1、/- _i A. E. C. M. A. STAN DARD prEN 3466 NORME A.E.C.M.A. Issue P 1 A.E.C.M.A. NORM March 1988 DIT PAR LASSOCIATION EUROPENNE DES CONSTRUCTEURS DE MATRIEL AROSPATIAL 88, boulevard Malesherbes, 75008 PARIS -TL. 45-63-82-85 UDC Key words : ENGLISH VERSION Aerospace series Titanium alloy TI-P68 Solutio
2、n treated and aged Rm3 1000 MPa Bar for machining DeG15mm Srie arospatiale Alliage de titane TI-P68 Mis en soution et revenu Rm, I000 MPa Barres pour usinage De, 1000 MPa Stangen De 960 - 920 - 870 1100 5 Rm 5 1280 1050 5 Rm 5 1220 - 9 - 9 - 9 - 25 - 20 - 20 1000 5 Rm 5 1200 - Strength R, MPa *) - U
3、I i- Elongation A5 % Reduction of area I- Hardness HB - Shear Strength R, MPa) Bending k- - - Impact IK I - Temperature I 8 1 Oc - h w w U O - NI Stress U, MPa *) - Elongation a % Elongotion .I 3s ine98 . Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under
4、 license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3466 Page 5 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 identif
5、ication code shall be as follows : Material standard number Letter code (see 6.2) Appropriate dimensional standard code (see 5.3) Data concerning dimension (see EN 2600) i) Determination not required for routine acceptance 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-,-,-
