ASD-STAN PREN 4611-004-2004 Aerospace series Cables electrical for general purpose single and multicore assembly XLETFE Family Part 004 Tin plated copper Operating temperatures bet.pdf
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1、AECMA STANDARD NORME AECMA AECMA NORM Edition approved for publication prEN 461 1-004 Edition P 1 July 2004 Comments should be sent within six months Electrical Domain ICs: Descriptors: ENGLISH VERSION Aerospace series Cables, electrical, for general purpose, single and multicore assembly XLETFE Fam
2、ily Part 004: Tin plated copper Operating temperatures, between - 65 OC and 135 OC Dual extruded wall for open applications UV laser printable Product standard Srie arospatiale Cbles, lectriques, dusage gnral, mono et multiconducteurs Famille XLETFE Partie 004 : Cuivre tam Tempratures de fonctionnem
3、ent comprises entre - 65 OC et 135 OC Fil double isol pour applications externes Marquable au laser UV Norme de produit Luft- und Raumfahrt Ein- und mehradrige elektrische Leitungen fr allgemeine Vewendung XLETFE Familie Teil 004: Kupfer verzinnt Doppelt extrudierte Isolierung fr externe Verwendung
4、UV-Laser bedruckbar Produktnorm Betriebstemperaturen zwischen - 65 OC und 135 OC This “Aerospace Series“ frestandard 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
5、Industry. It has been technically approved by the experts of the concerned Domain following member comments. Subsequent 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-identifi
6、cation of the standard. After examination and review by users and formal agreement of AECMA-STAN, it 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
7、then to implement the EN at national level by giving the EN the status of a national standard and by withdrawing any national standards conflicting with the EN. 31 July 2004 after the date of publication to AECMA-STAN I I Copytight 2004 O by AECMA-STA1 Page 2 prEN 461 1-004:2004 Foreword This standa
8、rd 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 Publication . Contents Page 1 Scope 3 2 Norm
9、ative references . 3 3 4 4.1 4.2 4.3 4.4 5 6 7 8 9 10 Definitions and symbols . Materials and construction Materials Construction . Number of cores . Colour coding of cores . Required characteristics . Quality assurance . Designation Identification and marking Packaging, labelling and delivery lengt
10、hs Technical specification 3 4 4 4 5 5 5 9 9 9 9 9 Page 3 prEN 461 1-004:2004 1 Scope This standard specifies the characteristics of UV laser printable, tin plated copper conductor, electrical cables Crosslinked Ethylene Tetra Fluoro Ethylene co-polymer (XLETFE) family for use in the on-board electr
11、ical systems of aircraft at operating temperatures between - 65 OC and 135 OC, operating at voltages not exceeding 600 V r.m.s and frequencies not exceeding 2 O00 Hz. These cables are suitable for airframe use without additional protection. In case of conflict between this standard and other referen
12、ced documents the requirements of this standard shall take precedence. 2 Normative references This European Standard incorporates by dated or undated reference provisions from other publications. These normative references are cited at the appropriate places in the text and the publications are list
13、ed hereafter. Dated references, subsequent amendments to or revisions of any of these publications apply to this European Standard only when incorporated in it by amendment or revision. For undated references the latest edition of the publication referred to applies. EN 2083, EN 2084, EN 2235 EN 347
14、5-loo*, EN 461 1-002, EN 9133, Aerospace series - Copper or copper alloy conductors for electrical cables - Product standard Aerospace series - Cables, electric, single-core, general purpose, with conductors in copper or copper alloy - Technical specification ) Aerospace series - Single and multicor
15、e electrical cables, screened and jacketed ) Aerospace series - Cables, electrical, aircraft use - Test methods - Part 700: General Aerospace series - Cables, electrical, for general purpose, single and multicore assembly - XLETFE Family- Part 002: General ) Aerospace series - Quality management sys
16、tems - Qualification Procedure for Aerospace Standard Parts 3 Definitions and symbols See EN 3475-100. * And all its parts 1) Published as AECMA Prestandard at the date of publication of this standard Page 4 prEN 461 1-004:2004 4 Materials and construction 4.1 Materials Conductor The cable conductor
17、s shall be made of tin plated copper according to EN 461 1-002 and EN 2083 code B. Insulation for conductor all size codes - first insulator extruded XLETFE, coloured blue or a contrasting colour if the second is blue; - second insulator extruded XLETFE. For single core, it shall be possible to mark
18、 the outer insulation by UV laser printing. 4.2 Construction See EN 461 1-002, Table 1 and Table 2. Table 1 - Single core cables Code for nominal section O01 002 004 006 O10 012 020 030 050 O90 140 220 340 530 680 Nominal section mm2 0,15 0,25 0,6 1 132 2 3 5 9 14 22 34 53 68 0,4 AWG a 26 24 22 20 1
19、8 16 14 12 10 8 6 4 3 1 O Linear resistance at 20 OC Q/km max. 149,O 106,O 60,O 33,2 21,l 15,3 10,9 63 432 431 293 1,58 0,97 0,61 0,51 Maximum external diameter mm 0,92 1 ,o2 1,17 1,52 1,68 1,85 2,28 2,73 3,61 5,16 6,38 8,13 10,67 13,36 14,88 Mass kg/km max. 2,10 2,84 4,10 6,95 9,80 12,99 18,68 28,6
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