AECMA PREN 3545-001-2006 Aerospace series Connectors electrical rectangular with sealed and non-sealed rear plastic housing locking device operating temperatures - 55 to 175 P.pdf
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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
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- AECMAPREN35450012006AEROSPACESERIESCONNECTORSELECTRICALRECTANGULARWITHSEALEDANDNONSEALEDREARPLASTICHOUSINGLOCKINGDEVICEOPERATINGTEMPERATURES55TO175PPDF
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