BS G 253-1995 Specification for type 1 terminal junction systems《一型终端连接系统规范》.pdf
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1、BRITISH STANDARD AEROSPACE SERIES BS G253:1995 ISO8668-3: 1994 Specification for Type1 terminal junction systemsBSG 253:1995 This BritishStandard, having been prepared under the directionof the Engineering SectorBoard, was published underthe authority of the Standards Board and comes intoeffect on 1
2、5May1995 BSI01-2000 The following BSI references relate to the work on this standard: Committee referenceACE/6 Draft for comment92/83129DC ISBN 0 580 24045 2 Committees responsible for this British Standard The preparation of this BritishStandard was entrusted to Technical Committee ACE/6, Aerospace
3、 anionic electrical and fibre-optic technology, upon which the following bodies were represented: British Airways British Cable Makers Confederation British Rubber Manufacturers Association Civil Aviation Authority (Airworthiness Division) Federation of the Electronics Industry Ministry of Defence S
4、ociety of British Aerospace Companies Ltd. Amendments issued since publication Amd. No. Date CommentsBSG 253:1995 BSI 01-2000 i Contents Page Committees responsible Inside front cover National foreword ii 1 Scope 1 2 Normative references 1 3 Definitions 1 4 Designation 1 5 Characteristics 3 6 Toolin
5、g 16 7 Production testing and quality control 16 Figure 1 Feedback module 3 Figure 2 Feedthrough module 4 Figure 3 Frame for feedback module: Standard frame P1 5 Figure 4 Frame for feedback module: Perforated frame P2 5 Figure 5 Frame for feedback module: Reinforced frame P3 6 Figure 6 Frame for fee
6、dthrough module: P4 6 Figure 7 Module clamps for feedback modules (code1) 7 Figure 8 Module clamps and inserts for feedthrough modules (code2) 7 Figure 9 Contact, size22 8 Figure 10 Contact, size20 9 Figure 11 Detail of the crimping shank of the size16 contact 9 Figure 12 Detail of the crimping shan
7、k of the size12 contact 9 Figure 13 Sealing plug 10 Figure 14 Assembly diagram 11 Figure 15 Size A modules 11 Figure 16 Size B modules 12 Figure 17 Size C modules 14 Figure 18 Hybrid interconnection diagram for size C modules 15 Figure 19 Size D modules 15 Table 1 Code for resistance to fluids 1 Tab
8、le 2 Coding of the protection of frames 2 Table 3 Feedback modules 3 Table 4 Feedthrough modules 4 Table 5 Frames for feedback modules (types P1 and P2) 5 Table 6 Frames for feedback modules (type P3) 6 Table 7 Frames for feedthrough modules (type P4) 6 Table 8 Contacts 10 Table 9 Sealing plugs 11 T
9、able 10 Size A modules 12 Table 11 Size B modules 13 Table 12 Size C modules 14 Table 13 Size D modules 15 Table 14 Connection wires 16 List of references Inside back coverBSG 253:1995 ii BSI 01-2000 National foreword This BritishStandard has been prepared by Technical CommitteeACE/6. It is identica
10、l with ISO8668-3:1994, Aircraft Terminal junction systems Part3: Detail specification for type1 system, published by the International Organization for Standardization (ISO). Cross-references The Technical Committee has reviewed the provisions of ISO8668-1:1986, ISO8668-2:1986 and Mil-I-81969:1982,
11、to which normative reference is made in the text, and has decided that they are acceptable for use in conjunction with this standard. 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. C
12、ompliance with a British Standard does not of itself confer immunity from legal obligations. Summary of pages This document comprises a front cover, an inside front cover, pagesi andii, pages1 to18, an inside back cover and a back cover. This standard has been updated (see copyright date) and may ha
13、ve had amendments incorporated. This will be indicated in the amendment table on the inside front cover.BSG 253:1995 BSI 01-2000 1 1 Scope 1.1 This part of ISO8668 specifies the particular characteristics of a terminal junction system (TJS), designated as type1 and intended for use at temperatures b
14、etween 55 C and+155 C. 1.2 The junction systems covered by this part of ISO8668 comprise: a) feedback modules in four sizes; b) feedthrough modules in four sizes; c) frames adapted to these modules: standard frameP1, perforated frameP2 or frameP3 for feedback modules; solid frameP4 for feedthrough m
15、odules; d) module clamps and inserts; e) removable identification tags; f) removable male crimp contacts of sizes22,20,16 and12; g) sealing plugs. 2 Normative references The following standards contain provisions which, through reference in this text, constitute provisions of this part of ISO8668. A
16、t the time of publication, the editions indicated were valid. All standards are subject to revision, and parties to agreements based on this part of ISO8668 are encouraged to investigate the possibility of applying the most recent editions of the standards indicated below. Members of IEC and ISO mai
17、ntain registers of currently valid International Standards. ISO 8668-1:1986, Aircraft Terminal junction systems Part1: Characteristics. ISO 8668-2:1986, Aircraft Terminal junction systems Part2: Tests. MIL-I-81969:1982, Connector and electrical contact General specification for installing and remova
18、l tools. 3 Definitions For the purposes of this part of ISO8668, the definitions given in ISO8668-1 apply. See also IEC50(581):1978, International Electrotechnical Vocabulary Chapter581: Electromechanical components for electronic equipment. 4 Designation 4.1 Modules The modules shall be designated
19、as follows: a) reference to this part of ISO8668; b) separated by a space, a figure indicating the type of module: 1=feedback module, 2=feedthrough module; c) a letter indicating the size of module: A, B, C or D (see Figure 1 and Figure 2); d) three figures indicating the interconnection diagram (se
20、e5.2); e) a letter defining resistance to fluids (see Table 1). Table 1 Code for resistance to fluids EXAMPLE The designation of a size A feedback module with21 contacts of size22, arranged according to interconnection diagram101 and resistant to fluids defined by code A is as follows: Feedback modu
21、le ISO8668-31 A101 A Fluids Code Synthetic oil for turbine aero engines Mineral oil for turbine aero engines Kerosene for turbine aero engines ABSG 253:1995 2 BSI 01-2000 4.2 Frames The frames shall be designated as follows: a) reference to this part of ISO8668; b) separated by a space, a figure ind
22、icating the type of module for which the frame is designated: 1=feedback modules, 2=feedthrough modules; c) a letter indicating the type of frame: P1=standard solid frame for feedback modules; P2=perforated frame for feedback modules; P3=reinforced frame for feedback modules; P4=full frame for feedt
23、hrough modules. d) three-figure code indicating the length of the frame, in millimetres; e) separated by a hyphen, a figure indicating the nature of the protection of the frame (see Table 2). Table 2 Coding of the protection of frames EXAMPLE The designation of a perforated frame for100mm long feedb
24、ack modules, protected by black anodic oxidation, is as follows: Perforated frame ISO8668-31 P21003 4.3 Module clamps and inserts Module clamps and inserts shall be designated as follows: a) reference to this part of ISO8668; b) separated by a space, two letters and one figure indicating the type of
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