1、ASD STANDARD NORME ASD ASD NORM prEN 3545-001 Edition P 4 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 3 August
2、2004 Will supersede EN 3545-001:2005 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 001: Technical specification Srie arospatiale Connecteurs lectriques, re
3、ctangulaires, tanches et non tanches larrire, botier en plastique, verrouillage, tempratures dutilisation 55 C 175 C Partie 001 : Spcification technique Luft- und Raumfahrt Elektrische Rechtecksteckverbinder mit und ohne hintere Abdichtung, Plastikgehuse, Verriegelungssystem, Betriebstemperaturen vo
4、n 55 C bis 175 C Teil 001: Technische Lieferbedingungen This “Aerospace Series“ Prestandard has been drawn up under the responsibility of ASD-STAN (The AeroSpace and Defence Industries Association of Europe - Standardization). It is published for the needs of the European Aerospace Industry. It has
5、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 is affected, physically or functionally, without re-identification of the sta
6、ndard. 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 full European Standard (EN). The CEN national members have then to implement t
7、he 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 six months after the date of publication to ASD-STAN Electrical Domain Copyri
8、ght 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 3545-001:20062 Contents Page Foreword2 1 Scope 3 2 Normative references 3 3 Terms and definitio
9、ns .4 4 Description .4 5 Design .5 6 Definition drawing and masses6 7 Contact arrangements.8 8 Tests. 16 9 Quality assurance. 22 10 Designation and marking. 27 11 Delivery conditions. 27 12 Packaging 27 13 Storage. 27 Foreword This standard was reviewed by the Domain Technical Coordinator of ASD-STA
10、Ns 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 Association of Aerospace Industries Provided by IHS under license with AECMA Not f
11、or ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3545-001:20063 1 Scope This standard specifies the technical requirements of rectangular connectors with sealed and non-sealed rear, plastic housing, locking device, for operating temperatures from 55 C to 175 C. 2 No
12、rmative references The following referenced documents are indispensable for the application of this document. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 2266-002, Aerospace series
13、Cables, electrical, for general purpose Operating temperatures between 55 C and 200 C Part 002: General. EN 2591-100 *, Aerospace series Elements of electrical and optical connection Test methods Part 100: General. EN 3155-001, Aerospace series Electrical contacts used in elements of connection Part
14、 001: Technical specification. EN 3155-003, Aerospace series Electrical contacts used in elements of connection Part 003: Contacts, electrical, female, type A, crimp, class S Product standard. EN 3155-008, Aerospace series Electrical contacts used in elements of connection Part 008: Contacts, electr
15、ical, male, type A, crimp, class S Product standard. EN 3155-070, Aerospace series Electrical contacts used in elements of connection Part 070: Contacts, electrical, male, type A, crimp, class S Product standard. 1)EN 3155-071, Aerospace series Electrical contacts used in elements of connection Part
16、 071: Contacts, electrical, female, type A, crimp, class S Product standard. 1)EN 3197, Aerospace series Installation of aircraft electrical and optical interconnection systems. 1)EN 3545-002, Aerospace series Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, loc
17、king device, operating temperatures 55 C to 175 C Part 002: Specification of performance and contact arrangements. EN 3545-008, Aerospace series Connectors, electrical, rectangular, with sealed and non-sealed rear, plastic housing, locking device, operating temperatures 55 C to 175 C Part 008: Tools
18、 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 standards. EN 9133, Aerospace series Quality management systems Qualification procedure for aerospace standard
19、 parts. *And all parts quoted in this standard. 1) Published as ASD 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 from IHS-
20、,-,-prEN 3545-001:20064 AS 1241C, Fire resistant phosphate ester hydraulic fluid for aircraft. 2)AMS 1424, Deicing/anti-icing fluid, aircraft, SAE type I. 2)MIL-PRF-7870C, Lubricating oil, general purpose, low temperature NATO code number O-142. 3)MIL-PRF-23699F, Lubricating oil, aircraft turbine en
21、gine, synthetic base NATO code number O-156. 3)MIL-PRF-87937D, Cleaning compounds aerospace equipment. 3)FED-STD-H28A, Screw-thread standards for federal services. 3)3 Terms and definitions For the purposes of this document, the terms and definitions given in EN 2591-100 apply. 4 Description 4.1 Gen
22、eral A pair of connectors comprises: a male housing fitted with female crimp contacts (code F); a female housing fitted with male crimp contacts and having an interfacial seal which provides sealing at each contact when the connectors are mated (code M). These housings are fitted with polarizing sys
23、tems permitting 36 combinations. They are able to take a cable clamp and comprise a locking device at each end. There are two types of connectors: sealed, grommet provided for sealing of cables at the rear (code E); non-sealed, grommet provided for non abrasion of cables at the rear (code D). 4.2 Ma
24、le and female housings There are one size of housing and twelve contact arrangements as shown in Table 1. See also Figures 2 to 13. 2) Published by: Society of Automotive Engineers, Inc. (SAE), 400 Commonwealth Drive, Warrendale, PA 15096-0001, USA. 3) Published by: Department of Defense (DOD), the
25、Pentagon, Washington, D.C. 20301 USA. 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 3545-001:2006 5 Table 1 Number of contacts Arrangement number Size 22 aSize 22
26、 bSize 20 Size 16 Size 12 Size 10 Size 8 01 0 0 50 0 0 0 0 02 78 0 0 0 0 0 0 03 39 0 0 10 0 0 0 04 0 0 0 21 0 0 0 05 0 0 0 0 13 0 0 06 0 0 0 0 0 7 0 07 0 0 0 0 0 0 5 08 0 0 18 0 0 0 3 09 0 0 25 12 0 0 0 12 78 78 0 0 0 0 0 13 39 39 0 10 0 0 0 16 0 0 0 0 0 7 0 aContacts size 22 according to EN 3155-00
27、3 and EN 3155-008. bContacts size 22 according to EN 3155-003 and EN 3155-008 or EN 3155-070 and EN 3155-071. 4.3 Materials 4.3.1 General The materials which are not specified or are not specially described, shall be as light as possible for the required application. Materials are chosen according t
28、o safety criteria as defined by the authority of certification. When dissimilar metals are in close contact, adequate protection against corrosion shall be provided such that the electromotive force of the galvanic couple shall not exceed 0,25 V. 4.3.2 Housings These are made of rigid material with
29、high dielectric qualities which will not deteriorate under normal conditions of operation and ageing. 4.3.3 Contacts Contacts shall comply with the requirements of EN 3155-001. 5 Design 5.1 Housings In the sealed and non-sealed types, the grommet shall be attached to the housing. Copyright European
30、Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-,-,-prEN 3545-001:20066 Identification of the various positions used for coding by the position indicator which appears on the attachments is gi
31、ven in EN 3545-002. Identification of the contact cavities shall be consistent with Figures 3 to 14 in EN 3545-002. 5.2 Contacts Removable contacts shall be inserted and extracted via the rear of the connector. The insertion and extraction tools shall be introduced via the rear of the connector. For
32、 connectors which are not sealed at the rear, it shall be possible to insert the contact without a tool, unless the mechanical strength of the wires prevents this. 5.3 Attachments, polarizing features They are constituted by two integral elements, which are removable from each housing with the aid o
33、f metal tools defined by EN 3545-008 and provide: rapid attachment of housings to boards; attachment of male housings to female housings; necessary polarization between male and female housings. The threads shall comply with FED-STD-H28A. It shall be impossible to mate housings when these are polari
34、zed differently. 5.4 Cable clamp The cable clamp, made of insulating material, shall be easy to fit and remove, shall be independent of the housing attachment system and shall not require any special fastener. The wires are held by means of a cable tie (binding hand for example). 6 Definition drawin
35、g and masses The general dimensions and the mass of the various elements which make up a pair of connectors are given in product standards. Dimensions and tolerances are in millimetres. Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo r
36、eproduction or networking permitted without license from IHS-,-,-prEN 3545-001:2006 7 Key 1 0,9 min. (see NOTE 1) 2 2,4 max. for contact size 20 2,3 max. for other sizes (see NOTE 2) 3 1 to 1,9 (see NOTE 3) 4 0,03 to 0,58 for arrangements 01 to 06 0,05 to 0,60 for arrangements 07 and 08 5 1,27 min.
37、for quadrax contacts (see NOTE 1) 6 Connector with male contacts 7 Male coding and attachment system 8 Female coding and attachment system 9 Connector with female contacts aApplicable dimensions for contact arrangement 07 and 08 NOTE 1 Electrical engagement of contacts. NOTE 2 Extreme limit position
38、 of electrical point of female contact. NOTE 3 Extreme limit position of male contact, maximum axial clearance: 0,5 Figure 1 Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without license from IHS-
39、,-,-prEN 3545-001:20068 7 Contact arrangements 7.1 General The theoretical positions in the various contact arrangements are defined in Figures 2 to 13, which show the front face (mating) of female housings (male contacts). Identification of the contact cavities consists of: identification of the en
40、d cavities in each row; identification of the 10th cavity and its multiples using the following symbols (except for arrangements 04, 05, 06, 07 and 09); oblique line joining together size 22 contact cavities, opposite chevrons for size 20 contact cavities. 7.2 Arrangement 01 50 contacts, size 20 See
41、 Figure 2. Figure 2 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 3545-001:2006 9 7.3 Arrangement 02 78 contacts, size 22 according to EN 3155-003 and EN 3155-008
42、. See Figure 3. Figure 3 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 3545-001:200610 7.4 Arrangement 03 39 contacts, size 22 according to EN 3155-003 and EN 315
43、5-008. 10 contacts, size 16 See Figure 4. Figure 4 7.5 Arrangement 04 21 contacts, size 16 See Figure 5. Figure 5 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 35
44、45-001:200611 7.6 Arrangement 05 13 contacts, size 12 See Figure 6. Figure 6 7.7 Arrangement 06 7 contacts, size 10 See Figure 7. Figure 7 Copyright European Association of Aerospace Industries Provided by IHS under license with AECMA Not for ResaleNo reproduction or networking permitted without lic
45、ense from IHS-,-,-prEN 3545-001:200612 7.8 Arrangement 07 5 contacts, size 8 (indexed or not) See Figure 8. Figure 8 NOTE Identification of the polarization key of the size 8 contact only on the rear grommet. 7.9 Arrangement 08 18 contacts, size 20 3 contacts, size 8 (indexed or not) See Figure 9. F
46、igure 9 NOTE Identification of the polarization key of the size 8 contact only on the rear grommet. 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 3545-001:2006 13
47、 7.10 Arrangement 09 25 contacts, size 20 12 contacts, size 16 See Figure 10. Figure 10 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 3545-001:200614 7.11 Arrange
48、ment 12 78 contacts, size 22 according to EN 3155-003 and EN 3155-008 or EN 3155-070 and EN 3155-071. See Figure 11. Figure 11 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 3545-001:2006 15 7.12 Arrangement 13 39 con
