Aerospace series - Pipe coupling 8°30' in titanium alloy - Elbows 90° with thrust wire nut

This standard specifies the characteristics of elbows 90°, with thrust wire nut, 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 90° mit Mutter mit Schubdraht

Diese Norm legt die Eigenschaften von Winkelverschraubungen 90° mit Muttern mit Schubdraht, für
Rohrverschraubungen 8°30', aus Titanlegierung, für Anwendungen in der Luft- und Raumfahrt fest.
⎯ Nenndruck: bis zu 28 000 kPa;
⎯ Temperaturbereich: –50 °C bis 135 °C.

Série aérospatiale - Système de raccordement 8°30' en alliage de titane - Raccords coudés à 90° avec écrou à jonc

Aeronavtika - Cevni priključek 8°30' iz titanove zlitine - Kotni cevni priključek 90° z matico s potisno žico

General Information

Status
Published
Publication Date
14-Jul-2009
Withdrawal Date
30-Jan-2010
Technical Committee
Drafting Committee
Current Stage
9093 - Decision to confirm - Review Enquiry
Start Date
21-Jan-2025
Completion Date
14-May-2025

Relations

Overview

EN 4018:2009 is a CEN aerospace standard that defines the characteristics of 90° elbows with thrust wire nut for pipe coupling 8°30' in titanium alloy. Intended for aerospace fluid systems, this standard covers design, materials, surface treatment and marking for elbows rated to a nominal pressure up to 28 000 kPa and a temperature range of −55 °C to 135 °C. EN 4018:2009 helps manufacturers and users ensure interchangeability, performance and quality of titanium elbow fittings in aircraft hydraulic and fluid systems.

Key topics and technical requirements

  • Scope and ratings
    • Elbows 90° for pipe coupling 8°30' in titanium alloy
    • Nominal pressure: up to 28 000 kPa
    • Temperature range: −55 °C to 135 °C
  • Configuration and dimensions
    • Geometric configuration and mass defined by Figure 1 and Table 1 (codes covering MJ thread sizes MJ10 to MJ39)
    • Unspecified dimensions may be manufacturer‑defined if EN 3275 Type II requirements are met
  • Materials
    • Titanium alloys per referenced EN documents (EN 3311 / EN 3312 / EN 3314 / EN 3315)
  • Surface treatment & lubrication
    • Lubrication per EN 2491 (molybdenum disulphide dry lubricants)
    • Surface pre-treatment: abrasive blasting with non‑metallic grit
    • Lubricant film thickness: 0.005 mm to 0.013 mm
  • Internal finishing
    • Internal junction radius R: 0.3 mm to 1.0 mm
    • Surface roughness: 0.8 µm
    • Hand deburring is not permitted
  • Marking and designation
    • Marking per EN 2424 (style A)
    • Example designation format: “ELBOW 90° EN4018‑05”
  • Quality & technical specifications
    • Technical spec and dynamic beam seal requirements reference EN 3275 / EN 3273 / EN 3274
    • Quality assurance/qualification per EN 9133

Applications and who uses EN 4018:2009

  • Aerospace OEMs and Tier suppliers producing or procuring titanium elbow fittings for hydraulic, pneumatic and fluid transfer systems
  • Design engineers specifying fittings for aircraft fluid systems needing high pressure and defined temperature performance
  • Quality, procurement and inspection teams ensuring component conformity, marking and traceability
  • Maintenance and repair organizations selecting replacement parts compatible with pipe coupling 8°30' systems

Related standards

  • EN 3273, EN 3274, EN 3275 - geometric and seal interfaces for 8°30' pipe couplings
  • EN 2491 - dry lubricant coating methods
  • EN 2424 - marking of aerospace products
  • EN 9133 - quality management and qualification for aerospace standard parts
  • ISO 5855‑3 - MJ thread limit dimensions

Keywords: EN 4018:2009, aerospace standard, pipe coupling 8°30', titanium alloy elbows, thrust wire nut, 28 000 kPa, −55 °C to 135 °C, surface roughness, EN 2491, EN 3275.

Standard
EN 4018:2009
English language
7 pages
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Frequently Asked Questions

EN 4018:2009 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Pipe coupling 8°30' in titanium alloy - Elbows 90° with thrust wire nut". This standard covers: This standard specifies the characteristics of elbows 90°, with thrust wire nut, 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 elbows 90°, with thrust wire nut, 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 4018:2009 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 4018:2009 has the following relationships with other standards: It is inter standard links to EN 4018:2001. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.

You can purchase EN 4018:2009 directly from iTeh Standards. The document is available in PDF format and is delivered instantly after payment. Add the standard to your cart and complete the secure checkout process. iTeh Standards is an authorized distributor of CEN standards.

Standards Content (Sample)


SLOVENSKI STANDARD
01-november-2009
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SIST EN 4018:2002
$HURQDYWLND&HYQLSULNOMXþHNƒ
L]WLWDQRYH]OLWLQH.RWQLFHYQLSULNOMXþHNƒ]
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Aerospace series - Pipe coupling 8°30' in titanium alloy - Elbows 90° with thrust wire nut
Luft- und Raumfahrt - Rohrverschraubung 8°30' aus Titanlegierung -
Winkelverschraubungen 90° mit Mutter mit Schubdraht
Série aérospatiale - Système de raccordement 8°30' en alliage de titane - Raccords
coudés à 90° avec écrou à jonc
Ta slovenski standard je istoveten z: EN 4018:2009
ICS:
49.080 /HWDOVNLLQYHVROMVNL Aerospace fluid systems and
KLGUDYOLþQLVLVWHPLLQGHOL components
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EUROPEAN STANDARD
EN 4018
NORME EUROPÉENNE
EUROPÄISCHE NORM
July 2009
ICS 49.080 Supersedes EN 4018:2001
English Version
Aerospace series - Pipe coupling 8°30' in titanium alloy - Elbows
90° with thrust wire nut
Série aérospatiale - Système de raccordement 8°30' en Luft- und Raumfahrt - Rohrverschraubung 8°30' aus
alliage de titane - Raccords coudés à 90° avec écrou à jonc Titanlegierung - Winkelverschraubungen 90° mit Mutter mit
Schubdraht
This European Standard was approved by CEN on 8 February 2009.

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 CEN 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 CEN Management Centre has the same status as the
official versions.
CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland,
France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal,
Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.

EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION

EUROPÄISCHES KOMITEE FÜR NORMUNG

Management Centre: Avenue Marnix 17, B-1000 Brussels
© 2009 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 4018:2009: E
worldwide for CEN national Members.

Contents Page
Foreword .3
1 Scope .4
2 Normative references .4
3 Required characteristics .5
3.1 Configuration — Dimensions — Mass.5
3.2 Surface roughness .5
3.3 Materials .5
3.4 Surface treatment .5
3.5 Internal surface finishing .5
4 Designation .7
5 Marking .7
6 Technical specification .7
7 Quality assurance .7

Foreword
This document (EN 4018:2009) has been prepared by the Aerospace and Defence Industries Association of
Europe - Standardization (ASD-STAN).
After enquiries 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 ASD,
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 January 2010, and conflicting national standards shall be withdrawn at
the latest by January 2010.
Attention is drawn to the possibility that some of the elements of this document may be the subject of patent
rights. CEN [and
...

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