EN 2402:2014
(Main)Aerospace series - Heat resisting nickel base alloy NiCr20Co3Fe3 - Annealed - Wire - D ≤ 10 mm
Aerospace series - Heat resisting nickel base alloy NiCr20Co3Fe3 - Annealed - Wire - D ≤ 10 mm
This European Standard specifies the requirements relating to: Heat resisting nickel base alloy NiCr20Co3Fe3 Annealed Wire D ≤ 10 mm
for aerospace applications.
NOTE Other designation: Only the chemical composition of this standard must be considered.
Luft- und Raumfahrt - Hochwarmfeste Nickelbasislegierung NiCr20Co3Fe3 - Geglüht - Draht - D ≤ 10 mm
Diese Norm legt die Anforderungen an
Hochwarmfeste Nickelbasislegierung NiCr20Co3Fe3
Geglüht
Draht D ≤ 10 mm
zur Anwendung in der Luft- und Raumfahrt fest.
ANMERKUNG Weitere übliche Bezeichnungen:
Es muss nur die chemische Zusammensetzung dieser Norm beachtet werden.
Série aérospatiale - Alliage résistant à base de nickel NiCr20Co3Fe3 - Requit - Fil - D ≤ 10 mm
Aeronavtika - Toplotnoodporna zlitina na osnovi niklja NiCr20Co3Fe3 - Žarjena - Žica - D ≤ 10 mm
EN 2402 določa zahteve glede: žarjene žice D ≤ 10 mm iz toplotnoodporne zlitine na osnovi niklja NiCr20Co3Fe3 za uporabo v aeronavtiki.
General Information
Standards Content (Sample)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.49.025.15Neželezove zlitine na splošnoNon-ferrous alloys in generalICS:Ta slovenski standard je istoveten z:EN 2402:2014SIST EN 2402:2014en,fr,de01-julij-2014SIST EN 2402:2014SLOVENSKI
STANDARD
SIST EN 2402:2014
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 2402
April 2014 ICS 49.025.15 English Version
Aerospace series - Heat resisting nickel base alloy NiCr20Co3Fe3 - Annealed - Wire - D ≤ 10 mm
Série aérospatiale - Alliage résistant à base de nickel NiCr20Co3Fe3 - Requit - Fil - D ≤ 10 mm
Luft- und Raumfahrt - Hochwarmfeste Nickelbasislegierung NiCr20Co3Fe3 - Geglüht - Draht - D ≤ 10 mm This European Standard was approved by CEN on 27 December 2013.
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
CEN-CENELEC Management Centre:
Avenue Marnix 17,
B-1000 Brussels © 2014 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 2402:2014 ESIST EN 2402:2014
EN 2402:2014 (E) 2 Contents
Page coreword .3 Introduction .4 1 Scope .5 2 kormative references .5 SIST EN 2402:2014
EN 2402:2014 (E) 3 coreword This document (EN 2402:2014) 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 October 2014, and conflicting national standards shall be withdrawn at the latest by October 2014. 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, 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 2402:2014
EN 2402:2014 (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 4500-003. SIST EN 2402:2014
EN 2402:2014 (E) 5 1 Scope This European Standard specifies the requirements relating to: Heat resisting nickel base alloy NiCr20Co3Fe3 Annealed Wire D ≤ 10 mm for aerospace applications. NOTE Other designation:
Only the chemical composition of this standard must be considered. 2 kormative references The following documents, in whole or in part, are normatively referenced in this document and are indispensable for its application.
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