SIST EN 4184:2004

Aerospace series - Pipe coupling 8°30' in titanium alloy - Elbows 45° double, welded ends

This standard specifies the characteristics of elbows 45°, welded ends, 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 - Winkelverschraubungen 45° mit Anschweißenden

Diese Norm legt die Eigenschaften von Winkelverschraubungen 45° mit Anschweißenden, 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 - Raccords coudés a 45° doubles, a souder

La présente norme spécifie les caractéristiques des raccords coudés a 45° a souder, doubles, pour les systemes de
raccordement 8°30', en alliage de titane, pour applications aérospatiales.
Pression nominale: jusqu'a 28 000 kPa
Plage de température:   55 °C a 135 °C

Aerospace series - Pipe coupling 8°30' in titanium alloy - Elbows 45° double, welded ends

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 4184:2001 - Aerospace series - Pipe coupling 8°30' in titanium alloy - Elbows 45° double, welded ends

Standards Content (Sample)

SLOVENSKI STANDARD
SIST EN 4184:2004
01-maj-2004
Aerospace series - Pipe coupling 8°30' in titanium alloy - Elbows 45° double,
welded ends
Aerospace series - Pipe coupling 8°30' in titanium alloy - Elbows 45° double, welded
ends
Luft- und Raumfahrt - Rohrverschraubung 8°30' aus Titanlegierung -
Winkelverschraubungen 45° mit Anschweißenden
Série aérospatiale - Systeme de raccordement 8°30' en alliage de titane - Raccords
coudés a 45° doubles, a souder
Ta slovenski standard je istoveten z: EN 4184:2001
ICS:
49.080 /HWDOVNLLQYHVROMVNL Aerospace fluid systems and
KLGUDYOLþQLVLVWHPLLQGHOL components
SIST EN 4184:2004 en
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

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SIST EN 4184:2004

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SIST EN 4184:2004
EUROPEAN STANDARD
EN 4184
NORME EUROPÉENNE
EUROPÄISCHE NORM
October 2001
ICS 49.080
English version
Aerospace series - Pipe coupling 8°30' in titanium alloy - Elbows
45°, welded ends
Série aérospatiale - Système de raccordement 8°30' en Luft- und Raumfahrt - Rohrverschraubung 8°30' aus
alliage de titane - Raccords coudés à 45°, à souder Titanlegierung - Winkelverschraubungen 45° mit
Anschweißenden
This 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 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 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 Management Centre has the same status as the official
versions.
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 STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION
EUROPÄISCHES KOMITEE FÜR NORMUNG
Management Centre: rue de Stassart, 36  B-1050 Brussels
© 2001 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 4184:2001 E
worldwide for CEN national Members.

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SIST EN 4184:2004
EN 4184:2001 (E)
Foreword
This 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 the
approval of the National Associations and the Official Services of the member countries of AECMA, 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 April 2002, and conflicting national standards shall be withdrawn at the latest by April 2002.
According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following countries are
bound to implement this European Standard: Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany,
Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and the United
Kingdom.
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SIST EN 4184:2004
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