1、A.E.C. M .A. STANDARD NORME A.E.C.M.A. A.E.C.M.A. NORM Edition approved for publication Comments should be sent within six months after the date of publication decision prEN 3528 Issue P 1 March 1988 C5 Chairman DIT PAR LASSOCIATION EUROPENNE DES CONSTRUCTEURS DE MATRIEL AROSPATIAL 88, boulevard Mal
2、esherbes, 75008 PARIS -TEL. 45-63-82-85 UDC : Key words : ENGLISH VERSION Aerospace series Steel FE-PA95 Solution treated and precipitation treated 1750 1650 - Lu -I - - 1750 6 4 - 75 - Strength R, MPa *) Lu - I- - Elongation A % Reduction of area * - 40 - - HB 5 352 I 510 5 HV 5 600 Hardness H - Sh
3、ear Strength R, MPa *) - end ino k- - Impact KCU J. - - - - 15 12 - Temperature 6 % - - Time t h - Stress Ua MPa *I - - - Elongation a % Rupture Stress Elongation at rupture - *) - - A% 1) I *) 1 MPa= 1 N/mm2 3) ins 98 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provide
4、d by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-1 Designation Notes Typical use 2 The rules governing the designation of semi-finished products are indicated in standard EN 2600. When the codified designation is used, the identifica
5、tion code shall be as follows : EN 352811 U 11 XX II- I Material standard number Data concerning dimension .(see EN 2600) I II I Letter code (see 6.2) I I Appropriate dimensional standard code (see 5.3) 1) Transverse where agreed between the manufacturer and purchaser. 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-,-,-
