AECMA PREN 4611-005-2004 Aerospace series Cables electrical for general purpose single and multicore assembly XLETFE Family Part 005 Silver plated copper Operating temperatures bet.pdf

1、AECMA STANDARD NORME AECMA AECMA NORM Edition approved for publication prEN 461 1-005 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 005: Silver plated copper Operating temperatures, between - 65 OC and 150 OC Single extruded wall for enclosed applications UV laser printable Product standard Srie arospatiale Cbles, lectriques, dusage gnral, mono et multiconducteurs Famille XLETFE Partie 005 : Cuivre argent Tempratures de

3、 fonctionnement comprises entre - 65 OC et 150 OC Fil simple isol pour applications internes Marquable au laser UV Norme de produit Luft- und Raumfahrt Ein- und mehradrige elektrische Leitungen fr allgemeine Vewendung XLETFE Familie Teil 005: Kupfer versilbert Betriebstemperaturen zwischen - 65 OC u

4、nd 150 OC Einfach extrudierte Isolierung fr interne (geschtzte) Verwendung UV-Laser bedruckbar Produktnorm 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

5、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 an extent that interchangeabilify is affected, physically or functio

6、nally, 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 formal vote and transformation to full European Standard (EN). The

7、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. 31 July 2004 after the date of publication to AECMA-STAN I I Copytight 2004 O by AECMA-STA1 Copyright Association

8、 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 1-005:2004 Foreword This standard was reviewed by the Domain Technical Coordinator of AECMA-STANS Electrical D

9、omain . 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 symbols .

10、 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 4 4 4 5 5 5 9 9 9 9 9 Copyright Association Europe

11、ene 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 1-005:2004 1 Scope This standard specifies the characteristics of UV laser printable, silver plated copper conductor,

12、 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 cables are

13、 for enclosed applications e.g. within equipment or conduit; they are only suitable for open airframe use when provided with additional protection against mechanical abuse. In case of conflict between this standard and other referenced documents this standard shall take precedence. 2 Normative refer

14、ences 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 revisions of any of these pu

15、blications 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 3475-loo*, EN 461 1-002, EN 9133, Aerospace series - Copper or copper alloy conductors for

16、 electrical cables - Product standard Aerospace series - Cables, electric, single-core, general purpose, with conductors in copper or copper alloy - Technical specification1) Aerospace series - Single and multicore electrical cables, screened and jacketed ) Aerospace series - Cables, electrical, air

17、craft 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 systems - Qualification Procedure for Aerospace Standard Parts 3 Definitions and symbols S

18、ee EN 3475-100. * 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 ResaleNo reproduction or networking permitted without license fr

19、om IHS-,-Page 4 prEN 461 1-005:2004 mm max. 4 Materials and construction 4.1 Materials Conductor The cable conductors shall be made of silver plated copper according EN 461 1-002 and EN 2083 code C. kg/km max. Insulation for conductor all size codes Single layer of extruded XLETFE For single core, i

20、t shall be possible to mark the outer insulation by UV laser printing. 0,82 0,91 1,08 1,35 1,59 1,82 2,29 2,74 4.2 Construction See EN 461 1-002, Table 1 and Table 2. 1,88 2,57 3,98 6,54 9,81 13,27 19,57 30,35 Table 1 - Single core cables Code for nominal section O01 002 004 006 o1 o o1 2 020 030 No

21、minal section mm2 AWG a 26 24 22 20 18 16 14 12 I 1 I Mass Linear External resistance I diameter at 20 OC Q/km mm max. I min. 149,O 106,O 553 31 ,O 19,6 14,9 10,2 64 0,72 0,81 0,98 1,19 1,44 1,56 1,93 2,37 Minimum insulation thickness mm 0,13 0,13 0,13 0,13 0,13 0,13 0,13 0,13 a AWG = Closest Americ

22、an Wire Gauge. Silver plated copper alloy conductor 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 5 prEN 461 1-005:2004 Size AWGa Max. dia. mm 1,6

23、4 1,82 2,16 2,70 3,18 3,64 4,58 5,48 Table 2 - Multicore without screen or jacket I I Mass max. kg/km 3,83 5,20 8,04 13,23 19,81 25,33 39,52 61,61 Max. dia. mm 1,77 1,97 2,33 2,92 3,43 3,93 4,95 5,92 DC Res. Q/km max. 153,5 109,2 60,O 31,9 20,2 15,3 10,5 6,6 Mass max. kg/km 5,74 7,90 12,05 19,84 29,

24、72 38,OO 59,29 92,41 Max. dia. mm 1,98 2,20 2,61 3,27 3,85 4,40 5,54 6,63 a AWG = Closest American Wire Gauge. Silver plated copper alloy conductor Mass max. kg/km 7,65 10,39 16,07 26,46 39,63 50,67 79,05 123,22 DC Res. Q/km max. O01 002 004 006 o1 o o1 2 020 030 153,5 109,2 60,O 31,9 20,2 15,3 10,5

25、 6,6 26 24 22 20 18 16 14 12 DC Res. Q/km max. 153,5 109,2 60,O 31,9 20,2 15,3 10,5 6,6 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. 5 Required characteristics According to EN 2084 and EN 3475-100 See Table 3. NOTE Tests EN 3475-302 to E

26、N 3475-706 shall be performed on the single core cables. 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 6 prEN 461 1-005:2004 Table 3 EN 3475- Test

27、 Details 20 1 Visual examination Applicable 202 Mass Applicable; see Table 1 and Table 2. 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,

28、 500 MQ.km minimum (95 f 2) OC, 1 MQ.km minimum 304 Surface resistance Applicable 12 500 MQ.mm minimum 305 Overload resistance Applicable Ti = (250 f 5) “Ci T2= (380 f 5) “C 40 1 Accelerated ageing Applicable Temperature (200 f 3) “C 402 Shrinkage and delamination Applicable Temperature (1 50 f 5) “

29、C Maximum shrinkage at each end of cable: 0,80 mm on size code O01 to 006 1 ,O0 mm on size code 012 to 012 1,20 mm on size code 020 to 050 403 Delamination and blocking Applicable Temperature (1 50 f 5) “C Applicable Temperatures (- 65 f 2) “C and (260 f 5) “C Maximum shrinkage at each end of cable:

30、 1 ,O0 mm on size code O01 to 050 404 Thermal shock 405 Bending at ambient temperature Cold bend test Applicable Applicable Temperature (- 65 f 2) “C Applicable Methods 1 and 2 Flame application 15 s Extinguishing time: 3 s max. 406 407 Flammability 408 Fire resistance Not applicable 409 Air-exclude

31、d ageing Not applicable 41 O Thermal endurance Applicable 50 O00 hours Temperature 150 “C 41 1 Resistance to fluids Applicable 41 2 Humidity resistance Applicable Method B Temperature (90 f 2) “C Duration 672 hours continued Copyright Association Europeene des Constructeurs de Materiel Aerospatial P

32、rovided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-Page 7 prEN 461 1-005:2004 Table 3 (continued) EN 3475- Test Details 41 3 Wrap back test Not applicable 414 Differential scanning calorimeter (DSC test) Not applicable 50 1 Dynamic

33、 cut-through Applicable single core Temperature (1 50 f 3) “C Size code Nominal section mm2 - force O0 1 002 004 006 o1 o o1 2 020 030 0,15 0,25 0,40 0,60 1 ,o0 1,20 2,oo 3,OO 502 503 Notch propagation Scrape abrasion Not applicable Applicable single core Temperature (1 50 f 3) “C Minimum number of

34、cycles = 50 Nominal section mm2 Size 020 030 0,15 0,25 0,40 0,60 0,95 1,35 1,80 3,OO 504 Torsion Not applicable 505 506 Tensile test on conductors and strands Plating continuity Applicable Applicable 507 Adherence of plating Applicable 508 Plating thickness Applicable 509 Solderability Applicable We

35、tting time 1 s max. 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 IHS-,-Page 8 prEN 461 1-005:2004 Size code Table 3 (concluded) Nominal section m

36、m2 O01 002 004 006 O10 012 020 030 0,15 0,25 0,40 0,60 1 12 2 3 Test Details EN 3475- 510 Applicable Tensile strength and elongation of extruded insulation, sheath and jacket material Cable to cable abrasion 51 1 Not applicable 51 2 Flexure endurance Applicable code 006 Mandrel 0 15 mm Weight 0,75 k

37、g - 750 cycles 60 1 Smoke density Applicable code 006 D, 50, 4 minutes 602 Toxicity Applicable code 006 603 604 Resistance to wet arc tracking Resistance to dry arc propagation Not applicable Not applicable 605 Wet short circuit test Not applicable 70 1 Strippability and adherence of insulation to t

38、he conductor Applicable min. N max. N 20 20 25 25 30 30 35 35 702 Screen pushback capability Not applicable Applicable 703 704 Permanence of manufacturers marking Flexibility Method 2 Size code Nominal section mm2 Force N Recoil Deg. Mandrel mm O0 1 002 004 006 - 0,15 0,20 0,40 0,60 20 20 25 25 70 7

39、0 60 60 15 15 15 15 705 Contrast measurement Applicable Laser marking K250% 706 Laser markability Not applicable Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license fro

40、m IHS-,-Page 9 prEN 461 1-005:2004 Description block CABLE, ELECTRICAL 6 Quality assu rance See EN 9133. Identity block EN461 1-005A010P 7 Designation EXAMPLE : Code Number letter of this for number standard of - cores (see EN 461 1-002, Table 2) 8 Identification and marking See EN 461 1-002. 9 See EN 2084. Packaging, labelling and delivery lengths 10 Technical specification 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-,-