1、CEN EN+2384 92 = 3404589 0033497 735 EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 2384 September 1992 UDC 669.715-42629.7 Descriptors: Aircraft industry, metal bars, metal sections, aluminium alloys, specifications, chemical composition, dimensions, characteristics English version Aerospace
2、series Aluminium alloy AL-P2014A T6511 Extruded bars and sections a or D 5 150 mm Srie arospatiale Luft- und Raumfahrt Alliage daluminium AL-PZ014A T6511 Barres et profils fils a ou D I 150 mm Aluminiumlegierung AL-P2014A T6511 Stranggeprete Stangen und Profile a oder D I 150 mm This European Standa
3、rd was accepted by CEN on 1992-03-09. CEN members are bound to comply with the requirements of CEN 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 concernin
4、g such national standards may be obtained on application to the CEN 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
5、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, Denmark, Finland, France, Germany, Greece, Iceland, Lreland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland
6、and 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 members Ref. No. EN 2384 : 1992 E CEN ENI2384 92 = 3404589 0033498 671 Page 2 EN 2384
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
8、Official 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 withdr
9、awn at the latest by March 1993. In accordance with the Common CENICENELEC Rules the following countries are bound to implement this European Standard: Austria, Belgium, Denmark, Finland, France, Germany, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Swit
10、zerland and United Kingdom. CEN ENx2384 92 = 3404589 0033499 508 D Page 3 EN 2384 : 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 T6511 condition, a
11、or D s 150 mm, for aerospace applications. This standard may also be used to supply material in the T6510 or T4510 condition if the purchaser specifies this condition on the order. In this case the designation of line 97 shall not be used. 2 Ref trences This European Standard incorporates by dated o
12、r undated reference, provisions from other publications. 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 Standard only
13、 when incorporated in it by amendment or revision. 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 L-section alumi
14、nium alloy extrusions - Dimensions - Aerospace series Channel section aluminium alloy extrusions - Dimensions - Aerospace series T-section aluminium alloy extrusions - Dimensions - Aerospace series Aerospace series - Aluminium and aluminium alloy wrought products - Tec. .niCa specification - Part 3
15、- Bars and sections Round aluminium alloy 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 f
16、or aluminium, aluminium alloys and magnesium alloys Aerospace series - Designation of metallic semi-finished products - Rules z). 1) Published as AECMA standard at the date of publication of this standard. 2) Published as AECMA pre-standard at the date of publication of this standard. CEN EN*:2384 9
17、2 3404589 0033500 05T I Ma&nrl dcrignrtion 2 Chernid Eicmcnt composition % min. nux. 3 Mcthdofmehing 4 Form Mew of pduction Ud1 dimenaions (mm) 5 5.1 Technic.al apecificiiion 5.2 Dimensional irrdarda Page 4 EN 2384 : 1992 Aluminium rlloy AL-PZOI 4A Si Fe Cu Mn Mg Cr Ni Zn Ti+Zr Ti Men Each Tau1 Al -
18、 - oso - 3.9 0,)o 0,20 - , Biw 0.9 OJO 5,0 1.2 0.8 0,iO 0.10 0.25 0.20 0,lS 0,OS 0,lS IIrn and YCLIOIU Extruded rorD S i50 EN 2070-3 EN 2047, EN 2048. EN 2049, EN 2050, EN 2134, EN mi 6.1 Delivery condiiion and hut trsrimcnt 6.2 Delivery condition code Ur condiiion and hui irutmeni T451 I SOOT s e s
19、 sio*c t WQ e s 40.c + 1 % s arciched S 3 % and minor tlnightening rliowabie + 8 = ambient I I 2 5 d K Delivery condiiion + iSS*C S 8 S 165.C I 12 h S t S 20 h or 170T S 8 S 180T I 5 h S i 5 12 h T6511 SOOT s e s 510.c I WQ e s UI*C +l%SurccMS 3% and minor anightening ailowable + ISST S 8 S i65.C I1
20、2 h S I S 20 h or i70C s 8 S 180.C I 5 h S t S 12 h U II Delivery condition Chrncteririicr 8 Simple Tea piece Hui vutmcni Dimenaions concemcd Thickmu of ckdding on UIC condiiion:T6Sii I mm I I a S 2.5 I 2.5 C a 5 IO I IO C .or D S 2S 1 25 iorD S 7S I 75 c .orb S IOD1) I lu) c aorD 5 1s ), I L I I i
21、1 1 Direction of tem piccc 16 19 hf mrrar Reduction I ofam I HardllCSS Shur arcngth Bending Lnpaci mrrngth 1 e Tim Strcsr Ca C Uongaiion a Rupiurc mrcas UR iongriion ai A nipiurc “I I 27 I Noies (see line 98) 1 I CEN ENx23AQ 92 3QOQ589 0033503 T9b Page 5 EN 23% : 1992 Noter Typic81 UY Set EN 2070-3
22、7 Back end defects : see EN 2070-3 See EN 2070-3 1 See EN 2070-3 5 T45 11 T65 1 1 7 Electrical conductivity y = 18.5 MS/m (typical vrlue) y - 22 MSlm (typical value) or Hrrdness 1 IS HB (typical vrlue) 6 5 16 HB per product 135 HB (typical value) 4 20 HB per product I I A S 24 HB per ntch A 4 30 HB per batch For extruded bars, see EN 2600. For extruded sections, see relevant drnwing. i) Bar only 2) or Aso mm 2 6%
