1、AECMA STANDARD NORME AECMA AECMA NORM Edition approved for publication prEN 461 1-006 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 006: Silver plated copper Operating temperatures, between - 65 OC and 150 OC Dual extruded wall for open applications UV laser printable Product standard Srie arospatiale Cbles, lectriques, dusage gnral, mono et multiconducteurs Famille XLETFE Partie 006 : Cuivre argent Tempratures de fonct
3、ionnement comprises entre - 65 OC et 150 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 006: Kupfer versilbert Doppelt extrudierte Isolierung fr externe Ver
4、wendung UV-Laser bedruckbar Produktnorm Betriebstemperaturen zwischen - 65 OC und 150 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 Ae
5、rospace 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-
6、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 CEN national membe
7、rs 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 Europeene des Con
8、structeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-Page 2 prEN 461 1-006:2004 Foreword This standard was reviewed by the Domain Technical Coordinator of AECMA-STANS Electrical Domain . After inqu
9、iries 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 . Materials and con
10、struction 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 Europeene des Constructe
11、urs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-Page 3 prEN 461 1-006:2004 1 Scope This standard specifies the characteristics of UV laser printable, silver plated copper conductor, electrical cables
12、 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 suitable for airf
13、rame use without additional protection. 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 reference provisions from other publications. These
14、 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 incorporated in it by amendment or revision. For undated ref
15、erences the latest edition of the publication referred to applies. EN 2083, EN 2084, EN 2235, EN 3475-1 OO*, 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 co
16、nductors in copper or copper alloy - Technical specification ) Aerospace series - Single and multicore electrical cables, screened and jacketed ) Aerospace series - Cables, electrical, aircraft use - Test methods - Part 700: General Aerospace series - Cables, electrical, for general purpose, single
17、and multicore assembly - XLETFE Family- Part 002: General ) Aerospace series - Quality management systems - 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 standar
18、d 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 461 1-006:2004 4 Materials and construction 4.1 Materials Conductor The cable conductors sh
19、all be made of silver plated copper according to EN 461 1-002 and EN 2083 code C. 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
20、the outer insulation by UV laser printing. 4.2 Construction See EN 461 1-002, Table1 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 18
21、16 14 12 10 8 6 4 3 1 O Linear resistance at 20 OC Q/km max. 149,O 106,O 55,3 31 ,O 19,6 14,9 10,2 64 1,37 0,87 0,56 0,46 0,28 0,22 4,o Maximum external diameter mm 1 ,o0 1,16 1,26 1,50 1,74 1,87 2,44 2,95 3,61 5,16 6,38 8,13 10,67 13,36 14,88 Mass kg/km max. 2,31 3,28 4,57 7,15 10,54 13,48 20,63 31
22、,51 48,80 92,12 140,63 235,13 370,55 601,22 744,08 Minimum insulation thickness mm 0,20 0,20 0,20 0,20 0,20 0,20 0,20 0,20 0,20 0,20 0,20 0,20 0,20 0,20 0,20 a AWG = Closest American Wire Gauge Silver plated copper alloy conductor Copyright Association Europeene des Constructeurs de Materiel Aerospa
23、tial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-Page 5 prEN 461 1-006:2004 Max. dia. mm Table 2 - Multicore without screen or jacket I I I I Mass DC Res. max. Q/km kg/km max. Size I AWG I 2 core 3 core I O01 002 004 006 o1
24、 o o1 2 020 030 050 26 24 22 20 18 16 14 12 10 2,16 2,51 2,72 3,24 3,76 4,41 5,27 6,37 7,80 2,oo 2,32 2,52 3,OO 3,48 3,74 4,88 5,90 7,22 7,04 9,97 13,85 21,74 31,93 41,05 62,51 95,46 147,86 4,69 6,65 9,23 14,49 21,29 27,37 41,67 63,64 98,57 2,42 2,81 3,05 3,63 4,21 433 5,90 7,14 8,74 1533 109,2 60,O
25、 31,9 20,2 15,3 103 6,6 431 9,39 13,30 18,47 28,98 42,57 54,74 83,34 127,29 197,14 a AWG = Closest American Wire Gauge. Silver plated copper alloy conductor dia. kg/km DC Res. Q/km max. Max. dia. mm 4 core Mass max. kg/km 1533 109,2 60,O 31,9 20,2 15,3 103 6,6 431 DC Res. Q/km max. 1533 109,2 60,O 3
26、1,9 20,2 15,3 103 6,6 431 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 EN 3475-706 shall be performed on the single core cables. Copyr
27、ight 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 1-006:2004 Table 3 Test EN 3475- Details 20 1 Visual examination Applicable 202 Mass Applicabl
28、e; see Table 1 and Table 2. 203 30 1 Applicable; see Table 1 and Table 2. Applicable; see Table 1 and Table 2. Dimensions Ohmic resistance per unit length 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 304 Surface re
29、sistance 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) “C Maximum shrinkage at each end of cable: 0,80 mm on size code
30、 O01 to 006 1 ,O0 mm on size code O10 to 012 1,20 mm on size code 020 to 050 Applicable Temperature (1 50 f 5) “C 403 Delamination and blocking 404 Thermal shock Applicable Temperatures (- 65 f 2) “C and (260 f 5) “C Maximum shrinkage at each end of cable: 1 ,O0 mm on size code O01 to 050 405 Bendin
31、g at ambient temperature Applicable 406 Cold bend 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-excluded ageing Not applicable 41 O Thermal endurance Applicable 50 O
32、00 hours Temperature 150 “C 41 1 41 2 Resistance to fluids Humidity resistance Applicable 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 continued Copyright Association Europeene des C
33、onstructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-Page 7 prEN 461 1-006:2004 Table 3 (continued) EN 3475- Test Details 50 1 Dynamic cut-through Applicable single core Temperature (1 50 f 3) “C
34、 Size code Nominal section mm2 Cut-through force N O0 1 002 004 006 o1 o o1 2 020 030 050 O90 140 220 340 530 680 0,15 0,25 0,6 1 12 2 3 5 9 14 22 34 53 68 0,4 15 20 25 25 25 25 25 25 25 25 25 25 25 25 25 502 Notch propagation Applicable Notch depth 40 pm 503 Scrape abrasion Applicable single core T
35、emperature (1 50 f 3) “C Minimum number of cycles = 100 Size code Nominal section mm2 Load N O0 1 002 004 006 o1 o o1 2 020 030 050 O90 140 220 340 530 680 0,15 0,25 0,6 1 12 2 3 5 9 14 22 34 53 68 0,4 504 Torsion Not applicable 505 Tensile test on conductors and strands Applicable 506 Plating conti
36、nuity Adherence of plating Applicable Applicable 507 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 1-006:2004 Size code Table
37、 3 (continued) Nominal section m m2 O01 O02 006 O10 012 020 030 050 O90 140 220 340 420 530 680 004 0,15 025 0,60 1 12 2 3 5 9 14 22 34 42 53 68 0,40 EN 3475- Test Details 508 Plating thickness Applicable 509 Solderability Applicable Wetting time 1 s max. 510 Tensile strength and elongation of extru
38、ded insulation, sheath and jacket material Not applicable 51 1 Cable to cable abrasion Applicable 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 60 1 Smoke density Applicable code 006 D, 50, 4 minutes 602 Toxicity App
39、licable code 006 603 Resistance to wet arc tracking Applicable Wire damage 70 mm 75 % of collateral wires shall not be open circuit wet dielectric voltage proof test (EN 3475-302) not applicable 604 Resistance to dry arc propagation Applicable Wire damage 70 mm 75 % of collateral wires must pass the
40、 wet dielectric voltage proof test at 1 kV r.m.s. (EN 3475-302) 605 Wet short circuit test Strippability and adherence of insulation to the conductor Not applicable Applicable 70 1 min. N max. N 5,O 5,O 5,O 83 12,5 12,5 12,5 15 20 20 20 20 20 20 20 20 20 20 25 25 30 30 35 35 40 40 40 40 40 40 40 40
41、702 Screen pushback capability Permanence of manufacturers marking Not applicable Applicable 703 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-
42、,-Page 9 prEN 461 1-006:2004 Recoil Deg. Table 3 (concluded) Mandrel mm EN 3475- 70 70 60 60 704 15 15 15 15 Test 706 Flexibility Laser markability 705 I Contrast measurement I 6 Quality assu rance See EN 9133. 7 Designation EXAMPLE: Number of this standart Description block Details Method 2 Size co
43、de - O0 1 002 004 006 Nominal section mm2 0,15 0,25 0,40 0,60 Force N 5 10 15 15 Applicable Laser marking K250% Not applicable Identity block CABLE, ELECTRICAL I EN461 1-006A010 TT Code letter for number of cores (see EN 461 1-002, Table 2) - Code for nominal section (see Table 1) Code letter for co
44、lour coding of cores (see EN 461 1-002) 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-,-
