ASD-STAN PREN 4611-008-2004 Aerospace series Cables electrical for general purpose single and multicore assembly XLETFE Family Part 008 BP - Nickel plated cooper Operating temperat.pdf
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1、AECMA STANDARD NORME AECMA AECMA NORM Edition approved for publication 31 July 2004 prEN 461 1-008 Edition P 1 July 2004 Comments should be sent within six months after the date of publication to Electrical Domain AECMA-STAN ICs: Descriptors: ENGLISH VERSION Aerospace series Cables, electrical, for
2、general purpose, single and multicore assembly XLETFE Family Part 008: BP - Nickel plated copper Operating temperatures, between - 65 OC and 150 OC Dual extruded wall for open applications, with additional protection in areas of high vibration, cable flexing and fluid contamination UV laser printabl
3、e Product standard Srie arospatiale Cbles, lectriques, dusage gnral, mono et multiconducteurs Famille XLETFE Partie 008 : BP - Cuivre nickel Tempratures de fonctionnement comprises entre - 65 “C et 150 “C Fil double isol pour applications externes avec protection additionnelle pour zones hautes vibr
4、ations, flexion de cbles et pollution des fluides Marquable au laser UV Norme de produit Luft- und Raumfahrt Ein- und mehradrige elektrische Leitungen fr allgemeine Verwendung XLETFE Familie Teil 008: BP - Kupfer vernickelt Betriebstemperaturen zwischen - 65 “C und 150 “C Doppelt extrudierte Isolier
5、ung fr externe Verwendung, mit zustzlichem Schutz in Gebieten mit hoher Vibration (Schwingung), bei Bewegung und bei Kontakt mit Flssigkeiten UV-Laser bedruckbar Produktnorm This “Aerospace Series“ frestandard has been drawn up under the responsibility of AECMA-STAN (The European Association of Aero
6、space 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. Subsequent to the publication of this frestandard, the technical content shall not be changed to a
7、n 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 submitted as a draft European Standard (prEN) to CEN (European Committee for Standardization) for
8、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 national standards conflicting with the EN. I I Copytight 2004 O by AECMA-STA1 Page 2 prEN
9、 461 1-008:2004 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 Publicat
10、ion . Contents Page 1 Scope 3 2 Normative 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 Pac
11、kaging, labelling and delivery lengths Technical specification 3 3 3 4 4 4 5 7 7 8 8 8 Page 3 prEN 461 1-008:2004 1 Scope This standard specifies the characteristics of UV laser printable, nickel plated copper conductor, electrical cables Crosslinked Ethylene Tetra Fluoro Ethylene co-polymer XLETFE
12、family for use in the on-board electrical systems of aircraft at operating temperatures between - 65 OC and 150 OC, operating at voltages not exceeding 600 V r.m.s and frequencies not exceeding 2 O00 Hz. These cables are intended for use with additional protection in areas where combinations of high
13、 vibration, cable flexing and fluid contamination are normal e.g. undercarriage harnesses. In case of conflict between this standard and other referenced documents the requirements of this standard shall take precedence. 2 Normative references This European Standard incorporates by dated or undated
14、reference provisions from other publications. These normative references are cited at the appropriate places in the text and the publications are listed hereafter. Dated references, subsequent amendments to or revisions of any of these publications apply to this European Standard only when incorpora
15、ted in it by amendment or revision. For undated references the latest edition of the publication referred to applies. EN 2084, Aerospace series - Cables, electric, single-core, general purpose, with conductors in copper or copper alloy - Technical specification ) EN 2235, Aerospace series - Single a
16、nd multicore electrical cables, screened and jacketed ) EN 3475-1 OO*, Aerospace series - Cables, electrical, aircraft use - Test methods - Part 700: General EN 461 1-002, Aerospace series - Cables, electrical, for general purpose, single and multicore assembly - XLETFE Family- Part 002: General ) E
17、N 9133, Aerospace series - Quality management systems - Qualifiation Procedure for Aerospace Standard Parts ) 3 Definitions and symbols See EN 3475-100. 4 Materials and construction 4.1 Materials Conductor The cable conductors shall be made of nickel plated copper according to EN 461 1-002. Insulati
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