA PREN 2089-2003 Aerospace Series Aluminium Alloy AL-P2014A T6 or T62 Sheet and Strip 0 4 mm Less Than or Equal to a Less Than or Equal to 6 mm Edition P 1《 航空航天系列.AL-P2014A T6.pdf

1、AECMA STANDARD NORME AECMA AECMA NORM Edition approved for publication 31 March 2003 prEN 2089 Edition P 1 March 2003 Comments should be sent within six months after the date of publication to AECMA-STAN ICs: Descriptors: ENGLISH VERSION Will supersede EN 2089:1994 Aerospace series Aluminium alloy A

2、L-P2014A T6 or T62 Sheet and strip 0,4 mm a 6 mm Srie arospatiale Alliage daluminium AL-P2014A T6 ou T62 Tles et bandes 0,4 mm i ai 6 mm Luft- und Raumfahrt Aluminiumlegierung AL-P2014A T6 oder T62 Bleche und Bnder 0,4 mm i ai 6 mm This “Aerospace Series“ Prestandard has been drawn up under the resp

3、onsibility of AECMA-STAN (The European Association of Aerospace Industries - Standardization). It is 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 publica

4、tion 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 review by users and formal agreement of AECMA-STAN it will be submitted as a draft Europ

5、ean Standard to CEN (European Committee for Standardization) for formal vote. Metallic Material Domain I I Copyright 2003 O by AECMA-STA1 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking perm

6、itted without license from IHS-,-,-Page 2 prEN 2089: 2003 Foreword This standard was reviewed by the Domain Technical Coordinator of AECMA-STANS Metallic Material Domain. After inquiries and votes carried out in accordance with the rules of AECMA-STAN defined in AECMA- STANS General Process Manual,

7、this standard has received approval for Publication. 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 3 prEN 2089: 2003 O Introduction This standar

8、d 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 requirements relating to: Aluminium alloy AL-P2014A

9、 T6 or T62 Sheet and strip 0,4 mm a 6 mm for aerospace application. 2 Normative references This European Standard incorporates by dated or undated refere ce provisia s from other publicatic S. These normative references are cited at the appropriate places in the text and the publications are listed

10、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 referred to applies. EN 4258, Aerospace series - Met

11、allic 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, Aerospace series - Metallic materials - Rules f

12、or drafting and presentation of material standards - Part 2: Specific rules for aluminium, aluminium alloys and magnesium alloys 1 ) 1) Published as AECMA Prestandard at the date of publication of this standard Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS

13、 under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-1 Material designation Aluminium alloy AL-P2014A 500 ?C 5 85 510 ?C I WQ 85 40 ?C + O= ambient It 2 5 d 500 oc 5 e 510 I WQ e 40 oc or + 157 ?C 5 85 163C I18 h 5 t 522 h + 170?C 85 180 ?CI7 h

14、5 t 5 12 h 3.3 9 10 11 12 13 14 15 16 17 18 19 20 21 - - - - - - - - - - - - - - Elongation at A % - Method of melting I Form Sheet and strip Method of production Rolled Limit dimension(s) mm 0,4 a 6 Technical specification EN 4400-2 Delivery condition FI0 T6 I T4 I- - Heat treatment Delivery condit

15、ion code FIA K I U Use condition T62 T62 I T6 Delivery condition + 500 5 e 510 IWQ 8540 + 157 ?C 5 85 163C I18 h 5 t 522 h or + 170C 5 85 180C I7 h t 12 h Delivery condition Delivery condition + 157 ?C 5 85 163 ?C I18 h 5 t 5 22 h or + 170 ?C 5 85 180 ?C I7 h 5 t 5 12 h Heat treatment Characteristic

16、s See EN 4400-2. 3.1 I Test sample(s) I See EN 4400-2. 3.2 I Test piece(s) I Heat treatment Delivery condition: T4 I Use condition: T6 or T62 Dimensions concerned I rn; Thickness of cladding on each face 3,2a6 I 0,4 a 6 Direction of test piece Proof stress - ?C MPa - -I Ambient -I 2 390 T I Strength

17、 I Rm I MPa -I 2 440 I Elongation I A I % -I A50mm 2 7 I Reductionofarea I Z I % -I Hardness -I -I Shear strength Impact strength Temperature e OC 1,5: a= 180? 2,5: a = 180? 33: a= 180? I - 22 I ITime Ihl 23 24 - I Oa Stress MPa I - C Elongation I a 25 I I Rupture stress I OR I MPa I - - 27 I Notes

18、(see line 98) 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-,-,-ixternal defects - 3atch uniformity See EN 4400-2. Marking inspection Iimensional inspe

19、ction - 5 Votes See EN 4400-2. T4 T6 Electrical conductivity y MSlm 18,5 (Typical value) 22,O (Typical value) rypical use Hard ness 115 (Typical value) 6 16 per product A 24 per batch 135 (Typical value) 6 20 per product A 30 per batch HB - - or I See EN 4400-2. See EN 4400-2. -I -I Copyright Associ

20、ation Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-100 See EN 4400-2. Qualification programme to be agreed between manufacturer and purchaser. Page 6 prEN 2089: 2003 - Product qualification 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-,-,-