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 - Système de raccordement 8°30' en alliage de titane - Olives à souder avec joint à lèvre

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

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

General Information

Status
Published
Publication Date
23-Oct-2001
Withdrawal Date
29-Apr-2002
Technical Committee
ASD-STAN - Aerospace
Drafting Committee
ASD-STAN/D 3 - Mechanical
Current Stage
9093 - Decision to confirm - Review Enquiry
Start Date
31-May-2017
Completion Date
21-Jan-2026

Relations

Effective Date
28-Jan-2026

Overview

EN 3243:2001 defines the characteristics and requirements for welded ferrules with dynamic beam seal end used with pipe coupling 8°30' in titanium alloy for aerospace applications. The standard covers ferrule configuration, materials, surface finish, marking and technical acceptance criteria for service up to 28 000 kPa and temperatures from −55 °C to 135 °C. It is part of the aerospace series of standards intended for aerospace fluid systems and components.

Key topics and requirements

  • Scope & limits
    • Applicable to ferrules welded to coupling ends 8°30' in titanium alloy for aerospace use.
    • Nominal pressure: up to 28 000 kPa.
    • Temperature range:−55 °C to 135 °C.
  • Configuration, dimensions and mass
    • Geometry and mass values are specified by figure and table references in the standard (dimensions that are unspecified may be at manufacturer’s option provided EN 3275 qualification/acceptance is met).
  • Materials
    • Titanium alloy requirements reference EN 3311 (annealed) or EN 3314 (solution treated and aged) for material selection.
  • Surface roughness
    • Surface finish requirements are specified relative to the ferrule geometry and sealing face (referenced figures).
  • Marking
    • Marking format follows EN 2424 (style F plus manufacturing date or batch number; style G for alternative marking) and includes the EN 3243 identity block format.
  • Technical specification and acceptance
    • Qualification and acceptance testing requirements reference EN 3275, type II (dynamic beam seal end tests and inspection).
  • Documentation
    • Design, manufacturing and inspection documentation should reference the appropriate codes and the EN 3243 designation.

Applications and who uses it

  • Intended for manufacturers, designers and quality engineers working on aerospace fluid systems and components where high-integrity pipe couplings are required.
  • Typical users:
    • Aerospace component manufacturers (ferrules, couplings)
    • Aircraft systems design and installation engineers
    • Procurement and quality assurance teams ensuring compliance with aerospace component standards
    • Certification and maintenance organizations verifying part conformity
  • Practical uses include welded coupling joints in high-pressure aerospace tubing assemblies where a dynamic beam seal is required for reliable sealing under thermal and pressure cycling.

Related standards

  • EN 3275 - Pipe coupling 8°30' dynamic beam seal end (geometric configuration / technical specification)
  • EN 2656 - Pipe coupling coupling ends, welded (geometric configuration)
  • EN 2424 - Marking of aerospace products
  • EN 3311 / EN 3314 - Titanium alloy material specifications

Keywords: EN 3243:2001, welded ferrules, dynamic beam seal, pipe coupling 8°30', titanium alloy, aerospace standard, nominal pressure 28000 kPa, −55 °C to 135 °C.

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Frequently Asked Questions

EN 3243:2001 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Pipe coupling 8°30' in titanium alloy - Ferrules, welded, with dynamic beam seal end". This standard covers: 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

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

EN 3243:2001 is classified under the following ICS (International Classification for Standards) categories: 49.080 - Aerospace fluid systems and components. The ICS classification helps identify the subject area and facilitates finding related standards.

EN 3243:2001 has the following relationships with other standards: It is inter standard links to EN 3311:2023. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.

EN 3243:2001 is available in PDF format for immediate download after purchase. The document can be added to your cart and obtained through the secure checkout process. Digital delivery ensures instant access to the complete standard document.

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
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
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