1、ASD STANDARD NORME ASD ASD NORM prEN 3120 Edition P 3 October 2005 PUBLISHED BY THE AEROSPACE AND DEFENSE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATION Gulledelle 94 - B-1200 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 775 8111 - www.asd-stan.orgICS: Supersedes edition P 2 May 1996 Descriptor
2、s: ENGLISH VERSION Aerospace series Titanium alloy TI-P64003 Cold worked and stress relieved Seamless tube for pressure systems 4 mm D 51 mm 690 MPa Rm 1 030 MPa Srie arospatiale Alliage de titane TI-P64003 tir froid et dtensionn Tube hydraulique sans soudure pour applications sous pression 4 mm D 5
3、1 mm 690 MPa Rm 1 030 MPa Luft- und Raumfahrt Titanlegierung TI-P64003 kaltverformt und spannungsarm geglht nahtlose Innendruckrohre 4 mm D 51 mm 690 MPa Rm 1 030 MPa This “Aerospace Series“ Prestandard has been drawn up under the responsibility of ASD-STAN (The European Association of Aerospace Ind
4、ustries - Standardization). 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 pre-standard, the technical content shall not be changed to an extent
5、 that interchangeability 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 vot
6、e and transformation 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 31 October 2005 Comment
7、s should be sent within six months after the date of publication to ASD-STAN Metallic Material Domain Copyright 2005 by ASD-STAN Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted wit
8、hout license from IHS-,-,-prEN 3120:2005Foreword This standard was reviewed by the Domain Technical Coordinator of ASD-STANs Metallic Material Domain. After inquiries and votes carried out in accordance with the rules of ASD-STAN defined in ASD-STANs General Process Manual, this standard has receive
9、d approval for Publication. 2 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-,-,-prEN 3120:20053 Introduction This standard is part of the series of EN me
10、tallic 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. 1 Scope This standard specifies the requirements relating to: Titanium alloy TI-P64003 Cold worked and stress relieved
11、Seamless tube for pressure systems 4 mm D 51 mm 690 MPa Rm 1 030 MPa for aerospace applications. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the edition cited applies. For undated references, the latest
12、edition of the referenced document (including any amendments) applies. ISO 4288:1996, Geometrical Product Specifications (GPS) Surface texture: Profile method Rules and procedures for the assessment of surface texture. ISO 6772:1998, Aerospace Fluid systems Impulse testing of hydraulic hose, tubing
13、and fitting assemblies. EN 2043, Aerospace series Metallic materials General requirements for semi-finished product qualification (excluding forgings and castings). 1)EN 4258, Aerospace series Metallic materials General organization of standardization Links between types of EN standards and their us
14、e. EN 4500-4, Aerospace series Metallic materials Rules for drafting and presentation of material standards Part 4: Specific rules for titanium and titanium alloys. 1)EN 4800-3, Aerospace series Titanium and titanium alloys Technical specification Part 3: Tube. 1)SAE AS4076, Contractile strain ratio
15、 testing of titanium hydraulic tubing. 2)1) Published as AECMA Prestandard at the date of publication of this standard. 2) Published by: Department of Defense (DOD), the Pentagon, Washington, DC 20301, USA. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS und
16、er license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3120:20054 1 Material designation Titanium alloy TI-P64003 Others aElement Al V O2N2H2Fe C Each Total Ti min. 2,5 2,0 2 Chemical composition % max. 3,5 3,0 0,120 0,020 0,0150 0,30 0,05 0,10 0
17、,40 Base 3 Method of melting See EN 4800-3. 4.1 Form Seamless tube 4.2 Method of production 4.3 Limit dimension(s) mm 4 D 51 5 Technical specification EN 4800-3 Delivery condition Cold worked and stress relieved 6.1 Heat treatment 380 C 10 C / t 30 min / AC or inert atmosphere 6.2 Delivery condition
18、 code U Use condition Delivery condition 7 Heat treatment Characteristics 8.1 Test sample(s) See EN 4800-3. 8.2 Test piece(s) See EN 4800-3. 8.3 Heat treatment Use condition 9 Dimensions concerned mm 4 D 7 7 90 at a bend radius of 3D 95 Marking inspection See EN 4800-3. 96 Dimensional inspection See
19、 EN 4800-3. 98 Notes aDetermination not required for routine acceptance b2 additional bend tests required if 2,5 CSR 2,8 c2 pressure impulse fatigue tests per batch required only if 1,3 CSR 1,5 99 Typical use Pressure systems100 Product qualification See EN 2043. Qualification programme to be agreed between manufacturer and purchaser. 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-,-,-
