ASD-STAN PREN 3310-2010 Aerospace series Titanium alloy TI-P64001 (Ti-6Al-4V) Not heat treated Forging stock for annealed forgings De Less than or equal to 360 mm (Edition P 3).pdf

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1、ASD-STAN STANDARD NORME ASD-STAN ASD-STAN NORM prEN 3310 Edition P 3 September 2010 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATIONAvenue de Tervuren, 270 - B-1150 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 775 8131 - www.asd-stan.orgICS: Supersedes editi

2、on P 2 of September 1995 Descriptors: ENGLISH VERSION Aerospace series Titanium alloy TI-P64001 (Ti-6Al-4V) Not heat treated Forging stock, for annealed forgings De 360 mm Srie arospatiale Alliage de titane TI-P64001 (Ti-6Al-4V) Non trait Demi-produits destins la forge, pour pices forges ltat recuit

3、 De 360 mm Luft- und Raumfahrt Titanlegierung TI-P64001 (Ti-6Al-4V) Nicht wrmebehandelt Schmiedevormaterial, fr geglhte Schmiedestcke De 360 mm This “Aerospace Series“ Prestandard has been drawn up under the responsibility of ASD-STAN (The AeroSpace and Defence Industries Association of Europe - Sta

4、ndardization). It is published for the needs of the European Aerospace Industry. It has been technically approved by the experts of the concerned Domain following member comments. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that intercha

5、ngeability is affected, physically or functionally, without re-identification of the standard. After examination and review by users and formal agreement of ASD-STAN, it will be submitted as a draft European Standard (prEN) to CEN (European Committee for Standardization) for formal vote and transfor

6、mation to full European Standard (EN). The CEN national members have then to implement the EN at national level by giving the EN the status of a national standard and by withdrawing any national standards conflicting with the EN. Edition approved for publication 1 September 2010 Comments should be s

7、ent within six months after the date of publication to ASD-STAN Metallic Material Domain Copyright 2010 by ASD-STAN prEN 3310:2010 (E) 3 Introduction This standard is part of the series of EN metallic material standards for aerospace applications. The general organization of this series is described

8、 in EN 4258. This standard has been prepared in accordance with EN 4500-4. 1 Scope This standard specifies the requirements relating to: 1)Titanium alloy TI-P64001 (Ti-6Al-4V) Not heat treated Forging stock, for annealed forgings De 360 mm for aerospace applications. 2 Normative references The follo

9、wing referenced documents are indispensable for the application of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 2032-2, Aerospace series Metallic materials Part 2: Cod

10、ing of metallurgical condition in delivery condition EN 2954-002, Aerospace series Macrostructure of titanium and titanium alloy wrought products Part 002: Macrostructure of bar, section, forging stock and forgings EN 3114-002, Aerospace series Test method Microstructure of ( + ) titanium alloy wrou

11、ght products Part 002: Microstructure of bars, sections, forging stock and forgings EN 4258, Aerospace series Metallic materials General organization of standardization Links between types of EN standards and their use EN 4500-4, Aerospace series Metallic materials Rules for drafting and presentatio

12、n of material standards Part 4: Specific rules for titanium and titanium alloys2) EN 4800-005, Aerospace series Titanium and titanium alloys Technical specification Part 005: Forging stock 2)1) Grade 2 according to EN 4800-005. 2) Published as ASD-STAN Standard at the date of publication of this sta

13、ndard by Aerospace and Defence Industries Association of Europe-Standardization (ASD-STAN), (www.asd-stan.org). prEN 3310:2010 (E) 4 1 Material designation Titanium alloy TI-P64001 (Ti-6Al-4V) Others Element Al V O+2N N H Fe C YEach Total Ti min. 5,50 3,50 2 Chemical composition % max. 6,75 4,50 0,2

14、5 0,03 0,010 0 0,30 0,08 0,005 00,100,40 Base 3 Method of melting Grade 2 see EN 4800-005. 4.1 Form Forging stock 4.2 Method of production 4.3 Limit dimension(s) mm De 360 5 Technical specification EN 4800-005 Delivery condition Not heat treated 6.1 Heat treatment 6.2 Delivery condition code U aUse

15、condition Delivery condition 7 Heat treatment Characteristics 8.1 Test sample(s) See EN 4800-005. 8.2 Test piece(s) Heat treated before machining 8.3 Heat treatment See line 29. 9 Dimensions concerned mm 10 Thickness of cladding on each face % 11 Direction of test piece See EN 4800-005. 12 Temperatu

16、re C Ambient 13 Proof stress Rp0,2 MPa 830 14 Strength Rm MPa 900 Rm 1 160 15 Elongation A % 10 16 T Reduction of area Z % 25 17 Hardness 18 Shear strength Rc MPa 19 Bending k 20 Impact strength 21 Temperature C 22 Time h 23 Stress a MPa 24 Elongation a % 25 Rupture stress R MPa 26 C Elongation at r

17、upture A % 27 Notes (see line 98) aprEN 3310:2010 (E) 5 29 Reference heat treatment Annealed 690 C 840 C / t 30 min / AC or cool in inert atmosphere See EN 4800-005. 1 EN 3114-002 7 Demm Acceptable microstructure Not acceptable microstructure To be submitted for approval 50 2 T1 to 2 T9 occasionally

18、 2 T100 2 T10 to 2 T15 2 T101 to 2 T117 2 T200 to 2 T201 50 D 110 2 T1 to 2 T12 occasionally 2 T13 to 2 T14, 2 T100, 2 T102 2 T15 2 T103 to 2 T117 2 T200 to 2 T201 110 D 200 2 T1 to 2 T12 occasionally 2 T100, 2 T102 to 2 T109 2 T110 to 2 T117 2 T200 to 2 T201 30 Microstructure 200 D 360 2 T1 to 2 T1

19、5 2 T100, 2 T 102 to 2 T111 2 T112 to 2 T117 2 T200 to 2 T201 2 T101 44 External defects See EN 4800-005. See EN 4800-005. 1 EN 2954-002 7 Demm Maximum acceptable macrostructure Not acceptable macrostructure To be submitted for approval 50 2 MA 2 50 D 150 2 MA 3 150 D 250 2 MA 5 51 Macrostructure 25

20、0 D 360 2 MA 6 2 MA 80 to 2 MA 84 and 2 MA 100 2 MA 40 to 2 MA 42and 2 MA 60 to 2 MA 62 61 Internal defects See EN 4800-005. 1 EN 4050-4 82 Batch uniformity (Material verification) See EN 4800-005. 95 Marking inspection See EN 4800-005. 96 Dimensional inspection See EN 4800-005. 98 Notes a According to EN 2032-2. 99 Typical use prEN 3310:2010 (E) 6 100 Product qualification See EN 4800-005. Qualification programme to be agreed between manufacturer and purchaser.