Aerospace series - Titanium alloy Ti-4Al-4Mo-2Sn - Solution treated and aged - Forgings - De ≤ 150 mm

This European Standard specifies the requirements relating to:  )
Titanium alloy Ti-4Al-4Mo-2Sn
Solution treated and aged
Forgings
De < or = 150 mm
for aerospace application.
NOTE   Other designation: WL: 3.7184   
   Only the chemical composition of this standard must be considered.

Luft- und Raumfahrt - Titanlegierung Ti-4Al-4Mo-2Sn - Lösungsgeglüht und ausgelagert - Schmiedestücke - De ≤ 150 mm

Diese Norm legt die Anforderungen an )
Titanlegierung Ti-4Al-4Mo-2Sn
Lösungsgeglüht und ausgelagert
Schmiedestücke
De 150 mm
zur Anwendung in der Luft- und Raumfahrt fest.
Anmerkung:   Andere gültige Bezeichnungen:
Ti550,
AECMA: TI-P63,
ASD-STAN: TI-P63001.

Série aérospatiale - Alliage de titane Ti-4Al-4Mo-2Sn - Mis en solution et revenu - Pièces forgées ou matricées - De ≤ 150 mm

Cette Norme européenne spécifie les exigences relatives à :  )
Alliage de titane Ti-4Al-4Mo-2Sn
Mis en solution et revenu
Pièces forgées ou matricées
De 150 mm
pour applications aérospatiales.
NOTE   Autre désignation :
   Ti550,   
   AECMA : TI-P63,
   ASD-STAN : TI-P63001.

Aeronavtika - Titanova zlitina Ti-4Al-4Mo-2Sn - Topilno žarjena in starana - Kovani izdelki - De ≤ 150 mm

General Information

Status
Published
Publication Date
09-Oct-2012
Technical Committee
Drafting Committee
Current Stage
6060 - Definitive text made available (DAV) - Publishing
Due Date
09-Jun-1997

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2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.49.025.30TitanTitaniumICS:Ta slovenski standard je istoveten z:EN 3351:2012SIST EN 3351:2014en01-marec-2014SIST EN 3351:2014SLOVENSKI

STANDARD
SIST EN 3351:2014
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 3351
October 2012 ICS 49.025.30 English Version

Aerospace series - Titanium alloy Ti-4Al-4Mo-2Sn - Solution treated and aged - Forgings - De ≤ 150 mm

Série aérospatiale - Alliage de titane Ti-4Al-4Mo-2Sn - Mis en solution et revenu - Pièces forgées ou matricées - De ≤ 150 mm

Luft- und Raumfahrt - Titanlegierung Ti-4Al-4Mo-2Sn - Lösungsgeglüht und ausgelagert - Schmiedestücke - De ≤ 150 mm This European Standard was approved by CEN on 23 June 2012.

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, Former Yugoslav Republic of Macedonia, 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 3351:2012: ESIST EN 3351:2014

EN 3351:2012 (E) 2 Contents Page Foreword .............................................................................................................................................................. 3Introduction ......................................................................................................................................................... 41Scope ...................................................................................................................................................... 52Normative references ............................................................................................................................ 5 SIST EN 3351:2014

EN 3351:2012 (E) 3 Foreword This document (EN 3351:2012) 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 April 2013, and conflicting national standards shall be withdrawn at the latest by April 2013. 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 organisations of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, 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 3351:2014

EN 3351:2012 (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

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