BS 2G 180-1974 Specification for permanent splicing of aircraft electrical cables《飞行器用电缆固定编接规范》.pdf
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1、BRITISH STANDARD AEROSPACE SERIES BS2G180: 1974 Superseding British Standard G180 Specification for Permanent splicing of aircraft electrical cables UDC 629.7.064.5:621.315.687.1BS2G180:1974 This British Standard, having been approved by the AerospaceIndustry Standards Committee, was published under
2、the authority of the Executive Board on 29November1974 BSI10-1999 The following BSI references relate to the work on this standard: Committee reference ACE/6/1 Draft for comment72/36973 ISBN 0 580 08620 8 Foreword This British Standard has been prepared to define approved methods of making and insta
3、lling joints in copper conductors of aircraft electrical cables and wires by the use of crimped splices. It also covers the repair of such cables and wires using the same techniques, and details certain design requirements to supplement those given in British Standard G178. Appendix A provides infor
4、mation about the types of device currently manufactured, to assist the definition of the subject. This standard makes reference to the following British Standards: 3G100, General requirements for equipment for use in aircraft Part1:Identification, declaration and construction Part2: All equipment. G
5、178, Crimped joints for aircraft electrical cables and wires. A British Standard does not purport to include all the necessary provisions of a contract. Users of British Standards are responsible for their correct application. Compliance with a British Standard does not of itself confer immunity fro
6、m legal obligations. Summary of pages This document comprises a front cover, an inside front cover, pagesi andii, pages1 to4 and a back cover. This standard has been updated (see copyright date) and may have had amendments incorporated. This will be indicated in the amendment table on the inside fro
7、nt cover. Amendments issued since publication Amd. No. Date CommentsBS2G180:1974 BSI 10-1999 i Contents Page Foreword Inside front cover Section 1. General 1 Scope 1 2 Definitions 1 Section 2. Application 3 Selection and use of splices 1 4 Restrictions on splicing 1 Section 3. Installation 5 Stagger
8、ing of splices 2 6 Location of splices 2 7 Support of splices 2 8 Post-insulation of splices 2 9 Tools 2 10 Recording 2 Section 4. Design requirements 11 General 2 12 Protective treatment 2 13 Insulation 3 14 Environmental requirements 3 Appendix A Types of splice currently manufactured 4ii blankBS2
9、G180:1974 BSI 10-1999 1 Section 1. General 1 Scope This British Standard defines the essential parameters for achieving acceptable jointing of the copper conductor of one cable to that of another, or the multiple connection of such conductors by means of permanent crimped splices. This standard does
10、 not cover the splicing of coaxial cables or of aluminium cables. 2 Definitions For the purposes of this British Standard the definitions contained in British Standard G178 and the following apply. 2.1 cable and wire a single core electrical cable or wire or an individual core of a multicore cable o
11、r wire 2.2 in-line splice a connecting device with a barrel or socket at each end to accommodate electrical cable conductors, with or without additional provision to accommodate and support the cable insulation. With this type of splice two separate crimping operations are normally necessary to join
12、 the conductors of the cables 2.3 parallel splice a connecting device with a single conducting barrel in which the electrical cable conductors lie side by side, whether inserted from the same end or from opposite ends of the barrel. With this type of splice only one crimping operation is normally ne
13、cessary to join the conductors of two or more cables 2.4 pre-insulated splice an in-line or parallel splice in which the conducting barrel is insulated by a sleeve which extends beyond the ends of the barrel, which remains firmly fixed to the barrel before, during and after the crimping operations,
14、and through which the crimping operations must be performed 2.5 post-insulated splice an in-line or parallel splice insulated after the crimping operation by the addition of a sleeve, which extends beyond the ends of the barrel 2.6 declaration of design and performance (DDP) the standard form specif
15、ied in British Standard3G100-1 2.7 Air Form100D a standard form relating to instrument and electrical equipment intended for United Kingdom Ministry of Defence aircraft, whereby the manufacturer or design authority certifies compliance with the specification for that equipment or, if necessary, stat
16、es any limitations in performance Section 2. Application 3 Selection and use of splices The selection and use of splices for given cable sizes, type and installation shall be made in accordance with the data supplied by the relevant design authority 1) . It is recognized that splices are occasionall
17、y used to effect an urgent repair of damaged wiring when specific instruction from an approved design authority is not available. In such cases, particular regard shall be given to the requirements of clause4, in addition to the general requirements of this standard. Any such splicing of cables shal
18、l be recorded in the aircraft technical log (or equivalent) as a “temporary repair”. The information recorded shall include that listed in clause10 and at the first opportunity the splice(s) shall be replaced or duly authorized by an approved procedure. It should be noted that the crimping of multip
19、le conductors in a splice with simultaneously crimped insulation support does not provide the normal insulation support. The installer should recognize this limitation and care should be taken to prevent compression of the insulation of multiple cables. 4 Restrictions on splicing 4.1 Joints shall no
20、t be made for repair purposes in the following cables unless specifically approved by a design authority: a) h.t. cables (greater than600V (r.m.s.) to earth); b) multicore cables; c) cables within a fire zone; d) thermocouple cables; 1) For aircraft subject to British civil or military airworthiness
21、 requirements, a design authority is an organization approved by the Airworthiness Division of the Civil Aviation Authority, or by the Ministry of Defence (Procurement Executive) (A.D.Elec.), as appropriate.BS2G180:1974 2 BSI 10-1999 e) cables in vital circuits declared by the aircraft constructor a
22、nd listed in the aircraft manual; f) cables larger than size10; g) cable or loom installations specifically designed to permit movement between aircraft stations in a predetermined manner. 4.2 Unless specifically approved by a design authority parallel splices shall not be used for repair purposes e
23、xcept as a direct replacement for an existing item. Section 3. Installation 5 Staggering of splices Where there is a loom or bundle of cables or cable core to be spliced, the splices shall be staggered to avoid an excessive increase in bulk of the loom and with due regard to possible tracking betwee
24、n splices, or from splice to earth. 6 Location of splices 6.1 Splices shall not be located under clips or ties. 6.2 The minimum distance between splices in any one cable shall be500mm and not more than two splices shall be used in3m of cable. 6.3 Splices shall be so positioned that they can be visua
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