1、AECMA PREN2389 81 10LS311 0003087 2 _ 3- _ - - - A. E.C.M. A. STANDARD prEN2389 NORME A.E.C.M.A. Edition 1 A.E.C.M.A. NORM September 1981 Approved by COMITG DE NORMALISATION Of A.E.C.M.A. 1980-11-21 ENGLISH VERSION The equivalent versions in French and German languages can be supplied by B.N.A.E., 8
2、, rue Moreau-Vauthier 92100 BOULOGNE-BILLANCOURT - FRANCE. ALUMINIUM ALLOY 6082-T4 TUBES FOR STRUCTURES 0,6 mm , 5 d T4 C :ondition ind ieat treatment Jse Delivery condition rest piece ieat treatment Sampling I a Imm 3imensions :oncerned . 0,6 & a 1,2 I 1,2 c a 4 6 6 c a Q 12,5 1% rhickness of :ladd
3、ing on each face Xrection of sample L L L ITemperature Room temperature Proof Stress -I 3 115 I a 115 3 115 5 215 I 215 3 215 Elongation Reduction of area Aardnen HEI - 90 (for information) Shear Strength 3ending Impact Temperature I Rupture Elongatton - *) 1MPe = 1N/mm2 i) in preparation. 21, 31, s
4、ee line 98. Noter Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN2389 Page 4 AECMA PREN2387 81 U L01231L 0003071 O m 1 Flattening test vote1 2 3 4
5、 E N2 002 - 1 O ) Z 6 2 a (if require.d by order) 1) In preparation. 2) Full section. 3) Cut-out section. I) B B b Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
