EN 3084:2001

Aerospace series - Pipe coupling 8°30' in titanium alloy - Unions, welded end threaded for repair

This standard specifies the characteristics of unions, welded end, threaded, for pipe couplings 8°30', in titanium alloy, for
aerospace applications to be used as repair couplings to replace EN 4233.
Nominal pressure: up to 28 000 kPa
Temperature range:   55 °C to 135 °C

Luft- und Raumfahrt - Rohrverschraubung 8°30' aus Titanlegierung - Gerade Erschraubungen mit Anschweißende für Reparatur

Diese Norm legt die Eigenschaften von geraden Verschraubungen mit Anschweißende, für Rohrverschraubungen 8°30' aus
Titanlegierung, zur Verwendung in der Luft- und Raumfahrt fest, die für Reparaturzwecke zum Austausch gegen
Verschraubungen nach EN 4233 zu verwenden sind.
Nenndruck: bis 28 000 kPa
Temperaturbereich:   55 °C bis 135 °C

Série aérospatiale - Système de raccordement 8°30' en alliage de titane - Raccords droits, à souder filetés pour réparation

La présente norme spécifie les caractéristiques des raccords droits, à souder, filetés, pour les systèmes de raccordement
8°30', en alliage de titane, pour applications aérospatiales, à utiliser comme éléments de réparation en remplacement de
EN 4233.
Pression nominale: jusqu'à 28 000 kPa
Plage de température:   55 °C à 135 °C

Aerospace series - Pipe coupling 8-30' in titanium alloy - Unions, welded end threaded for repair

General Information

• Status: Published
• Publication Date: 18-Sep-2001
• Withdrawal Date: 30-Mar-2002
• ICS: 49.080 - Aerospace fluid systems and components
• Technical Committee: ASD-STAN - Aerospace
• Drafting Committee: ASD-STAN/D 3 - Mechanical
• Current Stage: 9093 - Decision to confirm - Review Enquiry
• Completion Date: 31-May-2017
• Ref Project: SIST EN 3084:2002 - Aerospace series - Pipe coupling 8°30' in titanium alloy - Unions, welded end threaded for repair

Relations

• Corrected By: EN 3084:2001/AC:2003 - Aerospace series - Pipe coupling 8°30' in titanium alloy - Unions, welded end threaded for repair
• Effective Date: 22-Dec-2008

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 - Unions, welded end threaded for repairLuft- und Raumfahrt - Rohrverschraubung 8°30' aus Titanlegierung - Gerade Erschraubungenmit Anschweißende für ReparaturSérie aérospatiale - Systeme de raccordement 8°30' en alliage de titane - Raccords droits, a souder filetés pour réparationAerospace series - Pipe coupling 8°30' in titanium alloy - Unions, welded end threaded for repair49.080Aerospace fluid systems and componentsICS:Ta slovenski standard je istoveten z:EN 3084:2001SIST EN 3084:2002en01-januar-2002SIST EN 3084:2002SLOVENSKI
STANDARD



SIST EN 3084:2002



EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 3084September 2001ICS 49.080English versionAerospace series - Pipe coupling 8°30' in titanium alloy -Unions, welded end threaded for repairSérie aérospatiale - Système de raccordement 8°30' enalliage de titane - Raccords droits, à souder filetés pourréparationLuft- und Raumfahrt - Rohrverschraubung 8°30' ausTitanlegierung - Gerade Verschraubungen mitAnschweißende für ReparaturThis 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 3084:2001 ESIST EN 3084:2002



EN 3084:2001 (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 presen-tation to 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 countriesare bound to implement this European Standard: Austria, Belgium, Czech Republic, Denmark, Finland, France, Ger-many, Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland andthe United Kingdom.2SIST EN 3084:2002



EN 3084:2001 (E)1
ScopeThis standard specifies the characteristics of unions, welded end, threaded, for pipe couplings 8°30', in titanium alloy, foraerospace applications to be used as repair couplings to replace EN 4233.Nominal pressure: up to 28 000 kPaTemperature range:
55 °C to 135 °C2
Normative referencesThis European Standard incorporates by dated or undated reference provisions from other publications. These normativereferences are cited at the appropriate places in the text and the publications are listed hereafter. For dated references,subsequent amendments to or revisions of any of these publications apply to this European Standard only whenincorporated in it by amendment or revision. For undated references, the latest edition of the publication referred to applies(including amendments).ISO 5855-3,
Aerospace — MJ threads — Part 3: Limit dimensions for fittings for fluid systems.EN 2424,
Aerospace series — Marking of aerospace products.EN 2491,
Aerospace series — Molybdenum disulphide dry lubricants — Coating methods.EN 2656,
Aerospace series — Pipe coupling — Coupling ends, welded — Geometric configuration.EN 3274,
Aerospace series — Pipe coupling 8°30' — Thread ends — Geometric configuration.EN 3275,
Aerospace series — Pipe coupling 8°30' up to 28 000 kPa — Dynamic beam seal — Metric series — Technicalspecification.EN 3311,
Aerospace series — Titanium alloy TI-P64001 — Annealed — Bar for machining — D £ 150 mm.1)EN 3314,
Aerospace series — Titanium alloy TI-P64001 — Solution treated and aged — Bar for machining —D £ 75 mm.1)EN 4233,
Aerospace series — Pip
...