BS 3G 101-1987 Specification for general requirements for mechanical and electromechanical aircraft indicators《航空用机械和机电式指示仪的一般要求规范》.pdf
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1、BRITISH STANDARD AEROSPACE SERIES BS3G101: 1987 (Superseding BS2G101) Specification for General requirements for mechanical and electromechanical aircraft indicators UDC 629.7.054874BS3G101:1987 This BritishStandard, having been prepared under the directionof the Aerospace Standards Committee, was p
2、ublished under the authorityofthe Board of BSI andcomes into effect on 27February1987 BSI04-2000 The following BSI references relate to the work on this standard: Committee reference ACE/30 Draft for comment84/78651 DC ISBN 0 580 14955 2 Committees responsible The preparation of this BritishStandard
3、 was entrusted by the Aerospace Standards Committee (ACE/-) to Technical Committee ACE/30, upon which the following bodies were represented: Civil Aviation Authority (Airworthiness Division) GAMBICA (BEAMA Ltd.) Ministry of Defence Society of British Aerospace Companies Limited Amendments issued sin
4、ce publication Amd. No. Date of issue CommentsBS3G101:1987 BSI 04-2000 i Contents Page Committees responsible Inside front cover Foreword ii 1 Scope 1 2 Cases 1 3 Connections 1 4 Mounting attitude 2 5 Indicator movements 2 6 Presentation 2 7 Cover glasses and windows 4 8 Integral lighting 4 9 Lumine
5、scent and fluorescent markings 4 10 Self-test 5 Figure 1 Dimensions for flangeless round indicator cases 6 Figure 2 Dimensions for flangeless round indicator cases, panel cutouts 7 Figure 3 Standard dimensions for flangeless square and rectangular cases 8 Figure 4 Flangeless square indicator cases,2
6、in(50.8mm) 10 Figure 5 Flangeless square and rectangular cases, cutouts 11 Figure 6 Standard mooring plates, flangeless, square and rectangular cases 13 Figure 7 Standard adaptor plates, flangeless, square and rectangular cases 15 Figure 8 Mounting arrangement for flangeless squareandrectangularindi
7、cator cases 17 Figure 9 Recesses for pitot pressure connections 18 Figure 10 Recesses for static pressure connections 19 Table 1 Types of indicator case 1 Publications referred to Inside back coverBS3G101:1987 ii BSI 04-2000 Foreword This revision of BS2G101:1975 has been prepared under the directio
8、n of the Aerospace Standards Committee to align the general requirements for aircraft indicators with ISO268:1980 published by the International Organization for Standardization (ISO). The general requirements stipulated are for use in conjunction with G series BritishStandards for specific aircraft
9、 indicator types. As in the case of previous editions, the requirements of this standard will not be applied retrospectively. Imperial units are used in this standard to maintain compatibility with existing aircraft practice; metric dimensions are given in parentheses. A British Standard does not pu
10、rport 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 from legal obligations. Summary of pages This document comprises a front cover, an inside front
11、 cover, pagesi andii, pages1 to20, an inside back cover 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 front cover.BS3G101:1987 BSI 04-2000 1 1 Scope This BritishStandard spec
12、ifies requirements which are generally applicable to mechanical and electromechanical indicators for use in aircraft. It is to be read in conjunction with specifications for individual indicators and the relevant requirements of BS3G100. For the purpose of this standard, an indicator is regarded as
13、a unit primarily concerned with the visual display of information. NOTE 1The titles of the publications referred to in this standard are listed on the inside back cover. NOTE 2The latest revision of an aerospace standard is indicated by a prefix number. 2 Cases 2.1 The finished indicator cases shall
14、 be of the types given in Table 1, unless specified otherwise in the contract or order. Table 1 Types of indicator case 2.2 The mounting details for the front area of the indicator case and mounting shall comply with Figure 1 to Figure 5 as appropriate (seeTable 1). NOTE 1To allow physical interchan
15、geability of panel indicators, a range of preferred mounting dimensions has been established. NOTE 2The individual specification for the indicator, referred to in this Part of BS3G101 as “the individual specification”, states all the dimensions for the case. NOTE 3Information on panel cutouts is giv
16、en for each type. NOTE 4The two methods of mounting most commonly used are as follows. a) Clamp mounting, with the indicator secured in the operating position by a clamp mounted on the rear face of the indicator panel. For this arrangement access to the rear of the panel is not required when the ind
17、icator is fixed, as the clamp arrangement is operated from the front of the panel. The clamp method of mounting is also used by circular and square indicators. It is particularly important with this type of indicator to ensure that the surface around which the clamp fits is of uniform dimension and
18、of adequate strength to retain rigidity of mounting. b) Clamp mounting, with mooring plate and/or optional adaptor plate as shown in Figure 6, Figure 7 and Figure 8. 2.3 Any limitation in the use of a mounting for which the indicator has been declared shall be stated by the manufacturer. During vibr
19、ation and acceleration testing the declared mounting shall be used. 2.4 An indicator case with electrical connections shall be earthed through a connector terminal pin or bonding point. Unless otherwise required by the individual specification, no internal electrical circuit shall be returned via th
20、is case/earth bonding connection. The current-carrying capacity of the case earthing wire shall be greater than the current-carrying capacity of the associated airframe wiring. 2.5 The design and construction of the indicator case shall be such that the indicators specified performance is unaffected
21、 when the indicator, installed in accordance with the relevant declarations, is subjected to the test for drip-proof equipment in accordance with BS3G100-2, and to tests for resistance to other fluids, as required by the individual specification. 2.6 The legibility of the indicator shall not be affe
22、cted by any misting inside the glass under the conditions of use for which it is declared. 2.7 An indicator required by the individual specification to have an airtight or pressure-resisting case shall be capable of withstanding, without damage or leakage greater than that permitted by the individua
23、l specification, external pressures from100kPa (1000mbar) above that of the interior to20kPa (200mbar) below that of the interior, and there shall be no interference between the moving elements and the cover glass during and after the application of pressure. NOTEIndicators should not present a haza
24、rd due to implosion or explosion. 2.8 Where an indicator is vented to the surrounding atmosphere, the vent shall not affect the performance of the indicator. It shall be screened to prevent the ingress of sand and dust. The vent shall be protected against inadvertent closure and located at approxima
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