EN 4182:2001

Aerospace series - Pipe coupling 8°30' in titanium alloy - Tees, reduced

This standard specifies the characteristics of tees, reduced, 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 - T-Verschraubungen, reduziert

Diese Norm legt die Eigenschaften von T-Verschraubungen, reduziert, 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 - Système de raccordement 8°30' en alliage de titane - Raccords en té, réduits

La présente norme spécifie les caractéristiques des raccords en té, réduits, pour les systèmes de raccordement 8°30', en
alliage de titane, pour applications aérospatiales.
Pression nominale: jusqu'à 28 000 kPa
Plage de température:   55 °C à 135 °C

Aerospace series - Pipe coupling 8°30' in titanium alloy - Tees, reduced

General Information

• Status: Published
• Publication Date: 23-Oct-2001
• Withdrawal Date: 29-Apr-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: 16-Jun-2017
• Ref Project: SIST EN 4182:2004 - Aerospace series - Pipe coupling 8°30' in titanium alloy - Tees, reduced

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 - Tees, reducedLuft- und Raumfahrt - Rohrverschraubung 8°30' aus Titanlegierung - T-Verschraubungen, reduziertSérie aérospatiale - Systeme de raccordement 8°30' en alliage de titane - Raccords en té, réduitsAerospace series - Pipe coupling 8°30' in titanium alloy - Tees, reduced49.080Aerospace fluid systems and componentsICS:Ta slovenski standard je istoveten z:EN 4182:2001SIST EN 4182:2004en01-maj-2004SIST EN 4182:2004SLOVENSKI
STANDARD
EUROPEAN STANDARDNORME EUROPÉENNEEUROPÄISCHE NORMEN 4182October 2001ICS 49.080English versionAerospace series - Pipe coupling 8°30' in titanium alloy - Tees,reducedSérie aérospatiale - Système de raccordement 8°30' enalliage de titane - Raccords en té, réduitsLuft- und Raumfahrt - Rohrverschraubung 8°30' ausTitanlegierung - T-Verschraubungen, reduziertThis European Standard was approved by CEN on 28 February 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 4182:2001 ESIST EN 4182:2004

ScopeThis standard specifies the characteristics of tees, reduced, for pipe couplings 8°30', in titanium alloy, for aerospaceapplications.Nominal pressure: up to 28 000 kPaTemperature range:
55 °C to 135 °C2
Normative referencesThis Standard incorporates, by dated or undated reference provisions from other publications. These normative referencesare cited at the appropriate places in the text and the publications are listed hereafter. For dated references, subsequentamendments to or revisions of any of these publications apply to this European Standard only when incorporated in it byamendment or revision. For undated references, the latest edition of the publication referred to applies (includingamendments).ISO 5855-3,
Aerospace series — 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 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 3312,
Aerospace series — Titanium alloy TI-P64001 — Grade 2 — Annealed — Forgings — De £ 150 mm.1)EN 3314,
Aerospace series — Titanium alloy TI-P64001 — Solution treated and aged — Bar for machining —D £ 75 mm.1)EN 3315,
Aerospace series — Titanium alloy TI-P64001 — Solution treated and aged — Forgings — De £ 75 mm.1)3
Required characteri
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