Aerospace series - Clamps, saddle fixed and sliding version in aluminium alloy with rubber cushioning - Dimension, masses

This standard specifies the required characteristics of saddle clamps in aluminium alloy with various cushion materials.
These clamps, fixed version (type 1) or sliding version (type 2), are used for supporting pipe assemblies.
They are used up to 80 °C max.
Usage at a higher temperature is at the option of the user.
For temperature range and environmental considerations see the various cushion material standards.

Luft- und Raumfahrt - Schellen in Sattelform aus aluminiumlefierung mit Profilgummi für feste und gleitende Rohrhalterung - Maße, Massen

Diese Norm legt die Anforderungen an Schellen in Sattelform aus Aluminiumlegierung mit verschiedenen
Profilgummi-Werkstoffen fest.
Diese Schellen, die es in fester Ausführung (Typ 1) und gleitender Ausführung (Typ 2) gibt, werden als
Halterung für Rohrleitungen verwendet.
Sie werden bis zu einer Temperatur von max. 80 °C verwendet.
Die Verwendung bei höherer Temperatur erfolgt nach Wahl des Anwenders.
Temperaturbereich und Umweltbedingungen entsprechen den Angaben in den jeweiligen Werkstoffnormen
für Profilgummi.

Série aérospatiale - Colliers du type ''Oméga'' avec serrage ou coulissants en alliage d’aluminium avec profilé en élastomère - Dimensions, masses

Aeronavtika - Objemke, sedlaste oblike, iz aluminijeve zlitine, z gumo za pritrditev cevi - Mere, mase

General Information

Status
Published
Publication Date
30-Sep-2009
Technical Committee
Current Stage
6060 - National Implementation/Publication (Adopted Project)
Start Date
28-Sep-2009
Due Date
03-Dec-2009
Completion Date
01-Oct-2009

Relations

Overview

SIST EN 3730:2009 is a European standard developed by CEN that specifies the requirements for aerospace-grade saddle clamps made from aluminium alloy with rubber cushioning. These clamps are designed primarily for pipe assemblies in aerospace applications. The standard covers both fixed (type 1) and sliding (type 2) clamp versions, focusing on their dimensions, masses, materials, surface treatments, and marking for identification.

Designed for use at temperatures up to 80 °C, these clamps incorporate rubber cushion materials certified under related standards to ensure thermal and environmental compliance. SIST EN 3730:2009 supersedes the previous 2001 edition and provides updated specifications to meet modern aerospace requirements.

Key Topics

  • Materials

    • Aluminium alloy compliant with EN 2693 (AL-P5086-H111).
    • Cushion materials include:
      • Silicone rubber (VMQ) per EN 2261 (color: rust).
      • Fluorosilicone rubber (FVMQ) per EN 3826 (color: blue).
      • Fluorocarbon rubber (FPM) per EN 2566 (color: brown).
    • Rubber cushions comply with EN 4115 for dimensions and properties.
  • Clamp Types and Configuration

    • Type 1: Fixed saddle clamps (code J).
    • Type 2: Sliding saddle clamps (code K).
    • Each clamp consists of two halves (top and bottom) with specified forms (A, B, C) and precise dimensions to accommodate different pipe diameters.
  • Dimensions and Masses

    • Dimensions are detailed in millimeters with strict tolerances ensuring interchangeability.
    • Masses are provided per 1,000 pieces with specifics for each clamp part to aid design and weight calculations.
  • Surface Treatments

    • Options include none (code 0) or yellow chromate coating (code 1) according to EN 2437 to enhance corrosion resistance.
  • Marking and Designation

    • Clamps are clearly marked in compliance with EN 2424 for traceability.
    • Marking includes standard number, diameter code, form code, cushion material color, and surface treatment identifier.
  • Technical Specifications and References

    • Referenced standards for related materials and processes include EN 2261, EN 2424, EN 2437, EN 2566, EN 2693, EN 3078, EN 3825, EN 3826, and EN 4115.
    • Clamps must meet the aerospace industry's high reliability and safety standards.

Applications

SIST EN 3730:2009 clamps are essential components for aerospace fluid systems, providing secure pipe support while minimizing vibration and wear. Typical applications include:

  • Aircraft hydraulic and fuel pipeline assemblies.
  • Support systems in space vehicles and satellites.
  • Aerospace manufacturing and maintenance for dependable pipe fixation.
  • Environments requiring lightweight, corrosion-resistant clamp solutions with rubber cushioning to protect pipes from mechanical damage.

Their ability to operate at elevated temperatures up to 80 °C (with optional higher temperature usage) and compliance with international aerospace specifications make them indispensable in critical aerospace fluid systems.

Related Standards

  • EN 2693 – Aluminium alloy specifications for aerospace components.
  • EN 4115 – Rubber cushions for clamps dimension and mass standards.
  • EN 2424 – Marking requirements for aerospace products ensuring identification and traceability.
  • EN 2437 – Chromate conversion coating standards to protect aluminium alloys.
  • EN 2261, EN 2566, EN 3825, EN 3826 – Standards for elastomer cushion materials with defined hardness and environmental resistance.
  • EN 3078 – General technical specifications for clamps with rubber cushioning in aerospace applications.

By adhering to SIST EN 3730:2009, aerospace manufacturers and maintenance professionals can ensure compatibility, safety, and performance of saddle clamps used in demanding aerospace fluid systems. This standard plays a vital role in maintaining the structural integrity of pipe assemblies through robust design and material quality, fostering reliability across the aerospace industry.

Standard
SIST EN 3730:2009
English language
12 pages
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Standards Content (Sample)


SLOVENSKI STANDARD
01-november-2009
1DGRPHãþD
SIST EN 3730:2002
Aeronavtika - Objemke, sedlaste oblike, iz aluminijeve zlitine, z gumo za pritrditev
cevi - Mere, mase
Aerospace series - Clamps, saddle fixed and sliding version in aluminium alloy with
rubber cushioning - Dimension, masses
Luft- und Raumfahrt - Schellen in Sattelform aus aluminiumlefierung mit Profilgummi für
feste und gleitende Rohrhalterung - Maße, Massen
Série aérospatiale - Colliers du type ''Oméga'' avec serrage ou coulissants en alliage
d’aluminium avec profilé en élastomère - Dimensions, masses
Ta slovenski standard je istoveten z: EN 3730:2009
ICS:
49.025.20 Aluminij Aluminium
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 3730
NORME EUROPÉENNE
EUROPÄISCHE NORM
September 2009
ICS 49.080 Supersedes EN 3730:2001
English Version
Aerospace series - Clamps, saddle fixed and sliding version in
aluminium alloy with rubber cushioning - Dimension, masses
Série aérospatiale - Colliers du type ''Oméga'' avec serrage Luft- und Raumfahrt - Schellen in Sattelform aus
ou coulissants en alliage d'aluminium avec profilé en aluminiumlefierung mit Profilgummi für feste und gleitende
élastomère - Dimensions, masses Rohrhalterung - Maße, Massen
This European Standard was approved by CEN on 1 July 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 3730:2009: E
worldwide for CEN national Members.

Contents Page
Foreword .3
1 Scope .4
2 Normative references .4
3 Required characteristics .4
4 Designation .9
5 Marking . 11
6 Technical specification . 12

Foreword
This document (EN 3730:2009) 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 March 2010, and conflicting national standards shall be withdrawn at
the latest by March 2010.
Attention is drawn to the possibility that some of the elements of this document may be the subject of patent
rights. CEN [and/or CENELEC] shall not be held responsible for identifying any or all such patent rights.
This document supersedes EN 3730:2001.
According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following
countries are bound to implement this European Standard: 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 the United Kingdom.
1 Scope
This standard specifies the required characteristics of saddle clamps in aluminium alloy with various cushion
materials.
These clamps, fixed version (type 1) or sliding version (type 2), are used for supporting pipe assemblies.
They are used up to 80 °C max.
Usage at a higher temperature is at the option of the user.
For temperature range and environmental considerations see the various cushion material standards.
2 Normative references
The following referenced documents are indispensable for the application of this document. For dated
references, only the edition cited applies. For undated references, the latest edition of the referenced
document (including any amendments) applies.
EN 2261, Aerospace series — Silicone rubber (VMQ) — Hardness 70 IRHD.
EN 2424, Aerospace series — Marking of aerospace products.
EN 2437, Aerospace series — Chromate conversion coatings (yellow) for aluminium and aluminium alloys.
1)
EN 2566, Aerospace series — Fluorocarbon rubber (FPM) — Hardness 70 IRHD.
EN 2693, Aerospace series
...

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Frequently Asked Questions

SIST EN 3730:2009 is a standard published by the Slovenian Institute for Standardization (SIST). Its full title is "Aerospace series - Clamps, saddle fixed and sliding version in aluminium alloy with rubber cushioning - Dimension, masses". This standard covers: This standard specifies the required characteristics of saddle clamps in aluminium alloy with various cushion materials. These clamps, fixed version (type 1) or sliding version (type 2), are used for supporting pipe assemblies. They are used up to 80 °C max. Usage at a higher temperature is at the option of the user. For temperature range and environmental considerations see the various cushion material standards.

This standard specifies the required characteristics of saddle clamps in aluminium alloy with various cushion materials. These clamps, fixed version (type 1) or sliding version (type 2), are used for supporting pipe assemblies. They are used up to 80 °C max. Usage at a higher temperature is at the option of the user. For temperature range and environmental considerations see the various cushion material standards.

SIST EN 3730:2009 is classified under the following ICS (International Classification for Standards) categories: 49.025.20 - Aluminium; 49.080 - Aerospace fluid systems and components. The ICS classification helps identify the subject area and facilitates finding related standards.

SIST EN 3730:2009 has the following relationships with other standards: It is inter standard links to SIST EN 3730:2002. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.

You can purchase SIST EN 3730:2009 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 SIST standards.