BS EN 4608-001-2006 Aerospace series - Cable electrical fire resistant - Single and twisted multicore assembly screened (braided) and jacketed - Operating temperatures between -65 .pdf
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1、 g49g50g3g38g50g51g60g44g49g42g3g58g44g55g43g50g56g55g3g37g54g44g3g51g40g53g48g44g54g54g44g50g49g3g40g59g38g40g51g55g3g36g54g3g51g40g53g48g44g55g55g40g39g3g37g60g3g38g50g51g60g53g44g42g43g55g3g47g36g58twisted multicore assembly, screened (braided) and jacketed Operating temperatures between 65 C and
2、 260 C Part 001: Technical specificationThe European Standard EN 4608-001:2006 has the status of a British StandardICS 49.060Aerospace series Cable, electrical, fire resistant Single and BRITISH STANDARDBS EN 4608-001:2006BS EN 4608-001:2006This British Standard was published under the authority of
3、the Standards Policy and Strategy Committee on 31 October 2006 BSI 2006ISBN 0 580 49431 4Amendments issued since publicationAmd. No. Date CommentsThis publication does not purport to include all the necessary provisions of a contract. Users are responsible for its correct application.Compliance with
4、 a British Standard cannot confer immunity from legal obligations.National forewordThis British Standard was published by BSI. It is the UK implementation of EN 4608-001:2006. The UK participation in its preparation was entrusted by Technical Committee ACE/6, Aerospace avionic electrical and fibre o
5、ptic technology, to Subcommittee ACE/6/-/2, Aerospace Cables.A list of organizations represented on ACE/6/-/2 can be obtained on request to its secretary.EUROPEAN STANDARD NORME EUROPENNE EUROPISCHE NORM EN 4608-001 June 2006 ICS 49.060 English Version Aerospace series - Cable, electrical, fire resi
6、stant - Single and twisted multicore assembly, screened (braided) and jacketed - Operating temperatures between - 65 C and 260 C - Part 001: Technical specification Srie arospatiale - Cbles lectriques blinds rsistant au feu - Simple et multifilaire blind (tresse) gain - Tempratures de fonctionnement
7、 comprises entre - 65 C et 260 C - Partie 001 : Spcification technique Luft- und Raumfahrt - Feuerberstndige elecktrische Leitungen - Einzel- und mehradrig verdrillte Leitungen, geschirmt (Geflecht) und ummantelt - Betriebstemperaturen zwischen - 65 C und 260 C - Teil 001: Technische Lieferbedingung
8、en This European Standard was approved by CEN on 20 April 2006. 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 re
9、ferences concerning such national standards may be obtained on application to the Central Secretariat 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
10、 into its own language and notified to the Central Secretariat has the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithua
11、nia, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG Management Centre: rue de Stassart, 36 B-1050 Brussels 2006
12、CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4608-001:2006: E2 Contents Page Foreword3 1 Scope 4 2 Normative references 4 3 Terms and definitions .4 4 Materials and construction of cables 5 5 Required characteristics.5 6 Tests m
13、ethods6 7 Qualification and acceptance conditions.10 8 Identification, marking . 12 9 Packaging, labelling and delivery length . 12 EN 4608-001:20063 Foreword This European Standard (EN 4608-001:2006) has been prepared by the European Association of Aerospace Manufacturers - Standardization (AECMA-S
14、TAN). 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 AECMA, prior to its presentation to CEN. This European Standard shall be given the s
15、tatus of a national standard, either by publication of an identical text or by endorsement, at the latest by December 2006, and conflicting national standards shall be withdrawn at the latest by December 2006. Attention is drawn to the possibility that some of the elements of this document may be th
16、e subject of patent rights. CEN and/or CENELEC shall not be held responsible for identifying any or all such patent rights. According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgi
17、um, 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. EN 4608-001:20064 1 Scope Thi
18、s document specifies the required characteristics and test procedures for fire resistant or fire proof electrical cables for use in aircraft electrical systems. They shall be operated at a rated AC voltage of 600 VAC, a frequency of maximum 2 000 Hz and a long-term temperature of up to 260 C (ambien
19、t temperature plus temperatures rise in conductor). These cables shall also maintain a specific dielectric strength when they are subjected to a flame of 1 100 C after five minutes (fire resistant) or 15 minutes (fire proof) exposure. 2 Normative references The following referenced documents are ind
20、ispensable 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. These references are not fully applicable. The present specification defines the field of a
21、pplication of each document. ISO 2574, Aircraft Electrical cables Identification marking. EN 2234, Aerospace series Cable, electrical, fire resistant Technical specification. EN 2235, Aerospace series Single and multicore electrical cables, screened and jacketed Technical specification. EN 3475-100*
22、, Aerospace series Cables, electrical, aircraft use Test methods Part 100: General. EN 3838, Aerospace series Requirements and tests on user-applied markings on aircraft electrical cables. 1)EN 4608-002, Aerospace series Cable, electrical, fire resistant Single and twisted multicore assembly, screen
23、ed (braided) and jacketed Operating temperatures between 65 C and 260 C Part 002: General.EN 4608-005, Aerospace series Cable, electrical, fire resistant Single and twisted multicore assembly, screened (braided) and jacketed Operating temperatures between 65 C and 260 C Part 005: DW family lightweig
24、ht two-core gauge 24 for data transmission UV laser printable Product standard.1)EN 9133, Aerospace series Quality management systems Qualification procedure for aerospace standard parts. 3 Terms and definitions For the purposes of this European Standard, the terms and definitions given in EN 3475-1
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