AECMA PREN 4611-008-2004 Aerospace series Cables electrical for general purpose single and multicore assembly XLETFE Family Part 008 BP - Nickel plated cooper Operating temperature.pdf

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 Copyright A

9、ssociation Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-Page 2 prEN 461 1-008:2004 Foreword This standard was reviewed by the Domain Technical Coordinator of AECMA-STANS El

10、ectrical 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 Normative references . 3 3 4 4.1 4.2 4.3 4.4 5 6 7 8 9 10 Definitions and

11、 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 lengths Technical specification 3 3 3 4 4 4 5 7 7 8 8 8 Copyright Associat

12、ion 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 461 1-008:2004 1 Scope This standard specifies the characteristics of UV laser printable, nickel plated copper

13、conductor, electrical cables Crosslinked Ethylene Tetra Fluoro Ethylene co-polymer XLETFE 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

14、cables are intended for use with additional protection in areas where combinations of high 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 p

15、recedence. 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 listed hereafter. Dated references, subsequent amendments to or

16、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 2084, Aerospace series - Cables, electric, single-core, general purpose, with conductors

17、in copper or copper alloy - Technical specification ) EN 2235, Aerospace series - Single and 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,

18、 for general purpose, single and multicore assembly - XLETFE Family- Part 002: General ) EN 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

19、cable conductors shall be made of nickel plated copper according to EN 461 1-002. Insulation for conductor all size codes - first insulator extruded XLETFE, coloured blue; - second insulator extruded XLETFE. Coloured White for sizes 002, 006 and 010. Coloured light green for size 004 For single core

20、, it shall be possible to mark the outer insulation by UV laser printing. * And all its parts 1) Published as AECMA Prestandard at the date of publication of this standard Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for Resale

21、No reproduction or networking permitted without license from IHS-,-Page 4 prEN 461 1-008:2004 Code for nominal section 4.2 Construction See EN 461 1-002, Table 1 and Table 2. Nominal AWGa Linear section resistance at 20 OC Q/km mm2 max. Table 1 - Single core cables 002 006 o1 o 004 0,25 0,6 1 0,4 24

22、 22 20 18 114,O 60,O 33,2 21,l a AWG = Closest American Wire Gauge. Nickel plated copper alloy conductor DC Res. Maxi mum external diameter mm Max. dia. 1 ,O7 1,21 1,45 1,70 117,4 61,8 34,2 21,7 Mass kg/km max. 2,31 2,62 3,13 3,67 3,12 4,29 7,02 10,75 002 004 006 o1 o Minimum insulation thickness mm

23、 24 2,14 6,43 22 2,43 8,84 20 2,90 14,46 18 3,40 22,15 0,20 0,20 0,20 0,20 Table 2 - Multicore without screen or jacket Size I AWG I 2 core I 3 core I - I I Max. I Mass a AWG = Closest American Wire Gauge. Nickel plated copper alloy conductor Mass DC Res. Q/km max. Q/km max. I mm I kg/km I max. 9,64

24、 13,25 21,69 33,22 1 17,4 61,8 34,2 21,7 4.3 Number of cores See EN 461 1-002. See EN 2235 for cabling. 4.4 Colour coding of cores See EN 461 1-002. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or netw

25、orking permitted without license from IHS-,-Page 5 prEN 461 1-008:2004 5 Required characteristics According to EN 2084 and EN 3475-100 See Table 3. NOTE Tests EN 3475-302 to EN 3475-706 shall be performed on the single core cables. Table 3 EN 3475- Test Details 201 Visual examination Applicable Appl

26、icable; see Table 1 and Table 2. 202 Mass 203 Dimensions Applicable; see Table 1 and Table 2. 30 1 Ohmic resistance per unit length Applicable; see Table 1 and Table 2. 302 Voltage proof test Applicable 303 Insulation resistance Applicable (20 f 2) OC, 500 MQ.km minimum (95 f 2) OC, 1 MQ.km minimum

27、Applicable 12 500 MQ.mm minimum Applicable Ti = (250 f 5) “Ci T2= (380 f 5) “C 304 Surface resistance 305 Overload resistance 40 1 Accelerated ageing Applicable Temperature (200 f 3) “C 402 Shrinkage and delamination Applicable Temperature (1 50 f 5) “C Maximum shrinkage at each end of cable: 0,80 m

28、m on size code 002 to 006 1 ,O0 mm on size code O10 403 Delamination and blocking Applicable Temperature (1 50 f 5) “C 404 Thermal shock Applicable Temperatures (- 65 f 2) “C and (260 f 5) “C Maximum shrinkage at each end of cable: 1 ,O0 mm 405 Bending at ambient temperature Applicable 406 Cold bend

29、 test Applicable Temperature (- 65 f 2) “C 407 Flammability Applicable Methods 1 and 2 Flame application 15 s Extinguishing time: 3 s max. 408 Fire resistance Not applicable 409 Air-excl uded age ng Thermal endurance Not applicable Applicable 60 O00 hours Temperature 150 “C 41 O 41 1 Resistance to f

30、luids Applicable No crazing or delamination, 5 % maximum swell, colour changes or removal of marking continued Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from

31、IHS-,-Page 6 prEN 461 1-008:2004 Size code Table 3 (continued) Nominal Load section mm2 N Test Details EN 3475- 41 2 Humidity resistance Applicable Method B Temperature (90 f 2) “C Duration 672 hours 41 3 41 4 Wrap back test Differential scanning calorimeter (DSC test) Not applicable Not applicable

32、50 1 Dynamic cut-through Not applicable 502 Notch propagation Applicable Notch depth 40 pm 503 Scrape abrasion Applicable Temperature (20 f 3) “C Minimum number of cycles for size 24 100 All other sizes 150 002 0,25 006 0,6 O10 1 004 0,4 504 Torsion Not applicable 505 Tensile test on conductors and

33、strands Applicable 506 507 Plating continuity Adherence of plating Applicable Applicable 508 Plating thickness Applicable 509 510 Solderability Tensile strength and elongation of extruded insulation, sheath and jacket material Not applicable Applicable 35 MPa and 75 % 51 1 Cable-to-cable abrasion Ap

34、plicable size code 006 Load 1 kg - 6 O00 O00 cycles 51 2 Flexure endurance Applicable code 006 Mandrel 0 15 mm Weight 0,75 kg - 750 cycles Applicable code 006 D, 50, 4 minutes 60 1 Smoke density 602 Toxicity Applicable code 006 603 Applicable or use EN 3475-605 as an alternative Wire damage 70 mm 75

35、 % of collateral wires shall not be open circuit wet dielectric voltage proof test (EN 3475-302) not applicable Resistance to wet arc tracking continued Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or

36、networking permitted without license from IHS-,-Page 7 prEN 461 1-008:2004 Description block CABLE, ELECTRICAL Table 3 (concluded) Identity block EN461 1 -0OSAOlO EN 3475- 604 605 70 1 702 703 704 705 706 Test Resistance to dry arc propagation Wet short circuit test Strippability and adherence of in

37、sulation to the conductor Screen pushback capability Permanence of manufacturers marking Flexibility Contrast measurement Laser markability Details Applicable Wire damage 70 mm 75 % of collateral wires shall pass the wet dielectric voltage proof test at 1 ,O kV r.m.s. (EN 3475-302) Applicable Applic

38、able Not applicable Applicable Method 2 Size code - 002 004 006 section 0,40 0,60 Recoil Mandrel kl Applicable Laser marking K250% Not applicable 6 Quality assu rance See EN 9133. 7 Designation EXAMPLE: Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under l

39、icense with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-Page 8 prEN 461 1-008:2004 8 Identification and marking See EN 461 1-002. 9 See EN 2084. Packaging, labelling and delivery lengths 10 Tech n i cal s peci f icat io n See EN 2084. See EN 2235. 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-,-