ASD-STAN PREN 2234-2016 Aerospace series Cable electrical fire resistant Technical specification (Edition P 4).pdf
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1、ASD-STAN STANDARD NORME ASD-STAN ASD-STAN NORM ASD-STAN prEN 2234 Edition P 4 September 2016 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATION Rue Montoyer 10 - 1000 Brussels - Tel. 32 2 775 8126 - Fax. 32 2 775 8131 - www.asd-stan.org ICS: Supersedes edition
2、P 3 of November 2010 and will supersede EN 2234:2012 Descriptors: ENGLISH VERSION Aerospace series Cable, electrical, fire resistant Technical specification Luft- und Raumfahrt Elektrische Leitungen, feuerbestndig Technische Lieferbedingungen Srie arospatiale Cbles lectriques rsistant au feu Spcific
3、ation technique This “Aerospace Series“ Prestandard has been drawn up under the responsibility of ASD-STAN (The AeroSpace and Defence Industries Association of Europe - Standardization). It is published for the needs of the European Aerospace Industry. It has been technically approved by the experts
4、 of the concerned Domain following member comments. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that interchangeability is affected, physically or functionally, without re-identification of the standard. After examination and review by u
5、sers and formal agreement of ASD-STAN, the ASD-STAN prEN will be submitted as a draft European Standard (prEN) to CEN (European Committee for Standardization) for formal vote and transformation to full European Standard (EN). The CEN national members have then to implement the EN at national level b
6、y giving the EN the status of a national standard and by withdrawing any national standards conflicting with the EN. ASD-STAN Technical Committee approves that: “This document is published by ASD-STAN for the needs of the European Aerospace Industry. The use of this standard is entirely voluntary, a
7、nd its applicability and suitability for any particular use, including any patent infringement arising therefrom, is the sole responsibility of the user.” ASD-STAN reviews each standard and technical report at least every five years at which time it may be revised, reaffirmed, stabilized or cancelle
8、d. ASD-STAN invites you to send your written comments or any suggestions that may arise. All rights reserved. No parts of this publication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, witho
9、ut prior written permission of ASD-STAN. Order details: E-mail: salesasd-stan.org Web address: http:/www.asd-stan.org/ Edition approved for publication 1st September 2016 Comments should be sent within six months after the date of publication to ASD-STAN Electrical Domain Copyright 2016 ASD-STAN prE
10、N 2234:2016 (E) 2 Contents Page Foreword 2 1 Scope 3 2 Normative references 3 3 Terms, definitions and symbols . 3 4 Materials and construction . 3 5 Required characteristics 5 6 Tests method 5 7 Quality assurance 8 8 Identification marking 10 10 Packaging, labelling and delivery lengths 11 Foreword
11、 This standard was reviewed by the Domain Technical Coordinator of ASD-STANs Electrical Domain. After inquiries and votes carried out in accordance with the rules of ASD-STAN defined in ASD-STANs General Process Manual, this standard has received approval for Publication. prEN 2234:2016 (E) 3 1 Scop
12、e This standard specifies the required characteristics and test procedures for fire resistant or fire-proof electrical cables for use in aircraft electrical systems. These cables should also maintain a specific surface resistance when they are subjected to a flame of 1 100 C after 5 minutes (fire re
13、sistant) or 15 minutes (fire-proof) exposure. The insulation of these cables is designed to withstand aircraft voltages at a frequency not exceeding 2 000 Hz. Unless specified by individual product standards the maximum demonstrated ac voltage of rating of these cables is 115 V rms (phase to neutral
14、) and 200 V rms (phase to phase) and a long term temperature of up to 260 C (ambient temperature plus temperature rise in conductor). 2 Normative references The following documents, in whole or in part, are normatively referenced in this document and are indispensable for its application. For dated
15、references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 3475-100 (all parts), Aerospace series Cables, electrical, aircraft use Test methods Part 100: General EN 3838, Aerospace series Requirements and t
16、ests on user-applied markings on aircraft electrical cables EN 9102, Aerospace series Quality systems First article inspection EN 9133, Aerospace series Quality Management Systems Qualification Procedure for Aerospace Standard Products ISO 2574, Aircraft Electrical cables Identification marking ISO
17、8815, Aircraft Electrical cables and cable harnesses Vocabulary IEC 60028:1925, International standard of resistance for copper 3 Terms, definitions and symbols For the purposes of this document, the terms, definitions and symbols given in ISO 8815 and EN 3475-100 apply. 4 Materials and construction
18、 4.1 Conductors 4.1.1 Materials The individual strands used for the conductors shall be cylindrical and shall be: of nickel clad copper alloy for nominal cross section of 0,25 mm2 and 0,4 mm2; of nickel clad copper for nominal sections 0,6 mm2. The copper shall meet the requirements of IEC 60028 and
19、 the copper alloy the requirements of this standard. prEN 2234:2016 (E) 4 The nickel shall not represent less than 27 % of the total mass of the individual strand. Individual strands shall show the following minimum breaking strength: 280 N/mm2 for nickel clad copper; 315 N/mm2 for nickel clad coppe
20、r alloy. 4.1.2 Lay length Up to 9 mm2 cross section inclusive (code 090), concentric or unilay conductors are used. The lay for the stranded conductor, checked over the outside layer of a test piece 1 m long, shall be between 8 times and 16 times the maximum diameter of this conductor. For sectional
21、 areas between 14 mm2 and 68 mm2 (codes 140 to 680), the conductor comprises concentric or bunched conductors twisted together. The lay of the strands for the basic concentric or bunched conductors shall not exceed 30 times the diameter of the concentric or bunched conductor in question. The lay for
22、 concentric (or bunched) conductors, measured over the outer layer of the conductor, shall be between 8 times and 16 times the maximum conductor diameter. In all cases the lay of the outer layer shall be left-hand. 4.1.3 Joints The conductors shall be free from any joints. Each strand comprising the
23、 conductors may, however, include soldered or brazed joints. For strands with a diameter of 0,25 mm or greater, butt joints shall be used. The distance between two joints in individual strands shall exceed 3 m, measured between different strands. 4.1.4 Compaction Compaction of the causing deformatio
24、n of the strands or damage to the plating is not permitted. 4.2 Construction Finished cables The insulation shall be of a material, which takes on the circular shape of the conductor throughout its length. It shall closely cover the conductor without adhering to it, so that it reduces the corona eff
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