1、AECMA STANDARD NORME AECMA AECMA NORM Edition approved for publication 31 January 2005 prEN 2346-002 Edition P 2 January 2005 Comments should be sent within six months after the date of publication to AECMA-STAN PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES - STANDARDIZATION d%k?&?!f
2、f! Gulledelle 94 - B-1200 Brussels - Tel. + 32 2 775 81 10 - Fax. + 32 2 775 81 11 - www.aecma-stan.org ICs: 49.060 Descriptors: ENGLISH VERSION Aerospace series Cable, electrical, fire resistant Operating temperatures between - 65 OC and 260 OC Part 002: General Supersedes edition P 1 November 2001
3、 Srie arospatiale Cbles lectriques rsistant au feu Tempratures de fonctionnement comprises entre - 65 OC et 260 OC Partie 002 : Gnralits Luft- und Raumfahrt Feuerbestndige elektrische Leitungen Betriebstemperaturen zwischen - 65 OC und 260 OC Teil 002: Allgemeines This “Aerospace Series“ frestandard
4、 has been drawn up under the responsibility of AECMA-STAN (The European Association of Aerospace Industries - Standardization). It is published for the needs of the European Aerospace Industry. It has been technically approved by the experts of the concerned Domain following member comments. Subsequ
5、ent to the publication of this frestandard, the technical content shall not be changed to an extent that interchangeabilify is affected, physically or functionally, without re-identification of the standard. After examination and review by users and formal agreement of AECMA-STAN, it will be submitt
6、ed 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 by giving the EN the status of a national standard and by withdrawing any
7、 national standards conflicting with the EN. Electrical Domain I I Copytight 2005 O by AECMA-STA1 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page
8、2 prEN 2346-002:2005 Foreword This standard was reviewed by the Domain Technical Coordinator of AECMA-STANS Electrical Domain . After inquiries and votes carried out in accordance with the rules of AECMA-STAN defined in AECMA- STANS General Process Manual. this standard has received approval for Pub
9、lication . Contents 1 2 3 4 5 5.1 5.2 5.2.1 5.2.2 6 7 Scope Normative references . Definitions . List of product standards Materials and construction Materials Construction . Number of cores Colour coding . Identification and marking Technical specification Page 3 3 3 3 4 4 4 4 4 5 5 Copyright Assoc
10、iation Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 3 prEN 2346-002:2005 1 Scope This standard specifies the list of product standards and common characteristics of
11、fire resistant or fire-proof electrical cables for use in the on-board electrical systems of aircraft at operating temperatures between - 65 “C and 260 “C. (Except otherwise specified in the product standard). 2 Normative references The following referenced documents are indispensable for the applic
12、ation 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. I EC 28: 1925, international standard of resistance for copper. EN 2234, Aerospace series - Cable, electrical, fire
13、resistant - Technical specification I). EN 3475-1 00, Aerospace series - Cables, electrical, aircraft use - Test methods - Part 700: General. EN 3838, Aerospace series - Requirements and tests on user-applied markings on aircraft electrical cables I). TR 6058, Aerospace series - Cable code identific
14、ation list 2). 3 Definitions For the purposes of this standard, the definitions given in EN 3475-100 apply. 4 List of product standards EN 2346-003, Aerospace series - Cable, electrical, fire resistant - Operating temperatures between - 65 “C and 260 “C - Part 003: DL family, single core - Product s
15、tandard I). EN 2346-004, Aerospace series - Cable, electrical, fire resistant - Operating temperatures between - 65 “C and 260 “C - Part 004: DN family, single UV laser printable and multicore assembly - Light weight - Product standard ). EN 2346-005, Aerospace series - Cable, electrical, fire-resis
16、tant - Operating temperatures between - 65 “C and 260 “C - Part 005: DW family, single UV laser printable and multicore assembly - Light weight - Product standard ). 1) Published at AECMA Prestandard at the date of publication of this standard 2) Published as AECMA Technical Report at the date of pu
17、blication of this standard Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 4 prEN 2346-002:2005 5 Materials and construction 5.1 Materials The ind
18、ividual strands used for the conductors shall be cylindrical and shall be: - of nickel clad copper alloy for nominal cross sections of 0,4 mm2 (004) and 0,25 mm2(002) - of nickel clad copper for nominal cross sections 2 0,6 mm2 (006). The copper shall meet the requirements of IEC 28 and the copper a
19、lloy the requirements of EN 2234. 5.2 Construction 5.2.1 Number of cores See Table I. Table 1 I Number of conductors 11121314 I Factor of overall dimensions I - I 2 I 2,15 I 2,40 516171819 2,70 I3,OO I3,OO I3,30 I3,60 +I 4,OO For two cores or more: - factor for weight: 1 ,O3 - factor for ohmic resis
20、tance: 1 ,O3 5.2.2 Colour coding Outer insulation shall be white with a red stripe to indicate fire-resistant construction. This red stripe to be helical for cables with conductor sizes from 0,25 mm2 (002) to 5 mm2 (050) and helical or length wise for cables with conductors sizes from 9 mm2 (090) to
21、 68 mm2 (680). In order to allow a legible UV marking, the width of the stripe shall be between 0,3 mm and 0,5 mm. For multicore cable without jacket, each core shall be marked with its own designation. The colour of stripes is given in Table 2: Table 2 Number of cores Red Red Red Red Red Red Red Re
22、d Red Blue Blue Blue Blue Blue Blue Blue Blue Yellow Yellow Yellow Yellow Yellow Yellow Yellow Colour of stripe Green Green Green Green Green Green Black Black Black Black Black Brown Brown Brown Brown Orange Orange Orange Purple Purple Grey Copyright Association Europeene des Constructeurs de Mater
23、iel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 5 prEN 2346-002:2005 6 Identification and marking The identification and marking of cables by the manufacturer shall be in accordance with EN 2234. As the d
24、esignation required for orders is generally too long for use in electrical drawings, a shorter cross designation (without colour information) is given by the AECMA TR 6058 plus the corresponding AWG. This shorter designation shall be used for identification and marking as the following example: EXEM
25、PLE Designation EN2346-003A006 Cross reference DL 20 EN DL 20 Reference to EN standard cable 3 mandatory spaces FRF! Manufacturer country code Type code I 9 Manufacturer code Year of manufacturing For multicore cable with jacket, the marking shall be optional on cores(s) and mandatory on jacket. For
26、 multicore cable without jacket, each core shall be marked with its own designation. The cables shall be capable of being printed with the use-applied markings according to EN 3838. 7 Technical specification See EN 2234. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
