AECMA PREN 3545-002-2006 Aerospace series Connectors electrical rectangular with sealed and non-sealed rear plastic housing locking device operating temperatures - 55 to 175 P.pdf

1、ASD STANDARD NORME ASD ASD NORM prEN 3545-002 Edition P 5 December 2006 PUBLISHED BY THE AEROSPACE AND DEFENCE INDUSTRIES ASSOCIATION OF EUROPE - STANDARDIZATION Gulledelle 94 - B-1200 Brussels - Tel. + 32 2 775 8126 - Fax. + 32 2 763 3565 - www.asd-stan.orgICS: 49.060 Supersedes edition P 4 Septemb

2、er 2004 Will supersede EN 3545-002:2005 Descriptors: ENGLISH VERSION Aerospace series Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures 55 C to 175 C Part 002: Specification of performance and contact arrangements Srie arosp

3、atiale Connecteurs lectriques, rectangulaires, tanches et non tanches larrire, botier en plastique, verrouillage, tempratures dutilisation 55 C 175 C Partie 002 : Spcification de performances et darrangements des contacts Luft- und Raumfahrt Elektrische Rechtecksteckverbinder mit und ohne hintere Ab

4、dichtung, Plastikgehuse, Verriegelungssystem, Betriebstemperaturen von 55 C bis 175 C Teil 002: Leistungsdaten und Kontaktanordnungen This “Aerospace Series“ Prestandard has been drawn up under the responsibility of ASD-STAN (The AeroSpace and Defence Industries Association of Europe - Standardizati

5、on). 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 Prestandard, the technical content shall not be changed to an extent that interchangeability

6、 is affected, physically or functionally, without re-identification of the standard. After examination and review by users and formal agreement of ASD-STAN, it will be submitted as a draft European Standard (prEN) to CEN (European Committee for Standardization) for formal vote and transformation to

7、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. Edition approved for publication 31 December 2006 Comments should be sent within

8、 six months after the date of publication to ASD-STAN Electrical Domain Copyright 2006 by ASD-STAN Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3545-002:20062 Co

9、ntents Page Foreword2 1 Scope 3 2 Normative references 3 3 Terms and definitions .4 4 Operating conditions.5 5 List of product standards .8 6 Polarization Coding 8 7 Contact arrangements.9 8 Contacts. 13 9 Filler plugs. 13 10 Rear accessory . 13 11 Tooling . 13 12 Assembly and wiring instructions 13

10、 Foreword This standard was reviewed by the Domain Technical Coordinator of ASD-STANs Electrical Domain. After inquiries and votes carried out in accordance with the rules of ASD-STAN defined in ASD-STANs General Process Manual, this standard has received approval for Publication. Copyright European

11、 Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3545-002:20063 1 Scope This standard specifies conditions which are common to rectangular electrical connectors with sealed and non-se

12、aled rear, plastic housing, locking device, for operating temperatures from 55 C to 175 C. It shall be used together with EN 3545-001. 2 Normative references The following referenced documents are indispensable for the application of this document. For dated references, only the edition cited applie

13、s. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 2591-100, Aerospace series Elements of electrical and optical connection Test methods Part 100: General. EN 2591-209, Aerospace series Elements of electrical and optical connection Test me

14、thods Part 209: Current temperature derating. EN 3155-002, Aerospace series Electrical contacts used in elements of connection Part 002: List and utilization of contacts. EN 3155-003, Aerospace series Electrical contacts used in elements of connection Part 003: Contacts, electrical, female, type A,

15、crimp, class S Product standard. EN 3155-008, Aerospace series Electrical contacts used in elements of connection Part 008: Contacts, electrical, male, type A, crimp, class S Product standard. EN 3155-070, Aerospace series Electrical contacts used in elements of connection Part 070: Contacts, electr

16、ical, male, type A, crimp, class S Product standard.1)EN 3155-071, Aerospace series Electrical contacts used in elements of connection Part 071: Contacts, electrical, female, type A, crimp, class S Product standard. 1)EN 3197, Aerospace series Installation of aircraft electrical and optical intercon

17、nection systems. 1)EN 3545-001, Aerospace series Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures 55 C to 175 C Part 001: Technical specification. EN 3545-003, Aerospace series Connectors, electrical, rectangular, with seal

18、ed and non-sealed rear, plastic housing, locking device, operating temperatures 55 C to 175 C Part 003: Connectors with female contacts Product standard. EN 3545-004, Aerospace series Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating tem

19、peratures 55 C to 175 C Part 004: Connectors with male contacts Product standard. EN 3545-005, Aerospace series Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures 55 C to 175 C Part 005: Female coding and attachment system fo

20、r mounting on free housing (plug) Product standard. 1)1) Published as AECMA Prestandard at the date of publication of this standard. Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license f

21、rom IHS-,-,-prEN 3545-002:20064 EN 3545-006, Aerospace series Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures 55 C to 175 C Part 006 : Male coding and attachment system for mounting on fixed housing (receptacle) Product st

22、andard. 1)EN 3545-007, Aerospace series Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures 55 C to 175 C Part 007: Cable clamp Product standard. EN 3545-008, Aerospace series Connectors, electrical, rectangular, with sealed a

23、nd non-sealed rear, plastic housing, locking device, operating temperatures 55 C to 175 C Part 008: Tools for assembly/removal of coding and attachment systems Product standard. EN 4529-002, Aerospace series Elements of electrical and optical connection Sealing plugs Part 002: Index of product stand

24、ards. 3 Terms and definitions For the purposes of this document, the terms and definitions given in EN 2591-100 apply. Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-pr

25、EN 3545-002:20065 4 Operating conditions 4.1 Installation principle See Figure 1. Key 1 Panel 2 Connector with female or male contacts (see EN 3545-003 or EN 3545-004) 3 Female coding and attachment system for mounting on free housing (see EN 3545-005) 4 Male coding and attachment system for mountin

26、g on fixed housing (see EN 3545-006) 5 Cable clamp (see EN 3545-007) 6 Connector with female or male contacts (see EN 3545-003 or EN 3545-004) Figure 1 4.2 Combination of connectors The combination of a male housing connector with a female housing connector is possible only if: the contact layout; t

27、he attachment/coding systems; are correctly associated. 4.3 Plug/connector coupling Not applicable 2 3 1 6 5 4 Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3545-

28、002:20066 4.4 Permissible cables The performance of these connectors is achieved with the cables of the dimensions given in Table 1 and using the accessories and wiring tools specified. Table 1 External wire diameter mm Contact size min. max. 22 a0,75 1,27 22 b0,75 1,45 20 0,85 1,80 16 1,20 2,40 12

29、1,90 3,70 10 2,38 5,20 8 c c aFor arrangement 02 and 03. bFor arrangement 12 and 13. cThe cables for size 8 contacts are specified in the contact product standard. The use of cables exceeding the maximum diameter indicated is prohibited. Cables smaller than the minimum diameter may be used, subject

30、to a concession, provided that the requirements according to EN 3197 are observed. 4.5 Operating characteristics 4.5.1 Electrical conditions These conditions are: insulating resistance at ambient temperature: 5 000 M withstand voltage (sea level): contact size 22: 1 500 V r.m.s.; contact sizes 20, 1

31、6, 12, 10 and 8: 1 500 V r.m.s. permissible nominal current in contacts Table 2 specifies the permissible nominal current at extreme temperatures in the contacts, according to their size and to the wire used. Heating due to current flow should not cause the maximum temperature to be exceeded. See EN

32、 2591-209. Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3545-002:20067 Table 2 Size Conductor size Intensity Contact Barrel Section mm AECMA code AWG a A 0,40 00

33、4 22 5 0,25 002 24 3 22 22 0,15 001 26 2 0,60 006 20 7,5 0,40 004 22 5 20 20 0,25 002 24 3 1,00 010 18 7,5 0,60 006 20 7,5 0,40 004 22 5 20 18 0,25 002 24 3 1,20 012 16 13 1,00 010 18 10 16 16 0,60 006 20 7,5 2,00 020 14 13 1,20 012 16 13 1,00 010 18 10 16 14 0,60 006 20 7,5 3,00 030 12 23 12 12 2,0

34、0 020 14 17 5,00 051 10 33 10 10 3,00 030 12 23 8 b bbbbaAWG: closest American Wire Gage. bSee contact product standard. 4.5.2 Climatic conditions Continuous test in damp heat: 56 d Operating temperatures: minimum temperature: 55 C; maximum temperature: 175 C. Furthermore, the connector operating te

35、mperature shall be limited to the maximum operating temperature indicated in the contact product standards. Salt mist: duration 48 h 4.5.3 Mechanical conditions Mechanical endurance: 100 mating and unmating operations Copyright European Association of Aerospace Industries Provided by IHS under licen

36、se with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3545-002:20068 5 List of product standards EN 3545-003, Aerospace series Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures

37、 55 C to 175 C Part 003: Connectors with female contacts Product standard. EN 3545-004, Aerospace series Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures 55 C to 175 C Part 004: Connectors with male contacts Product standar

38、d. EN 3545-005, Aerospace series Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures 55 C to 175 C Part 005: Female coding and attachment system for mounting on free housing (plug) Product standard. EN 3545-006, Aerospace seri

39、es Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures 55 C to 175 C Part 006: Male coding and attachment system for mounting on free housing (receptacle) Product standard. EN 3545-007, Aerospace series Connectors, electrical,

40、 rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures 55 C to 175 C Part 007: Cable clamp Product standard. EN 3545-008, Aerospace series Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating

41、temperatures 55 C to 175 C Part 008: Tools for assembly/removal of coding and attachment systems Product standard. 6 Polarization Coding “Codable“ polarization is provided by the attachment systems (male or female), each of which provides six orientation possibilities in the hexagonal housings at th

42、e rear of the connectors. Each housing flat is marked 1 to 6. Tool for torquing coding and attachment systems is defined in EN 3545-008. A positioning index is provided at the (hexagonal) rear of the attachment systems: a dot for male keys; a dash for female keys. During coding, this index is positi

43、oned in front of the selected mark: first on side A; then on side B. In the following example (Figure 2), polarization coding is set to 1 3 Key orientation on side B Key orientation on side A Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for Resa

44、leNo reproduction or networking permitted without license from IHS-,-,-prEN 3545-002:2006 9 Key 1 Attachment system 2 Positioning index 3 Rear view of male housing 4 “Codable“ polarization 5 Fixed polarization 6 Rear view of female housing Figure 2 7 Contact arrangements 7.1 General Contact arrangem

45、ents in the insulators are defined on the figures showing the front side (coupling) of the female housings (male contacts). Contact cavity marking consists of: identification of the end cavities of each row; indication of the 10th cavity and its multiples using the following symbols (except arrangem

46、ents 04, 05, 06, 07 and 09); oblique line linking the cavities in size 22 contacts; opposite chevrons for cavities in size 20 contacts. Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without licens

47、e from IHS-,-,-prEN 3545-002:200610 7.2 Arrangement 01 50 contacts, size 20 See Figure 3. Figure 3 7.3 Arrangement 02 78 contacts, size 22 according to EN 3155-003 and EN 3155-008. See Figure 4. Figure 4 7.4 Arrangement 03 39 contacts, size 22 according to EN 3155-003 and EN 3155-008. 10 contacts, s

48、ize 16 See Figure 5. Figure 5 7.5 Arrangement 04 21 contacts, size 16 See Figure 6. Figure 6 Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3545-002:200611 7.6 Arrangement 05 13 contacts, size 12 See Figure 7. Fi