1、-I E a I- a I w (3 v) oc 3 *w 3 w t; a mg w a W z Z W UJ a 3 w 2 2 2 t? 4 a: 0 o O a w !I o w O 6 - 1 AECMA PREN25l.7 83 l.OLi33l.l. 0003383 2 A.E.C.M.A. STANDARD NORME A.E.C.M.A. A.E.C.M.A. NORM prEN2517 Edition 1 January 1983 ENGLISH VERSION TITANIUM ALLOY TI-P63 ANNEALED SHEETS, STRIPS AND PLATES
2、 a/ 8 2, Elongation Reduction Hardness Shear Strength Bending 1050 a 6 3 mm : k = 5 kI - -I- Impact KI 1 Temperature w E I Elongation al % -I- Rupture Stress Elongation I at rupture i 1 MPa = 1 Nimm ) etermination not I) see line 98 : . N ot es Copyright Association Europeene des Constructeurs de Ma
3、teriel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,- . _- - - _ AECMA PREN2517 83 1012311 0003385 b prt kM7 Page 4 1 doter ypical use 2 3 4 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-,-,-
