SIST EN 3243:2004

Aerospace series - Pipe coupling 8°30' in titanium alloy - Ferrules, welded, with dynamic beam seal end

This standard specifies the characteristics of welded ferrules with dynamic beam seal end for pipe couplings 8°30', in titanium alloy, for aerospace applications.
Nominal pressure: up to 28 000 kPa
Temperature range: - 55 °C to 135 °C

Luft- und Raumfahrt - Rohrverschraubung 8°30' aus Titanlegierung - Anschweißstutzen mit Dichtlippe

Diese Norm legt die Eigenschaften von Anschweißstutzen mit Dichtlippe für Rohrverschraubungen 8°30', aus Titanlegierung, zur Verwendung in der Luft- und Raumfahrt fest.
Nenndruck: bis 28 000 kPa
Temperaturbereich: - 55 °C bis 135 °C

Série aérospatiale - Systeme de raccordement 8°30' en alliage de titane - Olives a souder avec joint a levre

La présente norme spécifie les caractéristiques des olives a souder, avec joint a levre, pour les systemes de raccordement 8°30', en alliage de titane, pour applications aérospatiales.
Pression nominale: Jusqu'a 28 000 kPa
Plage de températures: - 55 °C a 135 °C

Aerospace series - Pipe coupling 8°30' in titanium alloy - Ferrules, welded, with dynamic beam seal end

General Information

• Status: Published
• Publication Date: 30-Apr-2004
• ICS: 49.080 - Aerospace fluid systems and components
• Technical Committee: I08 - Imaginarni 08
• Current Stage: 6060 - National Implementation/Publication (Adopted Project)
• Start Date: 01-May-2004
• Due Date: 01-May-2004
• Completion Date: 01-May-2004
• Ref Project: EN 3243:2001 - Aerospace series - Pipe coupling 8°30' in titanium alloy - Ferrules, welded, with dynamic beam seal end

Standards Content (Sample)

2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aerospace series - Pipe coupling 8°30' in titanium alloy - Ferrules, welded, with dynamic beam seal endLuft- und Raumfahrt - Rohrverschraubung 8°30' aus Titanlegierung - Anschweißstutzen mit DichtlippeSérie aérospatiale - Systeme de raccordement 8°30' en alliage de titane - Olives a souder avec joint a levreAerospace series - Pipe coupling 8°30' in titanium alloy - Ferrules, welded, with dynamic beam seal end49.080Aerospace fluid systems and componentsICS:Ta slovenski standard je istoveten z:EN 3243:2001SIST EN 3243:2004en01-maj-2004SIST EN 3243:2004SLOVENSKI
STANDARD



SIST EN 3243:2004



EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 3243October 2001ICS 49.080English versionAerospace series - Pipe coupling 8°30' in titanium alloy -Ferrule, welded, with dynamic beam seal endSérie aérospatiale - Système de raccordement 8°30' enalliage de titane - Olive soudée avec joint à lèvreLuft- und Raumfahrt - Rohrverschraubung 8°30' ausTitanlegierung - Anschweißstutzen mit DichtlippeThis European Standard was approved by CEN on 6 January 2001.CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this EuropeanStandard the status of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such nationalstandards may be obtained on application to the 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 translationunder the responsibility of a CEN member into its own language and notified to the Management Centre has the same status as the officialversions.CEN members are the national standards bodies of Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany, Greece,Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and United Kingdom.EUROPEAN COMMITTEE FOR STANDARDIZATIONCOMITÉ EUROPÉEN DE NORMALISATIONEUROPÄISCHES KOMITEE FÜR NORMUNGManagement Centre: rue de Stassart, 36
B-1050 Brussels© 2001 CENAll rights of exploitation in any form and by any means reservedworldwide for CEN national Members.Ref. No. EN 3243:2001 ESIST EN 3243:2004



EN 3243:2001 (E)2ForewordThis European Standard has been prepared by the European Association of Aerospace Manufacturers(AECMA).After inquiries and votes carried out in accordance with the rules of this Association, this Standard hasreceived the approval of the National Associations and the Official Services of the member countries ofAECMA, prior to its presentation to CEN.This European Standard shall be given the status of a national standard, either by publication of an identicaltext or by endorsement, at the latest by April 2002, and conflicting national standards shall be withdrawn atthe latest by April 2002.According to the CEN/CENELEC Internal Regulations, the national standards organizations of the followingcountries are bound to implement this European Standard: Austria, Belgium, Czech Republic, Denmark,Finland, Fran
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