EN 2100-1992 en Aerospace Series Aluminium Alloy AL-P2014A T4511 Extruded Bars and Sections a or D Less Than or Equal to 200 mm《航空航天系列 AL-P2014A-T4511铝合金 a D≤200挤压棒和型材》.pdf

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1、 CEN EN*E!100 92 W 3404589 O043668 BIT W EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 2100 September 1992 Um: 669.7 16-42: 629.7 Descriptors: Aircraft industry, metal bais, metal sections, aluminium alloys, specifications, chemical composition, dimensions, charactertistics English version Ae

2、rospace series Aluminium alloy AL-PZ014A T4511 Extruded bars and sections a or D 5 200 mm Srie arospatiale Alliage daluminium AL-P2014A T45ll Barres et profils fils a ou D 5 200 mni Luft- und Raumfahrt Aluminiumlegierung AL-PZO 14A T4511 StranggeprelJte Stangen und Profile a oder D I 200 mm This Eur

3、opean Standard was approved by CEN on 1992-03-09. CEN members are bound to comply with the CENKENELEC 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 concer

4、ning 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 translation under the responsibility of a CEN member into its own l

5、anguage and notified to the Central Secretariat has the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland a

6、nd United Kingdom. CEN European Committee for Standardization Comit Europen de Normalisation Europisches Komitee fr Normung Central Secretariat: rue de Stassart 36, B-1050 Brussels O 1992 Copyright reserved to CEN membeis Ref. Nr. EN 2100 : 1992 E CEN EN*2LOO 72 3404587 004Lbb7 756 Page 2 EN 2100 :

7、1992 Foreword This European Standard has been prepared by the European Association of Aerospace Manufacturers (AECMA). After inquiries and votes carried out in accordance with the rules of this Association, this Standard has successively received the approval of the National Associations and the Off

8、icial Services of the 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 March 1993, and conflicting national standards shall be withdrawn

9、 at the latest by March 1993. In accordance with the Common CENKENELEC Rules the following countries are bound to implement this European Standard: Austria, Belgium, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Noiway, Portugal, Spain, Sweden, Switzerl

10、and and United Kingdom. Page 3 EN 210 : 1992 O Introduction For the use of this standard, see EN 2500-2. 1 Scope This standard specifies the requirements relating to extruded bars and sections in aluminium alloy AL-P2014A, for use in the T4511 condition, a or D S 200 mrn, for aerospace applications.

11、 This standard may also be used to supply material in the T4510 condition, if the purchaser specifies this condition on the order. In this case the designation of line 97 shall not be used. 2 References This European Standard incorporates by dated or undated reference, provisions from other publicat

12、ions, These normative references are cited at the appropriate places in the text and the publications are listed hereafter. For dated references, subsequent amendments to or revisions of any of these publications apply to this European Stbndard only when incorporated in it by amendment or revision.

13、For undated references the latest edition of the publication referred to applies. EN 2047 EN 2048 EN 2049 EN 2050 EN 2070-3 EN 2134 EN 2341 EN 2500-2 EN 2600 Beaded L-section aluminium alloy extrusions - Dimensions - Aerospace series 2, L-section aluminium alloy extrusions - Dimensions - Aerospace s

14、eries 2, Channel section aluminium alloy extrusions - Dimensions - Aerospace series 2, T-section aluminium alloy extrusions - Dimensions - Aerospace series 2, Aerospace series - Aluminium and aluminium alloy wrought products - Technical specification - Pan 3 - Bars and sections Round aluminium alloy

15、 bars - Dimensions - Aerospace series Aluminium and aluminium alloy square and rectangular extruded bars - Dimensions - Aerospace series Aerospace series - Instructions for the drafting and use of metallic material standards - Part 2 - Specific requirements for aluminium, aluminium alloys and magnes

16、ium alloys 3, Aerospace series - DesiQnation of metallic semi-finished products - Rules 3), . Formerly incompletely designated as T45 1 . 3) Published as AECMA pre-standard at the date of publication of this standard. ;!r Published as AECMA standard at the date of publication of this standard. ._ .

17、CEN EN*ZLOO 92 W 3404589 004Lb7L 304 W 2 Page 4 EN 2100 : 1992 Chemicrl Elcmcni Si Fc Cu Mn Mg Cr Ni Zn Ti+Zr Ti Olhcll bch Toul- Al coqmition - - - Bare B min. 0.50 - 3.9 0,40 0,20 - mix. 0,9 OJO 5.0 1.2 0.8 0.10 0,lO 0.25 0.2Q 0,15 0.05 0.15 1 Miknil derinruiion 1 Aluminium alloy AL-P2014A 1 Mehod

18、 of rncliinp Form Mehod of production L.mii dimiuOfU (IlUIl) 5.1 Tochnicrl rpecificdon 5.2 bimeluionii rundirdi Ban and ieciiom . -de4 80rD S 200 EN 2070-3 EN 2047, EN 2048, EN 2049, EN 2050, EN 2134, EN 2341 i 6.1 Delivery condition rd hut Vulmcnt 6.2 Delivey condition code Ure condition and hui tm

19、tment T45 11 5w*c s e s 510 I WQ e s 4o*c + 1 I S siretched S 3 I rd minor rirrighlening rllowrblc + 8 = imbicntIt 2 5 d U 745 1 1 Delivery condition 8 Simple Tem picce Hui munent - - UK condition: T45 1 1 each face I Direction of ksi piece L - 9 Dimensionr conced iS2.5 2,5r510 10CaorDSZS 25CiorDS75

20、 7SiaD51XJ1) lSOiaDS1OO1) 17 - 10 hickneu of cladding on Tempenhire 8 *C Ambient iernpenmrc Proofiwcss v.2 MPi I 235 I 235 2 260 2 270 2 260 2 230 Strength 2 370 2 400 2 410 I 400 2 370 I345 R, MPi 5 Elongation A 5 211 2) 2 11 2, I 12 I 12 I12 28 Reduction % - 18 19 Shuruinnfi & MPi Bending k- 20 21

21、 22 - - I 77 Noies see line 98) kunul defccu ruenul dcfccm htch uniformity Deiigniiion Noler Typical use _ CEN EN*E!LOO 72 3404589 0041672 240 m Page 5 EN 2100: 1992 See EN 2070-3 Back end defects : see EN 2070-3 7 - See EN 2070-3 1 See EN 2070-3 7 Electrid conductivity y = 183 MSm (typid vaiue) or For extruded bars, see EN 2600. For extruded sections, see relevant drawing. 1) Bar only 2) or A, mm 2 10% I I I