ASD-STAN PREN 3860-1993 Aerospace Series Titanium Alloy TI-P19001 Annealed Sheet and Strip Cold Rolled a Less Than or Equal to 6 mm (Edition P 1)《航空航天系列 钛合金TI-P19001制a≤6mm的冷轧经退火处理的.pdf

1、CEN PRENs3860 93 3404587 004Li710 656 m Edition approved for publication AECMA STANDARD NORME AECMA AECMA NORM C5 Chairman Comments should be sent within six months after the date of publication to prEN 3860 Edition P 1 April 1993 EDITE PAR LASSOCIATION EUROPEENNE DES CONSTRUCTEURS DE MATERIEL AEROS

2、PATIAL Technopolis - 175, rue Jean-Jacques Rousseau - F-92138 Issy-les-Moulineaux Cedex - Tl. i1 i 47.36.98.76 UDC : Descriptors : ENGLISH VERSION Aerospace series Titanium alloy TI-PI 9001 Annealed Sheet and strip, cold rolled a56mm Srie arospatiale Alliage de titane TI-Pl9001 Recuit Tles et bandes

3、, lamines froid aI6mm Luft- und Raumfahrt Titanlegierung TI-Pl9001 Geglht Bleche und Bnder, kaltgewalzt aI6mm This “Aerospace Series“ Prestandard has been drawn up under the responsibility of AECMA (Association Europenne des Constructeurs de Matriel Arospatial). It is published on green paper for th

4、e needs of AECMA-Members. It has been technically approved by the experts of the concerned Technical Committee following comment by the Member countries. Subsequent to the publication of this prestandard, the technical content shall not be changed to an extent that interchangeability is affected, ph

5、ysically or functionally, without re-identification of the standard. After examination and signature of the AECMA Standard Checking Centre (NPS) and formal agreement of the Official Services of the Member countries it will be submitted as a draft European Standard to CEN (European Committee for Stan

6、dardization) for formal vote. 1993-04-26 AECMA Technopolis - 175, rue Jean-Jacques Rousseau 921 38 Issy-les-Moulineaux Cedex - FRANCE M. ODORICO I I aecma 199 COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesCEN PREN+3860 93 m 3404589 00

7、44733 592 m prEN 3860 Page 3 O Introduction For the use of this standard, see EN 2500-4. 1 Scope and field of application This standard specifies the requirements relating to sheet and strip, cold rolled, a I6 mm, annealed, in titanium alloy TI-Pl9001 for aerospace applications. 2 References EN 2339

8、 EN 2500-4 EN 2600 EN 3544-1 EN 3544-2 Sheets, titanium and titanium alloys - Cold rolled - Thickness 0,2 mm I a I 3 mm - Dimensions - Aerospace series Aerospace series - Instructions for the drafting and use of metallic material standards - Part 4 - Specific requirements for titanium and titanium a

9、lloys 2, Aerospace series - Designation of metallic semi-finished products - Rules 2, Aerospace series - Titanium and titanium alloys - Wrought products - Technical specification - Part 1 - General requirements 3, Aerospace series - Titanium and titanium alloys - Wrought products - Technical specifi

10、cation - Part 2 - Plate, sheet and strip 3, 1) Published as AECMA standard at the date of publication of this standard 2) Published as AECMA pre-standard at the date of publication of this standard 3) In preparation at the date of publication of this standard Previous page is blank COPYRIGHT Associa

11、tion Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling ServicesCEN PRENx3860 93 m 3404589 0044712 429 m 1 2 3 4 5 prEN 3860 Page 4 Material designation Chemical Element composition min. % max. Method of melting Form Method of production Limit dimensions (mm) 5.1 Techn

12、ical specification 5.2 Dimensional standards Cu O2 Np Titanium alloy TI - PI9001 Hq Fe C Others Ti Each I Total 2,Ol - I - I - I - I - I - I 3,O I 0,20 I 0,05 I 0,0125 I 0,20 0,08 I 0,lO) I 0,40 1 Base See EN 3544-1 Sheet and strip Cold rolled as6 6 6.1 Delivery condition and heat treatment 6.2 Deli

13、very condition code 7 Usecondition and heat treatment EN 3544-2 Annealed 780 “C s e s 820 “C / t 2 20 min I AC or inert atmosphere U Delivery condition EN 2339 25 26 27 - Rupturestress OR MPa Elongation at A% rupture Notes (see line 98) 1) COPYRIGHT Association Europeene Des Constructeurs de Materie

14、l AerospaceLicensed by Information Handling ServicesCEN PRENx38bO 93 m 3404589 0044733 3b5 m prEN 3860 Page 5 ixternal defects ;utface contamination Designation Notes Typical use I See EN 3544-2 See EN 3544-2 6 5 mm a 16 rnrn See EN 2600 1) Determination not required for routine acceptance COPYRIGHT Association Europeene Des Constructeurs de Materiel AerospaceLicensed by Information Handling Services