1、BRITISH STANDARD AEROSPACE SERIESBS EN 4007:2005Aluminium alloy AL-P6082-T6 or T62 Sheet and strip 0,4 mm ka k6 mmICS 49.025.20g49g50g3g38g50g51g60g44g49g42g3g58g44g55g43g50g56g55g3g37g54g44g3g51g40g53g48g44g54g54g44g50g49g3g40g59g38g40g51g55g3g36g54g3g51g40g53g48g44g55g55g40g39g3g37g60g3g38g50g51g6
2、0g53g44g42g43g55g3g47g36g58IncorporatingcorrigendumNovember 2010 National forewordThis British Standard is the UK implementation of EN 4007:2005. It supersedes BS L 113:1971 which is withdrawn.The UK participation in its preparation was entrusted by Technical Committee ACE/61, Metallic materials for
3、 aerospace purposes, to Subcommittee ACE/61/-/24, Light alloys.A list of organizations represented on this subcommittee can be obtained on request to its secretary.This publication does not purport to include all the necessary provisions of a contract. Users are responsible for its correct applicati
4、on.Compliance with a British Standard cannot confer immunity from legal obligations.BS EN 4007:2005This British Standard waspublished under the authorityof the Standards Policy andStrategy Committeeon 4 October 2005 BSI 2010Amendments/corrigenda issued since publicationDate Comments 30 November 2010
5、 Addition of supersession details to national foreword.ISBN 978 0 580 72943 0EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4007 June 2005 ICS 49.025.20 English version Aerospace series - Aluminium alloy AL-P6082-T6 or T62 - Sheet and strip - 0,4 mm a 6 mm Srie arospatiale - Alliage daluminium
6、 AL-P6082-T6 ou T62 - Tles et bandes - 0,4 mm a 6 mm Luft- und Raumfahrt - Aluminiumlegierung AL-P6082-T6 oder T62 - Bleche und Bnder - 0,4 mm a 6 mm This European Standard was approved by CEN on 22 April 2005. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate
7、 the conditions for giving this European Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the Central Secretariat or to any CEN member. This European Standard exists
8、 in three official versions (English, French, German). A version in any other language made by translation under the responsibility of a CEN member into its own language and notified to the Central Secretariat has the same status as the official versions. CEN members are the national standards bodie
9、s of Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom. EUROPEAN COMMITTEE FOR
10、STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG Management Centre: rue de Stassart, 36 B-1050 Brussels 2005 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4007:2005: E2 Foreword This document (EN 4007
11、:2005) has been prepared by the European Association of Aerospace Manufacturers - Standardization (AECMA-STAN). After enquiries and votes carried out in accordance with the rules of this Association, this Standard has received the approval of the National Associations and the Official Services of th
12、e member countries of AECMA, prior to its presentation to CEN. This European Standard shall be given the status of a national standard, either by publication of an identical text or by endorsement, at the latest by December 2005, and conflicting national standards shall be withdrawn at the latest by
13、 December 2005. Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. CEN and/or CENELEC shall not be held responsible for identifying any or all such patent rights. According to the CEN/CENELEC Internal Regulations, the national standa
14、rds organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slo
15、vakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. BS EN 4007:2005EN 4007:2005 (E)3 Introduction 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
16、prepared in accordance with EN 4500-2. 1 Scope This standard specifies the requirements relating to: Aluminium alloy AL-P6082- T6 or T62 Sheet and strip 0,4 mm a 6 mm for aerospace application. 2 Normative references The following referenced documents are indispensable for the application of this do
17、cument. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 4258, Aerospace series Metallic materials General organization of standardization Links between types of EN standards and their u
18、se. 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 for drafting and presentation of material standards Part 2: Specific rules for aluminium, aluminium alloys and magnes
19、ium alloys. 1) 1) Published as AECMA Prestandard at the date of publication of this standard. BS EN 4007:2005EN 4007:2005 (E)4 1 Material designation Aluminium alloy AL-P6082- Others Element Si Fe Cu Mn Mg Cr Zn Ti Each Total Al min. 0,7 0,40 0,6 2 Chemical composition % max. 1,3 0,50 0,10 1,0 1,2 0
20、,25 0,20 0,10 0,05 0,15 Base 3 Method of melting 4.1 Form Sheet and strip 4.2 Method of production Rolled 4.3 Limit dimension(s) mm 0,4 a 6 5 Technical specification EN 4400-2 Delivery condition O H111 T4 T6 6.1 Heat treatment 525 C 540 C / WQ 40 C + = ambient / t 5 d 525 C 540 C / WQ 40 C + 160 C 1
21、80 C / 8 h t 16 h 6.2 Delivery condition code A F K U Use condition T62 T6 T67 Heat treatment Delivery condition + 525 C 540 C / WQ 40 C + 160 C 180 C / 8 h t 16 h Delivery condition + 160 C 180 C / 8 h t 16 h Delivery condition Characteristics 8.1 Test sample(s) See EN 4400-2. 8.2 Test piece(s) See
22、 EN 4400-2. 8.3 Heat treatment Delivery condition: O or H111 Use condition: T6 or T62 9 Dimensions concerned mm 0,4 a 3,0 3,0 a 6 0,4 a 0,8 0,8 a 6 10 Thickness of cladding on each face % 11 Direction of test piece LT LT LT LT 12 Temperature C Ambient Ambient Ambient Ambient13 Proof stress Rp0,2MPa
23、85 85 260 260 14 Strength RmMPa 150 150 310 310 15 Elongation A % A50mm 16 A50mm 18 A50mm 8 A50mm 9 16 T Reduction of area Z % 17 Hardness 18 Shear strength RcMPa 19 Bending k 1; = 180 1; = 180 20 Impact strength 21 Temperature C 22 Time h 23 Stress aMPa 24 Elongation a % 25 Rupture stress RMPa 26 C
24、 Elongation at rupture A % 27 Notes (see line 98) BS EN 4007:2005EN 4007:2005 (E)5 44 External defects See EN 4400-2. 82 Batch uniformity See EN 4400-2. 5 T4 T6 60 (Typical value) 100 (Typical value) 16 per product 20 per product 7 Hardness HB 24 per batch 30 per batch 95 Marking inspection See EN 4
25、400-2. 96 Dimensional inspection See EN 4400-2. 98 Notes 99 Typical use BS EN 4007:2005EN 4007:2005 (E)6 100 Product qualification See EN 4400-2. Qualification programme to be agreed between manufacturer and purchaser. BS EN 4007:2005EN 4007:2005 (E)blankBSI GroupHeadquarters 389 Chiswick High Road,
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