1、A.E.C.M.A. STANDARD 1 NORME A.E.C.M.A. prEN2692 Edition 1 A.E.C.M.A. NORM May 1985 O ENGLISH VERSION Aerospace series Aluminium alloy 201 7A-T3 clad sheet and strip 0,4da6mm Srie arospatiale Alliage daluminium 201 7A-T3 tles et bandes plaques 0,4 z W i- =! - Temperature Proof Stress & 370 I *. * 390
2、 I t 390 , I r, 390 Strength Elongatlon Reduction of area -i ard ness Shear Strength Bendlng Impact - a W W U u - Temperature Time Cr, a - MPa % - Stress Elongation MPE * Rupture Stress Elongatlon at rupture % *) 1 MPa = 1 N/mm2 l), i), see line 98 Notes Copyright Association Europeene des Construct
3、eurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEKS692 Page 4 1 Notes Typical use AECIA PREN2b92 85 .I LOL23LL 00039b4 O 1) Cladding .of- chmical composition conforming EN2072. 2): Alternatvely, values for A5.67 may be agreed between producer and purchaser. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-
