1、I ._ - . i- o e e * A.E.C.M.A. STANDARD NORME A. E.C. M .A. prEN 3530 issue P 1 A.E.C.M.A. NORM March 1988 EDITE PAR LASSOCIATION EUROPEENNE DES CONSTRUCTEURS DE MATERIEL AROSPATIAL 88, boulevard Malesherbes, 75008 PARIS - TEL. 4563-82-85 UDC : Key words : ENGLISH VERSION Aerospace series Steel FE-P
2、A95 Softened Reference heat treatment : solution treated and precipitation treated Forging stock De G 200 mm Srie arospatiale Acier FE-PA95 Adouci Traitement thermique de rfrence : mis en solution et prcipit Demi-produits destins la forge De 1650 1750 8 I Elongation I A I % Reduction of area 45 H sr
3、d ness 510 15 - b W UI U u - Na Temperature I(+ _/i- Stress U, MPs* - - Rupture Stress Elongation at tuptura * - A% - *) 1 MPa = 1 Nlmm2 OS me Ilne 98 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or ne
4、tworking permitted without license from IHS-,-,- AECMA - PREN3530 - 88 L1123LL 0406056 2 U- prEN 3530 Page 5 I 2 1 I e ference ieat treatment Designation Notes Typical use Solution treated and precipitation treated 810 t 10C / AC t precipitation trated 480 2 5OC / t = 4 h 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-,-,-
