EN 4003-2006 en Aerospace series - Aluminium alloy AL-P2219-T87 - Sheet and strip 0 5 mm less than or equal to a less than or equal to 6 mm《航空航天系列 铝合金AL-P2219-T87 薄板材和带材0 5mm≤a≤6mm.pdf

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1、BRITISH STANDARDBS EN 4003:2006Aerospace series Aluminium alloy AL-P2219-T87 Sheet and strip 0,5 mm k a k 6 mmThe European Standard EN 4003:2006 has the status of a British StandardICS 77.150.10g49g50g3g38g50g51g60g44g49g42g3g58g44g55g43g50g56g55g3g37g54g44g3g51g40g53g48g44g54g54g44g50g49g3g40g59g38

2、g40g51g55g3g36g54g3g51g40g53g48g44g55g55g40g39g3g37g60g3g38g50g51g60g53g44g42g43g55g3g47g36g58BS EN 4003:2006This British Standard was published under the authority of the Standards Policy and Strategy Committee on 30 March 2007 BSI 2007ISBN 978 0 580 50390 0National forewordThis British Standard wa

3、s published by BSI. It is the UK implementation of EN 4003:2006.The UK participation in its preparation was entrusted by Technical Committee ACE/61, Metallic materials for aerospace purposes, to Panel ACE/61/-/24, Light alloys.A list of organizations represented on ACE/61/-/24 can be obtained on req

4、uest to its secretary.This publication does not purport to include all the necessary provisions of a contract. Users are responsible for its correct application.Compliance with a British Standard cannot confer immunity from legal obligations.Amendments issued since publicationAmd. No. Date CommentsE

5、UROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4003 December 2006 ICS 77.150.10 English Version Aerospace series - Aluminium alloy AL-P2219-T87 - Sheet and strip 0,5 mm a 6 mm Srie arospatiale - Alliage daluminium AL-P2219-T87 - Tles et bandes 0,5 mm a 6 mm Luft- und Raumfahrt - Aluminiumlegier

6、ung AL-P2219-T87 -Bleche und Bnder 0,5 mm a 6 mm This European Standard was approved by CEN on 12 June 2006. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standard the status of a national standard without any altera

7、tion. 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 in three official versions (English, French, German). A version in any other language made by transla

8、tion 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 bodies of Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hun

9、gary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG Management Cent

10、re: rue de Stassart, 36 B-1050 Brussels 2006 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4003:2006: E2 Contents Page Foreword3 Introduction .4 1 Scope 4 2 Normative references 4 EN 4003:20063 Foreword This document (EN 4003:200

11、6) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-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 t

12、he member countries of ASD, 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 June 2007, and conflicting national standards shall be withdrawn at the latest by June

13、 2007. 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 standards organ

14、izations 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, Romania, Slo

15、vakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. EN 4003:20064 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 prepared in accorda

16、nce with EN 4500-2. 1 Scope This standard specifies the requirements relating to: Aluminium alloy AL-P2219-T87 Sheet and strip 0,5 mm a 6 mm for aerospace applications. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated referen

17、ces, 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 use EN 4400-2, Aerospace s

18、eries Aluminium and aluminium alloy wrought products Technical specification Part 2: Sheet and strip1)EN 4500-2, Aerospace series Metallic materials Rules for drafting and presentation of material standards Part 2: Specific rules for aluminium, aluminium alloys and magnesium alloys1)1) Published as

19、ASD prestandard at the date of publication of this standard. EN 4003:20065 1 Material designation Aluminium alloy AL-P2219- Others Element Si Fe Cu Mn Mg Zn Ti V Zr Each Total Al min. 5,8 0,20 0,02 0,05 0,10 2 Chemical composition % max. 0,20 0,30 6,8 0,40 0,02 0,10 0,10 0,15 0,25 0,05 0,15 Base 3 M

20、ethod of melting 4.1 Form Sheet and strip 4.2 Method of production Rolled 4.3 Limit dimension(s) mm 0,5 a 6 5 Technical specification EN 4400-2 Delivery condition T37 T87 6.1 Heat treatment 530 C 540 C / WQ 40 C + approximately 7 % cold work + = ambient / t 5 d 530 C 540 C / WQ 40 C + approximately

21、7 % cold work + 157 C 168 C / 10 h t 28 h 6.2 Delivery condition code K U Use condition T87 T87 7 Heat treatment Delivery condition + 157 C 168 C / 10 h t 28 h Delivery condition Characteristics 8.1 Test sample(s) See EN 4400-2. 8.2 Test piece(s) See EN 4400-2. 8.3 Heat treatment Use condition 9 Dim

22、ensions concerned mm 0,5 a 1,0 1,0 a 6 10 Thickness of cladding on each face % 11 Direction of test piece LT LT 12 Temperature C Ambient Ambient 13 Proof stress Rp0,2 MPa 360 360 14 Strength RmMPa 440 440 15 Elongation A % A50 mm 5 A50 mm 6 16 T Reduction of area Z % 17 Hardness 18 Shear strength Rc

23、MPa 19 Bending k 20 Impact strength 21 Temperature C 22 Time h 23 Stress aMPa 24 Elongation a % 25 Rupture stress RMPa 26 C Elongation at rupture A % 27 Notes (see line 98) EN 4003:20066 44 External defects See EN 4400-2. See EN 4400-2.5 T37 T87 7 Electrical conductivity MS/m 16,5 (Typical value) 21

24、,5 (Typical value) or 95 (Typical value) 130 (Typical value) 16 per product 20 per product 82 Batch uniformity 7 Hardness HB 24 per batch 30 per batch 95 Marking inspection See EN 4400-2. 96 Dimensional inspection See EN 4400-2. 98 Notes 99 Typical use EN 4003:20067 See EN 4400-2. 100 Product qualif

25、ication Qualification programme to be agreed between manufacturer and purchaser. EN 4003:2006BS EN 4003:2006BSI389 Chiswick High RoadLondonW4 4ALBSI British Standards InstitutionBSI is the independent national body responsible for preparing British Standards. It presents the UK view on standards in

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