BS EN 2635-2005 Aerospace series - Aluminium alloy AL-P2014A - T6511 - Extruded bar and section - a or D 200 mm with peripheral coarse grain control《航空航天系列 AL-P2014A型铝合金 T6511 挤压棒材.pdf

1、 g49g50g3g38g50g51g60g44g49g42g3g58g44g55g43g50g56g55g3g37g54g44g3g51g40g53g48g44g54g54g44g50g49g3g40g59g38g40g51g55g3g36g54g3g51g40g53g48g44g55g55g40g39g3g37g60g3g38g50g51g60g53g44g42g43g55g3g47g36g58bar and section a or D k 200 mm with peripheral coarse grain controlThe European Standard EN 2635:2

2、005 has the status of a British StandardICS 49.025.20Aluminium alloy AL-P2014A T6511 Extruded BRITISH STANDARD AEROSPACE SERIESBS EN 2635:2005BS EN 2635:2005This British Standard was published under the authority of the Standards Policy and Strategy Committee on 18 November 2005 BSI 18 November 2005

3、ISBN 0 580 46846 1Cross-referencesThe British Standards which implement international or European publications referred to in this document may be found in the BSI Catalogue under the section entitled “International Standards Correspondence Index”, or by using the “Search” facility of the BSI Electr

4、onic Catalogue or of British Standards Online.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 does not of itself confer immunity from legal obligations.Summary of pagesThis d

5、ocument comprises a front cover, an inside front cover, the EN title page, pages 2 to 7 and a back cover.The BSI copyright notice displayed in this document indicates when the document was last issued.Amendments issued since publicationAmd. No. Date Commentsenquiries on the interpretation, or propos

6、als for change, and keep UK interests informed; monitor related international and European developments and promulgate them in the UK.A list of organizations represented on this subcommittee can be obtained on request to its secretary.National forewordThis British Standard is the official English la

7、nguage version of EN 2635:2005.The UK participation in its preparation was entrusted by Technical Committee ACE/61, Metallic materials for aerospace purposes, to Subcommittee ACE/61/-/24, Light alloys, which has the responsibility to: aid enquirers to understand the text; present to the responsible

8、international/European committee any EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 2635 October 2005 ICS 49.025.20 English Version Aerospace series - Aluminium alloy AL-P2014A - T6511 - Extruded bar and section - a or D 200 mm with peripheral coarse grain control Srie arospatiale - Alliage da

9、luminium AL-P2014A - T6511 - Barres et profils fils - a ou D 200 mm avec contrle de la zone priphrique gros grains Luft- und Raumfahrt - Aluminiumlegierung AL-P2014A - T6511 - Stranggeprete Stangen und Profile - a oder D 200 mm mit Kontrolle der Grobkornrandzone This European Standard was approved b

10、y CEN on 19 September 2005. 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 alteration. Up-to-date lists and bibliographical references concerning such national st

11、andards 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 translation under the responsibility of a CEN member into its own language and notified

12、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, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands,

13、 Norway, Poland, Portugal, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom. EUROPEAN COMMITTEE FOR 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 an

14、d by any means reserved worldwide for CEN national Members. Ref. No. EN 2635:2005: E2 Contents Page Foreword 3 Introduction4 1 Scope .4 2 Normative references .4 EN 2635:20053 Foreword This European Standard (EN 2635:2005) has been prepared by the European Association of Aerospace Manufacturers - St

15、andardization (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 the member countries of AECMA, prior to its presentation to CEN. This European Standar

16、d shall be given the status of a national standard, either by publication of an identical text or by endorsement, at the latest by April 2006, and conflicting national standards shall be withdrawn at the latest by April 2006. Attention is drawn to the possibility that some of the elements of this do

17、cument 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 organizations of the following countries are bound to implement this European Standard

18、: 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 the United Kingdom. EN 2635:20054 Introduc

19、tion 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 requirements relating to: Aluminiu

20、m alloy AL-P2014A T6511 Extruded bar and section a or D 200 mm with peripheral coarse grain control for aerospace applications. This standard may also be used to supply material for use in the T6510 condition if specified by the purchaser on the order and the product is marked accordingly. 2 Normati

21、ve references The following referenced documents are indispensable for the application of this document. 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

22、materials General organization of standardization Links between types of EN standards and their use. EN 4400-3, Aerospace series Aluminium and aluminium alloy wrought products Technical specification Part 3: Bar and section.1)EN 4500-2, Aerospace series Metallic materials Rules for drafting and pres

23、entation 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. EN 2635:20055 1 Material designation Aluminium alloy AL-P2014A Others Element Si Fe Cu Mn Mg Cr Ni Zn Ti Zr + T

24、i Each Total Al min. 0,50 3,9 0,40 0,20 2 Chemical composition % max. 0,9 0,50 5,0 1,2 0,8 0,10 0,10 0,25 0,15 0,20 0,05 0,15 Base 3 Method of melting 4.1 Form Bar and section 4.2 Method of production Extruded 4.3 Limit dimension(s) mm a or D 200 5 Technical specification EN 4400-3 Delivery conditio

25、n T4511 aT6511 6.1 Heat treatment 500 C 510 C / WQ 40 C + 1 % controlled stretched 3 % + = ambient / t 5 d 500 C 510 C / WQ 40 C + 1 % controlled stretched 3 % + 155 C 165 C / 12 h t 20 h or 170 C 180 C / 5 h t 12 h 6.2 Delivery condition code K U Use condition T6511 T6511 7 Heat treatment Delivery

26、condition 155 C 165 C / 12 h t 20 h or 170 C 180 C / 5 h t 12 h Delivery condition Characteristics 8.1 Test sample(s) See EN 4400-3. 8.2 Test piece(s) See EN 4400-3. 8.3 Heat treatment Use condition 9 Dimensions concerned mm a or D 2,5 2,5 a or D 10 10 a or D 25 25 a or D 75 75 a or D 100 100 a or D

27、 150 150 a or D 200 10 Thickness of cladding on each face % 11 Direction of test piece L L L L L L L 12 Temperature C Ambient Ambient Ambient Ambient Ambient Ambient Ambient 13 Proof stress Rp0,2MPa 370 385 415 440 435 420 390 14 Strength RmMPa 415 435 460 490 480 465 435 15 Elongation A % A50 mm 7

28、A50 mm 7 7 7 7 7 7 16 T Reduction of area Z % 17 Hardness 18 Shear strength RcMPa 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) aEN 2635:20056 44 External defects See EN 4400-3.

29、 61 Internal defects See EN 4400-3. 82 Batch uniformity See EN 4400-3.7 T4511 T6511 Electrical conductivity MS/m 18,5 (Typical value) 22,0 (Typical value) or 115 (Typical value) 135 (Typical value) 7 16 per product 20 per product Hardness HB 24 per batch 30 per batch 87 Extrusion back-end defect See

30、 EN 4400-3. 88 Peripheral coarse grain See EN 4400-3. 7 Level A95 Marking inspection See EN 4400-3. 96 Dimensional inspection See EN 4400-3. 98 Notes aT4510 if the use condition is T6510. 99 Typical use EN 2635:20057 100 Product qualification See EN 4400-3. Qualification programme to be agreed betwe

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