BS 2G 132-1981 Specification for general requirements for electromagnetically operated contactors for aircraft《飞行器用电磁操纵的接触器的一般要求规范》.pdf
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1、BRITISH STANDARD AEROSPACE SERIES BS2G132: 1981 Specification for General requirements for electromagnetically operated contactors for aircraft UDC629.7.064.5:621.316.53BS2G132:1981 This British Standard, having been prepared under the directionof the Aerospace Standards Committee, was published und
2、er the authority ofthe Board of BSI and comes intoeffect on 31December1981 BSI11-1999 The following BSI references relate to the work on this standard: Committee reference ACE/43 Draft for comment80/74178 DC ISBN 0 580 12409 6 Foreword This British Standard has been prepared at the request of the Ae
3、rospace Standards Committee and Society of British Aerospace Companies to cover electromagnetically operated a.c. and d.c. contactors for use in aircraft. It supersedes British Standard G132:1951 which is therefore withdrawn. A British Standard does not purport to include all the necessary provision
4、s of a contract. Users of British Standards are responsible for their correct application. Compliance 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 and ii, pages1 to18 and a bac
5、k 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 front cover. Amendments issued since publication Amd. No. Date of issue CommentsBS2G132:1981 BSI 11-1999 i Contents Page Foreword Inside
6、front cover 1 Scope 1 2 References 1 3 Definitions 1 4 General requirements 2 5 Particular requirements 3 6 Tests 4 7 Type approval tests 5 8 Production acceptance tests 10 9 Quality assurance test 11 10 Serviceability tests 12 Appendix A Driving sand test 15 Appendix B Impact shock test 15 Appendix
7、 C Fluid contamination tests 15 Figure 1 Symbols and identification of terminals: single-pole contactors 17 Figure 2 Symbols and identification of terminals: three pole contactors 17 Figure 3 Typical test circuit for short-circuit test 18 Table 1 Environmental tests: proof conditions 5 Table 2 Stren
8、gth of terminations 6 Table 3 Contact voltage drop 6 Table 4 Altitude, temperature and cycles of operation 7 Table 5 Type tests schedule 13 Table 6 Quality assurance test schedule 14 Table 7 Sand composition 15 Table 8 Pulse acceleration and duration (shock) 15 Table 9 Test fluids 16ii blankBS2G132:
9、1981 BSI 11-1999 1 1 Scope This British Standard specifies the requirements for single and three-pole electromagnetically operated contactors, in the range25A to600A for use in nominal28V d.c. and115/200V three-phase400Hz a.c. systems in aircraft. Two environmental classes and two enclosure categori
10、es are specified as follows. Environmental classes Class1. Contactors suitable for high altitude and wide temperature conditions. Class2. Contactors suitable for lower altitudes and narrower temperature conditions. Enclosure categories Category A. Hermetically sealed contactors. Category B. Non-herm
11、etically sealed contactors. 2 References This standard makes reference to the following standards publications. BS410, Specification for test sieves. BS2011, Basic environmental testing procedures Part2.1Ea: Test Ea. Shock. BS6001, Sampling procedures and tables for inspection by attributes. 2G100,
12、General requirements for electrical equipment and indicating instruments for aircraft Part2: Environmental and operating conditions, paragraph213, Leakage tests for hermetically sealed equipment. 3G100, General requirements for equipment for use in aircraft Part0: Introduction Part1:Identification a
13、nd declarations Part2: All equipment Section1 Construction Section3 Environmental conditions Subsection3.1 Vibration Subsection3.2 Temperature-pressure requirements Subsection3.3 Mould growth Subsection3.5 Explosion-proofness Subsection3.6 Acceleration requirements Subsection3.8 Salt mist Subsection
14、3.12 Fluid contamination Part3: Characteristics of aircraft electrical power supplies Part4: Electrical equipment Section1 Construction and general Subsection1.1 Electrical insulation tests. G 176, Cartridge fuses for aircraft. 3G178, Crimped joints for aircraft electrical cables and wires. G216, Ha
15、nd operated, thermally compensated, miniature single- and triple-pole circuit breakers. 3 Definitions For the purposes of this British Standard the following definitions apply. 3.1 normally open contacts contacts which do not allow the passage of current when the contactor control coil(s) are de-ene
16、rgized and the contactor is not latched ON. These contacts will close to allow the passage of current when the control coil only is energized 3.2 normally closed contacts contacts which allow the passage of current when the contactor control coil(s) are de-energized and the contactor is not latched
17、ON. These contacts will open to prevent the passage of current when the control coil only is energized 3.3 control coil a coil which has to be energized to cause the normally open contacts to change from the open to closed position and/or the normally closed contacts to change from the closed to ope
18、n position 3.4 release coil a coil which, in a latched contactor has to be energized to cause the normally open contacts to change from the closed to the open position and/or the normally closed contacts to change from the open to the closed position 3.5 pull in voltage the minimum voltage, rising,
19、which has to be applied to the control coil to ensure complete closure of the normally open main and auxiliary contacts, in one movement 3.6 drop out voltage a) for magnetically held contactors. The maximum voltage, falling, at which complete closing of the normally closed main and auxiliary contact
20、s occurs in one movement, in the case of a change-over contactor, or complete opening of all main and auxiliary normally-open contacts occurs in one movement, in the case of a one-way contactor. b) for latched contactors. The minimum voltage rising, at which the latch is fully operated, allowing the
21、 contacts to revert to the de-energized position.BS2G132:1981 2 BSI 11-1999 3.7 response time at closure the period of time between application of voltage to the control coil, and the closing of the last of the normally open contacts 3.8 response time on opening the period of time between removal of
22、 voltage to the control coil, or application of voltage to the release coil, and the closing of the last of the normally closed contacts in the case of a changeover contactor, or opening of the last of the normally open contacts in the case of a one way contactor 3.9 current rating the maximum curre
23、nt at each specified load condition which the contact can make, carry continuously and break, at the maximum permitted voltage for the specified number of operations 4 General requirements 4.1 Description and design requirements 4.1.1 The contactors shall comply with the requirements of this British
24、 Standard. 4.1.2 Both categories of contactors, (A) hermetically sealed or (B) non-hermetically sealed, shall be suitable for one of the following temperature and altitude classifications. Class1. Contactors for use at altitudes up to21300m and for temperatures within the range54 C to+85 C shall not
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