EN 3682-001-2006 en Aerospace series - Connectors plug and receptacle electrical rectangular interchangeable insert type rack to panel operating temperature 150 Degrees C continuou.pdf
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1、BSI Standards PublicationBS EN 3682-001:2013Aerospace series Connectors, plug andreceptacle, electrical,rectangular, interchangeableinsert type, rack to panel,operating temperature 150 CcontinuousPart 001: Technical specificationBS EN 3682-001:2013 BRITISH STANDARDNational forewordThis British Stand
2、ard is the UK implementation of EN 3682-001:2013.It supersedes BS EN 3682-001:2006 which is withdrawn.The UK participation in its preparation was entrusted to TechnicalCommittee ACE/6, Aerospace avionic electrical and fibre optictechnology.A list of organizations represented on this committee can be
3、obtained on request to its secretary.This publication does not purport to include all the necessaryprovisions of a contract. Users are responsible for its correctapplication. The British Standards Institution 2013. Published by BSI StandardsLimited 2013ISBN 978 0 580 81717 5ICS 49.060Compliance with
4、 a British Standard cannot confer immunity fromlegal obligations.This British Standard was published under the authority of theStandards Policy and Strategy Committee on 30 September 2013.Amendments issued since publicationDate Text affectedBS EN 3682-001:2013EUROPEAN STANDARD NORME EUROPENNE EUROPI
5、SCHE NORM EN 3682-001 September 2013 ICS 49.060 Supersedes EN 3682-001:2006English Version Aerospace series - Connectors, plug and receptacle, electrical, rectangular, interchangeable insert type, rack to panel, operating temperature 150 C continuous - Part 001: Technical specification Srie arospati
6、ale - Connecteurs lectriques rectangulaires rackables, fiches et embases, inserts interchangeables, temprature dutilisation 150 C continu - Partie 001: Spcification technique Luft- und Raumfahrt - Elektrischer Rechtecksteckverbinder, freie und feste Bauform, auswechselbare Isolierkrper, Gestell-Eins
7、chubsteckverbinder, Betriebstemperatur 150 C konstant - Teil 001: Technische Lieferbedingungen This European Standard was approved by CEN on 8 May 2013. CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this European Standard the stat
8、us of a national standard without any alteration. Up-to-date lists and bibliographical references concerning such national standards may be obtained on application to the CEN-CENELEC Management Centre or to any CEN member. This European Standard exists in three official versions (English, French, Ge
9、rman). A version in any other language made by translation under the responsibility of a CEN member into its own language and notified to the CEN-CENELEC Management Centre has the same status as the official versions. CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Croat
10、ia, Cyprus, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and Un
11、ited Kingdom. EUROPEAN COMMITTEE FOR STANDARDIZATION COMIT EUROPEN DE NORMALISATION EUROPISCHES KOMITEE FR NORMUNG Management Centre: Avenue Marnix 17, B-1000 Brussels 2013 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 3682-001:2
12、013: EBS EN 3682-001:2013EN 3682-001:2013 (E) 2 Contents Page Foreword . 3 Introduction 4 1 Scope . 4 2 Normative references . 4 3 Terms and definitions . 5 4 Description 5 5 Design 6 6 Definition drawings and masses . 7 7 Tests . 47 8 Quality assurance . 65 9 Designation and marking . 69 10 Deliver
13、y conditions . 70 11 Packaging 70 12 Storage . 70 BS EN 3682-001:2013EN 3682-001:2013 (E) 3 Foreword This document (EN 3682-001:2013) has been prepared by the Aerospace and Defence Industries Association of Europe - Standardization (ASD-STAN). After enquiries and votes carried out in accordance with
14、 the rules of this Association, this Standard has received the approval of the National Associations and the Official Services of the member countries of ASD, prior to its presentation to CEN. This European Standard shall be given the status of a national standard, either by publication of an identi
15、cal text or by endorsement, at the latest by March 2014, and conflicting national standards shall be withdrawn at the latest by March 2014. Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. CEN and/or CENELEC shall not be held respo
16、nsible for identifying any or all such patent rights. This document supersedes EN 3682-001:2006. According to the CEN-CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Croatia, Cypr
17、us, Czech Republic, Denmark, Estonia, Finland, Former Yugoslav Republic of Macedonia, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the United
18、 Kingdom. BS EN 3682-001:2013EN 3682-001:2013 (E) 4 Introduction This family of connectors is derived from MIL-C-83527 with which it is intermateable and interchangeable. It offers a comprehensive range of contact arrangements. The plug is fitted with a grounding spring system which is replaceable i
19、n the field. It is particularly for use on rack application in zones of severe environmental conditions on board aircraft, applying EN 2282. 1 Scope This European Standard specifies the general characteristics, the conditions for qualification, acceptance and quality assurance, as well as the test p
20、rograms and groups for connectors intended for use in a temperature range from 65 C to 150 C continuous. 2 Normative references The following documents, in whole or in part, are normatively referenced in this document and are indispensable for its application. For dated references, only the edition
21、cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 2282, Aerospace series Characteristics of aircraft electrical supplies EN 2267-002, Aerospace series Cables, electrical, for general purpose Operating temperatures between 55 C
22、 and 260 C Part 002: General EN 2591 (all parts), Aerospace series Elements of electrical and optical connection Test methods EN 3155 (all parts), Aerospace series Electrical contacts used in elements of connection EN 3197, Aerospace series - Design and installation of aircraft electrical and optica
23、l interconnection systems EN 3682 (all parts), Aerospace series Connectors, plug and receptacle, electrical, rectangular, interchangeable insert type, rack to panel, operating temperature 150 C continuous EN 3909, Aerospace series Test fluids and test methods for electric components and sub-assembli
24、es 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 parts MIL-C-83527 (all parts), Connectors, plug and receptacle, electr
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