EN 3120:2012

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

This European Standard specifies the requirements relating to:
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
for aerospace applications.

Luft- und Raumfahrt - Titanlegierung TI-P64003 - Kaltverformt und spannungsarm geglüht - Nahtlose Innendruckrohre - 4 mm ≤ D ≤ 51 mm - 690 MPa ≤ Rm ≤ 1 030 MPa

Diese Norm legt die Anforderungen an Titanlegierung TI-P64003 Kaltverformt und spannungsarm geglüht Nahtlose Innendruckrohre 4 mm <+/- D <+/-  51 mm 690 MPa <+/- Rm <+/- 1 030 MPa für Anwendungen in der Luft- und Raumfahrt fest.

Série aérospatiale - Alliage de titane TI-P64003 - Étiré à froid et détensionné - Tube hydraulique sans soudure pour applications sous pression - 4 mm ≤ D ≤ 51 mm - 690 MPa ≤ Rm ≤ 1 030 MPa

Cette Norme européenne spécifie les exigences relatives à :
Alliage de titane TI-P64003
Étiré à froid et détensionné
Tube hydraulique sans soudure pour applications sous pression
4 mm  D  51 mm
690 MPa  Rm  1 030 MPa
pour applications aérospatiales.

Aeronavtika - Titanova zlitina TI-P64003 - Hladno preoblikovana in s popuščenimi napetostmi - Nevarjena cev za tlačne sisteme - 4 mm ≤ D ≤ 51 mm - 690 MPa ≤ Rm ≤ 1030 MPa

Ta evropski standard določa zahteve glede: titanove zlitine TI-P64003, hladno preoblikovane in s popuščenimi napetostmi, nevarjene cevi za tlačne sisteme 4 mm ≤ D ≤ 51 mm 690 MPa ≤ Rm ≤ 1030 MPa za uporabo v aeronavtiki.

General Information

• Status: Published
• Publication Date: 31-Jan-2012
• Withdrawal Date: 30-Aug-2012
• ICS: 49.025.30 - Titanium
• Technical Committee: ASD-STAN - Aerospace
• Drafting Committee: ASD-STAN/D 4 - Metallic
• Current Stage: 6060 - Definitive text made available (DAV) - Publishing
• Start Date: 01-Feb-2012
• Completion Date: 01-Feb-2012
• Ref Project: SIST EN 3120:2012 - 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

Standards Content (Sample)

2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.49.025.30TitanTitaniumICS:Ta slovenski standard je istoveten z:EN 3120:2012SIST EN 3120:2012en,de01-maj-2012SIST EN 3120:2012SLOVENSKI
STANDARD



SIST EN 3120:2012



EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 3120
February 2012 ICS 49.025.30 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
Série aérospatiale - Alliage de titane TI-P64003 - Étiré à froid et détensionné - Tube hydraulique sans soudure pour applications sous pression - 4 mm ≤ D ≤ 51 mm - 690 MPa ≤ Rm ≤ 1 030 MPa
Luft- und Raumfahrt - Titanlegierung TI-P64003 - Kaltverformt und spannungsarm geglüht - Nahtlose Innendruckrohre - 4 mm ≤ D ≤ 51 mm - 690 MPa ≤ Rm ≤ 1 030 MPa This European Standard was approved by CEN on 27 August 2011.
CEN members are bound to comply with the CEN/CENELEC Internal Regulations which 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-CENELEC Management Centre or to any CEN member.
This European Standard 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-CENELEC Management Centre has the same status as the official versions.
CEN members are the national standards 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, Turkey and United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION EUROPÄISCHES KOMITEE FÜR NORMUNG
Management Centre:
Avenue Marnix 17,
B-1000 Brussels © 2012 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 3120:2012: ESIST EN 3120:2012



EN 3120:2012 (E) 2 Contents Page Foreword .3 Introduction .4 1 Scope .4 2 Normative references .4
SIST EN 3120:2012



EN 3120:2012 (E) 3 Foreword This document (EN 3120:2012) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). After 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 national standard, either by publication of an identical text or by endorsement, at the latest by August 2012, and conflicting national standards shall be withdrawn at the latest by August 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 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, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the United Kingdom. SIST EN 3120:2012



EN 3120:2012 (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. 1 Scope This European Standard specifies the requirements relating to: 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 for aerospace applications. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the
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