AECMA PREN 2084-2000 Aerospace Series Cables Electric Single-Core General Purpose with Conductors in Copper or Copper Alloy Technical Specification Edition P 1《航空航天系列.一般用途单核铜及铜合金电缆.pdf

《AECMA PREN 2084-2000 Aerospace Series Cables Electric Single-Core General Purpose with Conductors in Copper or Copper Alloy Technical Specification Edition P 1《航空航天系列.一般用途单核铜及铜合金电缆.pdf》由会员分享，可在线阅读，更多相关《AECMA PREN 2084-2000 Aerospace Series Cables Electric Single-Core General Purpose with Conductors in Copper or Copper Alloy Technical Specification Edition P 1《航空航天系列.一般用途单核铜及铜合金电缆.pdf（9页珍藏版）》请在麦多课文档分享上搜索。

1、STD-AECMA PREN 208q-ENGL 2000 30123LL 0038849 512 m - - - AECMA STANDARD prEN 2084 NORME AECMA Edition P 1 AECMA NORM October 2000 PUBLISHED BY THE EUROPEAN ASSOCIATION OF AEROSPACE INDUSTRIES (AECMA) Gulledelle 94 - 6-1200 BRUXELLES - Tel. (42) 2 775 81 1 O - Fax. ($32) 2 i75 81 11 ICs: Descriptors

2、: ENGLISH VERSION Aerospace series Cables, electric, single-core, general purpose, with conductors in copper or copper alloy Technical specification Srie arospatiale Cbles lectriques, monoconducteurs, dusage gnral, avec conducteurs en cuivre ou en alliage de cuivre Spcification technique Luft- und R

3、aumfahrt Elektrische Leitungen, elnadrlg, fr allgemeine Verwendung, mit Leitern aus Kupfer oder Kupferlegierung Technische Lieferbedingungen This “Aerospace Series“ Prestandard has been drawn up under the responsibility of AECMA (The European Association of Aerospace Industries). It is published on

4、green paper for the needs of AECMA- Members. It has been technically approved by the experts of the concerned Technical Committee following comment by the Member countries. Subsequent to the publication of this Prestandard, the technical content shall not be changed to an extent that interchangeabil

5、ity is affected, physically or functional/y, without re-identification of the standard. After examination and signature of the AECMA Standard Checking Centre (NPS) and formal agreement of the Official Services of the Member countries it will be submitted as a draft European Standard to CEN (European

6、 Committee for Standardization) for formal vote. Nota - Extra copies can be supplied by B.N.A.E. - Technopolis 54 - 199, rue Jean-Jacques Rousseau - 92138 ISSY-LES-MOULINEAUX CEDEX I I Edition approved for publication 1 Comments should be sent within six months after the date of oublication to AECMA

7、 I Gulledelle 94 2000-1 0-31 I 8-1200 BRUXELLES I C2 Chairman Mr Peuetta I I Q aecrna 2000 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 2 prEN

8、2084: 2000 Contents Page . Normative references . 3 . 3 Materials and construction of cables 3 . 4 Tests methods . Quality assurance 7 Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitt

9、ed without license from IHS-,-,-Page 3 prEN 2084: 2000 1 Scope This standard specifies the characteristics, test methods, qualification and acceptance conditions of single- core electric cables for general purpose with conductors in copper or copper alloy, intended for installation in aircraft circu

10、its. The insulation of these cables is designed to withstand a maximum service voltage of 600 V r.m.s. at a frequency not exceeding 2 O00 Hz. They are divided into types, the characteristics of which are given in the product standards. Unless otherwise specified in the product standard, the tests de

11、fined in this standard apply. 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. For dated references, subse

12、quent 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. IS0 2574 EN 2083 EN 3042 EN 3475-1 00* EN 3838 Aircraft - Electrical

13、cables - Identification marking Copper and copper alloy conductors for electrical cables - Aerospace series 1) Aerospace series - Quality assurance - EN aerospace products - Qualification procedure Aerospace series - Cables, electrical, aircraft use - Test methods - Part 100: General 2) Aerospace se

14、ries - Requirements and test on user-applied markings on aircraft electrical cables 2) 3 Definitions and symbols For the purposes of this standard, the definitions given in EN 3475-100 apply. 4 Materials and construction of cables 4.1 Conductors They shall conform to EN 2083 unless otherwise specifi

15、ed. 4.2 Finished cables The insulation material shall present a uniform circular cross-section throughout the length of the cable. Covering over the insulation shall be treated and applied in such a manner that the cables present a smooth appearance and are able to accept marking. All materials used

16、 shall have no corrosive effect upon the conductors and shall not be susceptible to attack by mould or other micro-organisms. And all parts of this series quoted in table 1 1) Published as AECMA Standard at the date of publication of this standard 2) Published as AECMA Prestandard at the date of pub

17、lication 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 from IHS-,-,-STD-AECMA PREN 208Li-ENGL 2000 1OL23Ll 0038852 O07 = 201 202 3 X 3 X 301 302

18、3 X 3 X X 40 1 Mandrel 0 and test load: table 4 Temperature: product standard 3 402 Temperature: product standard 403 Mandrel diameter: table 4 Temperature: product standard 3 3 Page 4 prEN 2084: 2000 5 Req u red characteristics The characteristics of the cables, tested according to the methods desc

19、ribed hereafter shall comply with the values given in the product standard. 6 Tests methods See table 1. Table 1 - Tests: methods, application, requirements Tests 1 Each delivery II Requirements (and/or particulars) Test conditions FLlL 1 O0 Ixlxlx XI Marking: according 9 8 Minimum length: 0,5 m 6.2

20、 I Mass 6.3 Dimensions (ali) - outer diameter Conductor: EN 2083 unless otherwise specified Product standard Product standard 2,5 kV r.m.s. 5 kV r.m.s. 8 kV peak voltage Electrical resistance per unit length Voltage proof test: immersion test dry test or dry impulse test (Alternative to dry test) 6.

21、4 6.5 6.6 131 303 For a length of 1 km: 1 500 MSZ minimum 15 MQ minimum Insulation resistance at 20 I2 “C at 95 I2 OC Surface resistance X 2 304 131 6.7 Minimum: 1 250 MS2 mm Applicable to cable of 0,6 mm2 only T1 and T2: product standard 6.9 Accelerated ageing X 6.1 O Shrinkage and delamination X P

22、roduct standard 6.1 1 Delamination and blocking X (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-,-,-STD*AECMA PREN 2084-ENGL 2000 W LOL23LL 0

23、018853 T43 W 502 Cut depth: product standard 503 Load: product standarc Page 5 prEN 2084: 2000 407 409 Temperature and time: product standard Table 1 - Tests: methods, application, requirements (continued) 505 I Tests 6.21 6.22 6.23 6.24 Differential scanning calorimeter (DSC) test Dynamic cut- thro

24、ugh Notch propagation Scrape abrasion 6.25 Torsion 6.26 Tensile test on conductors and strands EN 3475- and additional details, it any Requirements (andor particulars) 6.12 Thermal shock T- 404 Temperature: product standard 405 Mandrel diameter: table 4 roduct standard 3 3 3 3 X l/fluid 3 6.14 Coidb

25、end test -I 406 Mandrel 0 and test load: table 4 Voduct standard ageing 6.17 Thermal endurance I 41 O roduct standard 4pplicable to cable of ),6 mm2 only Ipplicable to cable of 1,6 mm2 only 6.1 8 Resistance to fluids 6.19 Humidity -I- resistance 41 l 41 2 if method B: temperature and time: product s

26、tandard Method A or 0 as requestec n product standard 6.20 Wrap back test I 413 X Applicable to cables 2 5 mm2 41 4 X X Product standard (arithmetic mean value of 8 tests per specimen) 501 (for insulation wall thickness s 0,38 mm) X X Product standard (Requirements to be considered at 20 “C unless o

27、therwise specified) Applicable to cables I 5 mrn2 504 Test load: table 4 T3 and T4: product standard EN 2083 unless otherwise specified 6.27 I Plating continuity I 506 (continued) Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot fo

28、r ResaleNo reproduction or networking permitted without license from IHS-,-,-h Y I .si y = un na V 1 Zb alal I Requirements (and/or particulars) EN 2083 unless otherwise specified X Product standard Smoke density Toxicity Resistance to wet arc tracking 601 X 602 X 603 X Resistance to dry arc propaga

29、tion Wet short circuit test 604 X 605 X Page 6 prEN 2084: 2000 Table 1 - Tests: methods, application, requirements (concluded) Tests 1 1 I Eachc!elivery No. Adherence of plating Plating thickness 6.28 6.29 Solderability I 509 131 lx I Product standard 6.30 6.31 Tensile strength and elongation of ext

30、ruded insulation, sheath and jacket material 51 O 4 X Product standard 6.32 Cable to cable abrasion 51 1 Weight: product standard 1 6.33 Flexure endurance 51 2 Mandrel diameter and weight: product standard 3 X I Product standard Product standard Product standard 6.34 6.35 6.36 I Product standard 6.3

31、7 6.38 Product standard Product standard 6.39 Strippability and adherence of insulation to the conductor 701 Adherence force minimum : table 5 Product standard X Product standard Product standard 6.40 Permanence of manufacturers marking 703 Flexibility I 704 6.41 6.42 Permanence of user-applied mark

32、ing Contrast measurement prEN 3838 705 Laser parameters: EN3475-706 I Number of specimens per cross-section for each test unless otherwise specified. In preparation at the date of publication of this standard Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS u

33、nder license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Page 7 prEN 2084: 2000 0,15 0,25 0,6 2 9 53 7 Quality assurance 26 0,25 24 24 0,15 26 20 0,4 to 1 22 to 18 14 1,2 to 5 16 to 10 8 9 to 34 8 to 2 O 42 to 107 1 to0000 7.1 Qualification 7.1.1 Gene

34、ral requirements See EN 3042. 7.1.2 Qualification conditions The cables shall be submitted for qualification tests on drums, spools or in coils in sufficient lengths, wound evenly and uniformly. Each drum, spool or coil shall have a label containing information given in 9.1. 7.1.3 Qualification test

35、s See table 1. 7.1.4 Extension of qualification The qualification granted may be applicable to adjacent cross-sections in accordance with table 2. Table 2 - Qualified cables and extension of qualification I Qualified cables I Cables covered by the same qualiflcatlon AWG a Nominal cross sectlon mm2 A

36、WG a Nominal cross section mm2 For cross sections 9 mm2 to 107 mm2, different reference cross-section may be selected after agreement with the Design Authority. 7.2 Acceptance tests 7.2.1 Required conditions See table 1. The acceptance tests shall be carried out on cables delivered against an order

37、to check that the cable characteristics are maintained. 7.2.1.1 The cables which fail any of the tests specified in 7.2.2 shall be rejected. Tests to be carried out on all cables 7.2.1.2 Ramdom sampling tests: retest If any of the specimens fails one of the tests specified in 7.2.3, that test shall

38、be repeated on another set of specimens of the same cross-section selected at random from the same batch. If one of these new specimens fails the test, the batch submitted for acceptance shall be rejected. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS unde

39、r license with AECMANot for ResaleNo reproduction or networking permitted without license from IHS-,-,-7.2.2 Production routine tests The tests shall be carried out on all cables delivered. See table 1. Minimum acceptable continuous lengths for at least 85 % of cables delivered m 7.2.3 Tests prior t

40、o delivery They shall be carried out by sampling on each delivery batch. See table 1. Minimum acceptable continuous lengths for not more than 15 % of cables delivered m 7.2.4 Periodic tests They shall be carried out by sampling at least every three years. See table 1. mm2 0,15 to 1 1,2 to 3 5 9 to 1

41、07 8 Identification marking 26 to 18 16 to 12 10 8 to O000 Unless otherwise specified, the type, cross section and a reference for identification of country of origin, manufacturer, and the year of manufacture shall be indelibly marked on the cables, in accordance with IS0 2574. 150 1 O0 70 9 Packag

42、ing, labelling and delivery lengths 30 20 20 9.1 Packaging and labelling Cables supplied on drum, spools or in coils shall be wound evenly and uniformly. All cable ends shall be easily accessible and protected where necessary. Each drum, spool or coil shall have a label indicating: - manufacturers n

43、ame and designation; - cable designation according to the EN product standard; - batch number; - date of manufacture (month, year); - inspectors mark; - total length and length of each piece of cable in metres from inside to outside. 9.2 Delivery lengths They shall conform to table 3 unless otherwis

44、e specified. Table 3 - Delivery lengths I Nominal conductor cross-section AWG a I I a AWG: Closest American Wire Gage. Copyright Association Europeene des Constructeurs de Materiel Aerospatial Provided by IHS under license with AECMANot for ResaleNo reproduction or networking permitted without licen

45、se from IHS-,-,- STDmAECMA PREN 2084-ENGL 2000 3t332331 0038857 by7 Code O01 002 004 o1 o 012 020 030 050 O90 140 220 340 420 530 680 850 107 006 Page 9 prEN 2084: 2000 Mandrel Test diameter load AWG a Nominal conductor cross-section mm2 mm N 0,15 26 215 0,25 24 3,5 0,4 22 5 1 ,o 18 the maximum 10 1

46、2 16 cable diameter 10 210 14 15 3,o 12 15 5,O 10 15 9 8 16 times 45 14 6 the maximum 45 22 4 cable diameter 45 34 2 75 75 120 42 1 120 53 O 150 68 O0 85 O00 107 O000 150 0,6 20 12 times 715 22 times the maximum cable diameter Tabie 4 - Mandrel diameter and test load Code O0 1 002 004 006 o1 o o1 2

47、020 030 050 Adhesion force minimum AWG a Nominal conductor cross-section mm2 N 0,15 26 5 0,25 24 5 0,4 22 5 086 20 8,s 1 ,o 18 12,5 12 16 16 280 14 18 380 12 22 5,o 10 22 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-,-,-