BS EN 3459-2010 Aerospace series - Titanium alloy TI-P63001 (Ti-4Al-4Mo-2Sn) - Solution treated and aged - Plate - 6 mm a 50 mm《航空航天系列 TI-P63001(Ti-4Al-4Mo-2Sn)钛合金 经溶解处理和老化处理的6 mm .pdf

1、BS EN 3459:2010ICS 49.025.30NO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBRITISH STANDARDAerospace series Titanium alloy TI-P63001 (Ti-4Al-4Mo-2Sn) Solution treated and aged Plate 6 mm a null 50 mmThis British Standard was published under the authority of the Standards Polic

2、y and Strategy Committee on 31 May 2010. BSI 2010ISBN 978 0 580 65923 2Amendments/corrigenda issued since publicationDate CommentsBS EN 3459:2010National forewordThis British Standard is the UK implementation of EN 3459:2010. Together with BS 2TA 57:2009, it supersedes BS TA 57:1974 which is withdra

3、wn.BS EN 3459:2010 covers plate in the thickness range 6 mm to 50 mm, and BS 2TA57:2009 covers plate in the thickness range 50 mm to 65 mm. The UK participation in its preparation was entrusted to Technical Committee ACE/61/-/49, Titanium and its Alloys for Aerospace Purposes.A list of organizations

4、 represented on this committee can be obtained on request to its secretary.This publication does not purport to include all the necessary provisions of a contract. Users are responsible for its correct application.Compliance with a British Standard cannot confer immunity from legal obligations.BS EN

5、 3459:2010EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 3459 April 2010 ICS 49.025.30 English Version Aerospace series - Titanium alloy TI-P63001 (Ti-4Al-4Mo-2Sn) -Solution treated and aged - Plate - 6 mm a 50 mm Srie arospatiale - Alliage de titane TI-P63001 (Ti-4Al-4Mo-2Sn) - Mis en solutio

6、n et revenu - Plaques - 6 mm a 50 mm Luft- und Raumfahrt - Titanlegierung TI-P63001 (Ti-4Al-4Mo-2Sn) - Lsungsgeglht und ausgelagert - Platten - 6 mm a 50 mm This European Standard was approved by CEN on 16 January 2010. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which

7、stipulate the conditions for giving this European 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 Management Centre or to any CEN member. This European Stan

8、dard exists in three official versions (English, 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 Management Centre has the same status as the official versions. CEN members are the national st

9、andards bodies of Austria, Belgium, 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 an

10、d United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG Management Centre: Avenue Marnix 17, B-1000 Brussels 2010 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 3459:2

11、010: EBS EN 3459:2010EN 3459:2010 (E) 2 Contents Page Foreword 3Introduction . 41 Scope 52 Normative references 5BS EN 3459:2010EN 3459:2010 (E) 3 Foreword This document (EN 3459:2010) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). After

12、 enquiries and votes carried out 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 na

13、tional standard, either by publication of an identical text or by endorsement, at the latest by October 2010, and conflicting national standards shall be withdrawn at the latest by October 2010. Attention is drawn to the possibility that some of the elements of this document may be the subject of pa

14、tent rights. CEN and/or CENELEC shall 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, C

15、roatia, 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 the United Kingdom. BS EN 3459:2010EN 3459:20

16、10 (E) 4 Introduction This standard 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 standard has been prepared in accordance with EN 4500-4. BS EN 3459:2010EN 3459:2010 (E) 5 1 Scope This standa

17、rd specifies the requirements relating to: Titanium alloy TI-P63001 (Ti-4Al-4Mo-2Sn) Solution treated and aged Plate 6 mm a 50 mm for aerospace applications. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only t

18、he edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 2043, Aerospace series Metallic materials General requirements for semi-finished product qualification (excluding forgings and castings) EN 3114-003, Aerospace serie

19、s Test method Microstructure of ( + ) titanium alloy wrought products Part 003: Microstructure of plate EN 4050-1, Aerospace series Test method for metallic materials Ultrasonic inspection of bars, plates, forging stock and forgings Part 1: General requirements EN 4050-4, Aerospace series Test metho

20、d for metallic materials Ultrasonic inspection of bars, plates, forging stock and forgings Part 4: Acceptance criteria 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

21、 Rules for drafting and presentation of material standards Part 4: Specific rules for titanium and titanium alloys EN 4800-001, Aerospace series Titanium and titanium alloys Technical specification Part 001: Plate, sheet and strip BS EN 3459:2010EN 3459:2010 (E) 6 1 Material designation Titanium all

22、oy TI-P63001 (Ti-4Al-4Mo-2Sn) 2 Chemical composition % Element AI Mo Si Sn O N H C Fe Others 1) Ti Each Total min. 3,0 3,0 0,3 1,5 _ _ _ _ _ _ Base max. 5,0 5,0 0,7 2,5 0,25 0,03 0,0125 0,08 0,20 0,10 0,40 3 Method of melting See EN 4800-001 4.1 Form Plate 4.2 Method of production Wrought 4.3 Limit

23、dimension(s) mm 6 a 50 5 Technical specification EN 4800-001 6.1 Delivery condition Solution treated and aged Heat treatment 900 C 10 C/t 20 min/AC + 500 C 10 C/t = 24 h/AC 6.2 Delivery condition code U 7 Use condition Delivery condition Heat treatment _ Characteristics 8.1 Test sample(s) EN 4800-00

24、1 8.2 Test piece(s) EN 4800-001 8.3 Heat treatment Delivery condition 9 Dimensions concerned mm 6 a 40 40 a 50 10 Thickness of cladding on each face % _ 11 Direction of test piece L LT L LT ST 12 T Temperature C Ambient 13 Proof stress Rp0,2 MPa 900 920 900 920 900 14 Tensile strength Rm MPa 1 030 R

25、m 1 220 1 030 Rm 1 220 1 030 Rm 1 220 1 030 Rm 1 220 1 030 Rm 1 22015 Elongation A % 9 9 9 9 7 16 Reduction of area Z % 20 20 20 20 20 17 Hardness _ 18 Shear strength Rc MPa _ 19 Bending k _ 20 Impact strength _ 21 C Temperature C _ 22 Time h _ 23 Stress a MPa _ BS EN 3459:2010EN 3459:2010 (E) 7 24

26、Elongation a % _ 25 Rupture stress R MPa _ 26 Elongation at rupture A % _ 27 Notes (see line 98) 1) 30 Microstructure See EN 4800-001 1EN 3114-003 7 a (mm) Acceptable microstructure Unacceptable microstructure 6 a 30 3 T 1 to 3 T 19 3 T 20 and 3 T 21 3 T 22 to 3 T 27 3 T 28 to 3 T 30 3 T 31 to 3 T 3

27、3 3 T 34 to 3 T 38 3 T 100 and 3 T 101, if incidence less than 5 per cm of the sampling section 3 T 100 and 3 T 101, if incidence of 5 or more per cm of the sampling section _ 3 T 102 to 3 T 106 3 A 1 to 3 A 8 _ _ 3 T 200 to 3 T 202 30 a 50 3 T 1 to 3 T 19 3 T 20 and 3 T 21 3 T 22 to 3 T 38 _ 3 T 10

28、0 to 3 T 102 3 T 103 and 3 T 104 3 T 105 _ 3 T 106; if incidence less than 5 per cm of the sampling section 3 T 106; if incidence of 5 or more per cm of the sampling section 3 A 1 to 3 A 8 _ _ 3 T 200 to 3 T 202 44 External defects _ See EN 4800-001 61 Internal defects _ See EN 4800-001 1 EN 4050-1

29、7 Class 5 of EN 4050-4 74 Surface contamination _ See EN 4800-001 95 Marking inspection _ See EN 4800-001 96 Dimensional inspection _ See EN 4800-001 98 Notes _ 1) Determination not required for routine acceptance 99 Typical use _ _ 100 Product qualification Qualification programme to be agreed betw

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