EN 3310-2011 en Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Not heat treated - Forging stock for annealed forgings - De 360 mm《航空航天系列 TI-P64001(Ti-6AL-4V)型钛合金 无热处理 退火.pdf

《EN 3310-2011 en Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Not heat treated - Forging stock for annealed forgings - De 360 mm《航空航天系列 TI-P64001(Ti-6AL-4V)型钛合金 无热处理 退火.pdf》由会员分享，可在线阅读，更多相关《EN 3310-2011 en Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Not heat treated - Forging stock for annealed forgings - De 360 mm《航空航天系列 TI-P64001(Ti-6AL-4V)型钛合金 无热处理 退火.pdf（12页珍藏版）》请在麦多课文档分享上搜索。

1、raising standards worldwideNO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBSI Standards PublicationBS EN 3310:2011Aerospace series Titanium alloy TI-P64001 (Ti-6Al-4V) Not heat treated Forging stock, for annealed forgings De 360 mmBS EN 3310:2011 BRITISH STANDARDNational forew

2、ordThis British Standard is the UK implementation of EN 3310:2011. Itsupersedes BS3TA12:2009 which is withdrawn.The UK participation in its preparation was entrusted to TechnicalCommittee ACE/61/-/49, Titanium and its Alloys for AerospacePurposes.A list of organizations represented on this committee

3、 can beobtained on request to its secretary.This publication does not purport to include all the necessaryprovisions of a contract. Users are responsible for its correctapplication. BSI 2011ISBN 978 0 580 75191 2ICS 49.025.30Compliance with a British Standard cannot confer immunity fromlegal obligat

4、ions.This British Standard was published under the authority of theStandards Policy and Strategy Committee on 30 November 2011.Amendments issued since publicationDate Text affectedBS EN 3310:2011EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 3310 November 2011 ICS 49.025.30 English Version Aer

5、ospace 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 - De 360 mm Luft- und Raumfahrt - Titanleg

6、ierung TI-P64001 (Ti-6Al-4V) - Nicht wrmebehandelt - Schmiedevormaterial, fr geglhte Schmiedestcke - De 360 mm This European Standard was approved by CEN on 22 July 2011. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European

7、 Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the CEN-CENELEC Management Centre or to any CEN member. This European Standard exists in three official versions (E

8、nglish, French, German). A version in any other language made by translation under the responsibility of a CEN member into its own language and notified to the CEN-CENELEC Management Centre has the same status as the official versions. CEN members are the national standards bodies of Austria, Belgiu

9、m, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom. EUROPEAN COMMIT

10、TEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG Management Centre: Avenue Marnix 17, B-1000 Brussels 2011 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 3310:2011: EBS EN 3310:2011EN 3310:2011

11、 (E) 2 Contents Page Foreword 3 Introduction .4 1 Scope 5 2 Normative references 5 BS EN 3310:2011EN 3310:2011 (E) 3 Foreword This document (EN 3310:2011) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). After enquiries and votes carried o

12、ut in accordance with the rules of this Association, this Standard has received the approval of the National Associations and the Official Services of the member countries of ASD, prior to its presentation to CEN. This European Standard shall be given the status of a national standard, either by pub

13、lication of an identical text or by endorsement, at the latest by May 2012, and conflicting national standards shall be withdrawn at the latest by May 2012. Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. CEN and/or CENELEC shall

14、not be held responsible for identifying any or all such patent rights. According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmar

15、k, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and the United Kingdom. BS EN 3310:2011EN 3310:2011 (E) 4 Introduction This European St

16、andard is part of the series of EN metallic material standards for aerospace applications. The general organization of this series is described in EN 4258. This European Standard has been prepared in accordance with EN 4500-4. BS EN 3310:2011EN 3310:2011 (E) 5 1 Scope This European Standard specifie

17、s 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 following referenced documents are indispensable for the application of this document. For dated references, on

18、ly 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: Coding of metallurgical condition in delivery condition EN 2954-002, Aerospace series Macrostructure of titan

19、ium 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 wrought products Part 002: Microstructure of bars, sections, forging stock and forgings EN 4258, Aerospace ser

20、ies 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 presentation of material standards Part 4: Specific rules for titanium and titanium alloys 2)EN 4800-005, Aerospace s

21、eries 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 standard by Aerospace and Defence Industries Association of Europe-Standardization (ASD-STAN), (www.asd-stan.

22、org). BS EN 3310:2011EN 3310:2011 (E) 6 1 Material designation Titanium alloy TI-P64001 (Ti-6Al-4V) 2 Chemical composition % Element Al V O+2N N H Fe C YOthers Ti Each Total min. 5,50 3,50 Base max. 6,75 4,50 0,25 0,03 0,010 0 0,30 0,08 0,005 00,100,40 3 Method of melting Grade 2 see EN 4800-005. 4.

23、1 Form Forging stock 4.2 Method of production 4.3 Limit dimension(s) mm De 360 5 Technical specification EN 4800-005 6.1 Delivery condition Not heat treated Heat treatment 6.2 Delivery condition code Ua7 Use condition Delivery condition Heat treatment Characteristics 8.1 Test sample(s) See EN 4800-0

24、05. 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 T Temperature C Ambient 13 Proof stress Rp0,2MPa 830 14 Strength RmMPa 900 Rm 1 160 15 Elongation A % 1

25、0 16 Reduction of area Z % 25 17 Hardness 18 Shear strength RcMPa 19 Bending k 20 Impact strength 21 C Temperature C 22 Time h 23 Stress aMPa 24 Elongation a % 25 Rupture stress RMPa 26 Elongation at rupture A % 27 Notes (see line 98) aBS EN 3310:2011EN 3310:2011 (E) 7 29 Reference heat treatment An

26、nealed 690 C 840 C/t 30 min/AC or cool in inert atmosphere 30 Microstructure 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 2 T100 2 T10 to 2 T15 2 T101 to 2 T117 2 T200 to 2 T201 2 T101 50 D 110

27、 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 200 D 360 2 T1 to 2 T15 2 T100, 2 T 102 to 2 T111 2 T112 to 2 T117 2 T200 to 2 T201 44 External defects S

28、ee EN 4800-005. 51 Macrostructure 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 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 50 D 150 2 MA 3 150 D 250 2 MA 5 250 D 360 2 MA 6 61

29、 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 BS EN 3310:2011EN 3310:2011 (E) 8 100 Product qualification

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