BS G 133-1951 Specification for electro-magnetic indicators for extra low voltage aircraft systems《航空用超低电压系统电磁指示器规范》.pdf
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1、BRITISH STANDARD BS G133:1951 Incorporating Amendment No.1 Specification for Electro-magnetic indicators for extra low voltage aircraft systems UDC629.13.056BSG133:1951 This BritishStandard, having been approved by the Aircraft Industry Standards Committee and endorsed by the Chairman ofthe Engineer
2、ing Divisional Council, was published under theauthority of the General Council on 6 September1951 BSI02-2000 ISBN 0 580 34525 4 Foreword Warning lights as indicators of the condition of electrical circuits tend to confuse the pilot, particularly when they remain illuminated: this BritishStandard pr
3、ovides an alternative in the form of a magnetic indicator which can give a continued indication of the maintenance of a certain condition in a circuit without irritation to the pilot. A British Standard does not purport to include all the necessary provisions of a contract. Users of British Standard
4、s 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 andii, pages1 to3 and a back cover. This standard has been updated (see
5、 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 Comments 1273 September 1951 Indicated by a sideline in the marginBSG133:1951 BSI 02-2000 i Contents Page For
6、eword Inside front cover Section 1. General requirements 1 Scope 1 2 ConstructionGeneral 1 Section 2. Design requirements 3 Operation 1 4 Presentation 1 5 Operating voltage 1 6 Temperature rise 1 7 Vibration, acceleration and climatic proofing 1 8 Magnetic interference 2 9 Marking 2 Section 3. Tests
7、 10 General 2 A. Type test 11 Vibration test 2 12 Acceleration test 2 13 Climatic proofing 2 14 Functioning tests 2 15 Compass safe distance 2 16 Endurance test 2 17 Temperature rise test 2 18 High voltage and insulation resistance tests 3 B. Type test 19 Functioning test 3 20 High voltage and insul
8、ation resistance tests 3 Figure 1 Holes in panel 1ii blankBSG133:1951 BSI 02-2000 1 Section 1. General requirements 1 Scope This BritishStandard applies to a single-pole or multi-pole indicator comprising a flag or shutter, operated electro-magnetically at a nominal voltage of24volts D.C., giving a
9、visible signal appropriate to the state of the electrical circuit or circuits to which it is connected. 2 ConstructionGeneral The indicator shall satisfy the general airworthiness requirements specified in Part1 1)of BS G100 2)“General requirements for electrical equipment and indicating instruments
10、 for aircraft.” It shall be so designed that it may be mounted in any attitude without affecting its operational efficiency. The preferred fixing arrangement is that which would render the indicator interchangeable with the existing British aircraft warning light, the fixing holes of which are as sh
11、own in Figure 1. Section 2. Design requirements 3 Operation The indicating flag or shutter shall be operable to one or more positions, apart from the null position. The means of operation shall be such that any one signal is rapidly presented and it shall be impossible for the flag or shutter to rem
12、ain in any position beyond or between these signals. 4 Presentation Signals shall be clearly distinguishable by suitable colouring, marking, fluorescing, or luminizing of the flag or shutter. Fluorescent brightness shall conform to the requirements of BS G100. A plain matt black surface shall be pre
13、sented when the supply is discontinued and, if possible, when there is any failure of the indicator. The window of the indicator shall have a clear area of not less than0.07sq. in. and its smallest dimension shall be not less than 3 / 16 in. The dimensions and shape of the shutter or shutter segment
14、 and/or indicator window shall be such that it is possible to distinguish the indicator signals clearly at any point within a cone subtending an angle of not less than120 at the window, with the axis of the cone normal to the plane of the window. No portion of an unwanted signal shall be visible whe
15、n the indicator is viewed from within that cone. 5 Operating voltage The indicating mechanism shall be designed to function normally within an applied D.C. voltage range of20 to28.5volts. The mechanism shall give a positive and rapid change of signal at all voltages in this range, and shall return t
16、o the null position if the voltage drops to a value of less than3volts. The requirements of this clause shall be fulfilled irrespective of the polarity of the connections to the supply. 6 Temperature rise When the indicator is continuously energized at28.5volts D.C. the temperature rise of the windi
17、ngs shall be within the limits specified in BSG100. 7 Vibration, acceleration and climatic proofing The design and construction of the indicator shall be such as to satisfy the requirements of BS G100 in respect of: a) vibration, including resonanceGrade III. b) accelerationGrade II. c) climatic pro
18、ofingGrade II. 1) This indicator is not an indicating instrument within the meaning of Part2 of BS G100. 2) In course of preparation. Figure 1 Holes in panelBSG133:1951 2 BSI 02-2000 8 Magnetic interference The indicator shall be designed to be suitable for mounting near a compass and it shall be co
19、nstructed to satisfy the requirements of BS G100 in respect of magnetic interference. 9 Marking Each indicator shall be clearly and indelibly marked with the following information: a) the number of this BritishStandard, i.e.BSG133. b) manufacturers name or identification. c) type number. d) operatin
20、g voltage. Section 3. Tests 10 General Tests shall be made to prove compliance with all requirements of this BritishStandard. It is not intended or recommended that complete tests shall be made on every indicator supplied. Two kinds of tests, therefore, are specified as follows: A. Type tests (Claus
21、es1118) which shall be made on each particular class of indicator. B. Routine (individual) tests (Clauses1920) which shall be made on every indicator manufactured to this BritishStandard. The tests prescribed in Clauses1114 inclusive and Clause18 shall be performed in that order on the same indicato
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