SIST EN 3081:2002
(Main)Aerospace series - Pipe coupling 8°30' in titanium alloy - Ferrules, welded with dynamic beam seal end, for repair
Aerospace series - Pipe coupling 8°30' in titanium alloy - Ferrules, welded with dynamic beam seal end, for repair
This standard specifies the characteristics of welded ferrules with dynamic beam seal end for pipe couplings 8°30', in
titanium alloy, for aerospace applications, to used as repair couplings to replace EN 3243.
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, für Reparatur
Diese Norm legt die Eigenschaften von Anschweißstutzen, mit Dichtlippe, für Rohrverschraubungen 8°30' aus
Titanlegierung, zur Verwendung in der Luft- und Raumfahrt fest, die für Reparaturzwecke zum Austausch gegen Stutzen
nach EN 3243 zu verwenden sind.
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, pour réparation
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, a utiliser comme éléments de réparation en remplacement de
EN 3243.
Pression nominale: jusqu'a 28 000 kPa
Plage de température: 55 °C a 135 °C
Aerospace series - Pipe coupling 8-30' in titanium alloy - Ferrules, welded with dynamic beam seal end, for repair
General Information
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 end, for repairLuft- und Raumfahrt - Rohrverschraubung 8°30' aus Titanlegierung - Anschweißstutzenmit Dichtlippe, für ReparaturSérie aérospatiale - Systeme de raccordement 8°30' en alliage de titane - Olives a souder avec joint a levre, pour réparationAerospace series - Pipe coupling 8°30' in titanium alloy - Ferrules, welded with dynamic beam seal end, for repair49.080Aerospace fluid systems and componentsICS:Ta slovenski standard je istoveten z:EN 3081:2001SIST EN 3081:2002en01-januar-2002SIST EN 3081:2002SLOVENSKI
STANDARD
SIST EN 3081:2002
EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 3081September 2001ICS 49.080English versionAerospace series - Pipe coupling 8°30' in titanium alloy -Ferrules, welded with dynamic beam seal end, for repairSérie aérospatiale - Système de raccordement 8°30' enalliage de titane - Olive à souder avec joint à lèvre, pourréparationLuft- und Raumfahrt - Rohrverschraubung 8°30' ausTitanlegierung - Anschweißstutzen mit Dichtlippe, fürReparaturThis European Standard was approved by CEN on 20 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 3081:2001 ESIST EN 3081:2002
EN 3081:2001 (E)ForewordThis 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 has received theapproval of the National Associations and the Official Services of the member countries of AECMA, prior to its presentationto CEN.This European Standard shall be given the status of a national standard, either by publication of an identical text or byendorsement, at the latest by March 2002, and conflicting national standards shall be withdrawn at the latest by March2002.According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following countries arebound to implement this European Standard: Austria, Belgium, Czech Republic, Denmark, Finland, F
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