1、AECMA STANDARD NORME AECMA AECMA NORM Edition approved for publication 14 March 2003 prEN 4100 Edition P 2 March 2003 Comments should be sent within six months after the date of publication to AECMA-STAN ICs: Descriptors: ENGLISH VERSION Supersedes edition P 1 August 1993 Aerospace series Aluminium
2、alloy AL-P2219- T6 or T62 Sheet and strip 0,5 mm a 6 mm Srie arospatiale Alliage daluminium AL-P2219- T6 ou T62 Tles et bandes 0,5 mm i ai 6 mm Luft- und Raumfahrt Aluminiumlegierung AL-P2219- T6 oder T62 Bleche und Bnder 0,5 mm i ai 6 mm This “Aerospace Series“ Prestandard has been drawn up under t
3、he responsibility 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
4、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 review by users and formal agreement of AECMA-STAN it will be submitted as a draf
5、t European 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 networki
6、ng permitted without license from IHS-,-,-Page 2 prEN 4100: 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 M
7、anual, 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 4100: 2003 O Introduction This
8、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 requirements relating to: Aluminium alloy AL
9、-P2219- T6 or T62 Sheet and strip 03 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 l
10、isted 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
11、 - 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, Aerospace series - Metallic materials -
12、Rules for 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
13、by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-1 Material designation Aluminium alloy AL-P2219- Heat treatment Delivery condition code Use condition Delivery condition + 185 “C 6% 196 “C I30 h t 40 h - - + 530 OC e so OC 1 WQ e 40 OC
14、 A F U T62 T6 Heat treatment Delivery condition + 530 OC e 540 OC 1 WQ e 40 OC + 185 “C 6% 196 “C I30 h t 40 h Delivery condition Impact strength Temperature e OC Time h - - - 41 I Method of melting I Form Sheet and strip Method of production Rolled Limit dimension(s) mm 0,5 a 6 Technical specificat
15、ion EN 4400-2 T6 I HI11 I O I Delivery condition Characteristics I See EN 4400-2. I 3.1 I Test sample(s) I See EN 4400-2. 3.2 I Test piece(s) I I 3.3 I Heat treatment I Delivery condition: O or HI 11 I Use condition: T6 or T62 Dimensions concerned mm I 0,5 a 6 I 0,5 a 1,0 I 1,0 a 6 Thickness of clad
16、ding on each face LT LT LT D - ection of test piece Temperature Proof stress Strength “C Ambient Ambient Ambient MPa 110 2 250 2 250 MPa 220 2 375 2 375 T I Elongation I A I Reduction of area I Z I I 17 I Hardness 18 I Shearstrength I R, I MPa I I 19 I Bending Ikl-l I 20 21 22 23 24 - - - - I ch Str
17、ess I MPa I C Elongation I a 25 26 - Rupture stress I Elongation at ru Dtu re I MPa I 27 I Notes (see line 98) I I Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license f
18、rom IHS-,-,-Page 5 prEN 4100: 2003 - 5 ixternal defects See EN 4400-2. T6 3atch uniformity Hardness Marking inspection Iimensional inspection 105 (Typical value) HB 6 16 per product A 24 per product Votes - - rypical use See EN 4400-2. See EN 4400-2. -I See EN 4400-2. 7 I Electrical conductivity I y
19、 I MSlm I 19 (Typicalvalue) -I -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-,-,-100 See EN 4400-2. Qualification programme to be agreed between manufacturer and purchaser. Page 6 prEN 4100: 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-,-,-
