BS G 183-1963 Specification for interconnections in analogue data transmission systems in aircraft《航空用模拟数据传输系统互连规范》.pdf
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1、BRITISH STANDARD BS G183:1963 Incorporating Amendment No.1 Specification for Interconnections in analogue data transmission systems in aircraft UDC 621.316.5:621-5:629.13.05BSG183:1963 This BritishStandard, having been approved by the Aircraft Industry Standards Committee and endorsed by the Chairma
2、n ofthe Engineering Divisional Council, was published undertheauthority of theGeneralCouncil of the Institution on 31December1963 BSI03-2000 The following BSI references relate to the work on this standard: Committee reference ACE/30 Draft for comment AC(ACE)703 ISBN 0 580 34538 6 Foreword This Brit
3、ishStandard has been written to provide uniformity of interconnections in control and indicating systems in aircraft using analogue data transmissions. In general, the requirements of the standard are compatible with those of the synchro system manual of Aeronautical Radio Incorporated of America (A
4、RINC), the handbook of the Electronic Engineering Association on a.c. systems for civil aircraft, the Ministry of Aviation publication EL.1790, Notes on manufacture and testing requirements for a.c. synchros, and the Aeronautical Recommended Practice in Synchros (ARP461A) of the Society of Automotiv
5、e Engineers. The standard covers the use of synchros, potentiometers and other analogue transducers in analogue data transmission systems for aircraft. It does not cover such things as energizing volts, transformation ratios, accuracy, voltsperdegree, etc, all of which data should be obtained from t
6、he relevant specification for the device being used. The standard requires reference to BS1523, “Glossary of terms used in automatic controlling and regulating systems”, Section3: “Kinetic control”, and Section5: “Components of servo-mechanisms”. A British Standard does not purport to include all th
7、e 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 cover, pagesi andii, p
8、ages1 to13 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. Amendments issued since publication Amd. No. Date of issue Comments 2281 May1977 Indicated by a sideline
9、 in the marginBSG183:1963 BSI 03-2000 i Contents Page Foreword Inside front cover 1 Scope 1 2 Definitions 1 Section 1. Basic principles 3 Sensing 1 4 Error signals 1 5 Reference voltage (a.c. or d.c.) 1 Section 2. Signal polarities of synchros 6 Synchro types and circuits 1 7 Pin (or terminal) lette
10、ring 1 8 Pin connection sequence 3 9 Rotation convention 3 10 Positive rotation 3 Section 3. A.C. and D.C. signal polarities other than synchros 11 A.C. signals 5 12 D.C. signals 5 13 A.C. motors 5 14 D.C. motors 6 15 Amplifier units 6 a) Inputs 6 b) Feedback inputs 6 c) Outputs 6 d) Motors 6 Sectio
11、n 4. Power supplies 16 A.C. supply 7 17 D.C. supply 7 Section 5. Datum settings 18 Sensing 7 Appendix Datum and sensing of synchros 8 Introduction 8 A.1 Torque transmitter TX: Control transmitter CX: Torque receiver TR 8 A.2 Control transformer CT 9 A.3 Torque differential transmitter TDX: Control d
12、ifferential transmitter CDX: Torque differential receiver TDR 10 A.4 Resolver RS (seven-terminal) 12 A.5 Resolver RS (eight-terminal) 13 A.6 Resolver RS (six-terminal) 13 Figure 1 Functions and symbols of synchros 2 Figure 2 3 Figure 3 3 Figure 4 4 Figure 5 5 Figure 6 6 Figure 7 8 Figure 8 9 Figure
13、9 9 Figure 10 9 Figure 11 10BSG183:1963 ii BSI 03-2000 Page Figure 12 10 Figure 13 10 Figure 14 11 Figure 15 11 Figure 16 12 Figure 17 12 Figure 18 12 Figure 19 13 Figure 20 13 Table 1 Equivalent connections 3 Table 2 3 Table 3 4 Table 4 5 Table 5 7BSG183:1963 BSI 03-2000 1 1 Scope This BritishStand
14、ard relates to the interconnections in control and indicating systems in aircraft using analogue transmissions. 2 Definitions For the purposes of this BritishStandard, the definitions in BS1523, Sections3 and 5, and the following apply: error signal desired (or command) signal minus actual signal eq
15、uals error signal NOTEThis definition has not appeared previously in BritishStandards, but the term “error signal” has been used in this context because of its common usage and of its appearance in the ARINC synchro system manual. It should be noted that it differs from the terms “indication error”
16、in BS2643, Section3, Term311, and “deviation” in BS152, Section3, Term3113. Section 1. Basic principles 3 Sensing The basic principle for sensing shall be: positive signal for an increasing function. 4 Error signals For command signals the error signal shall be the desired (or command) signal less t
17、he actual signal. Thus, if the desired signal is greater than the actual signal, the error signal is positive, and vice versa. Hence, an error signal is positive if an increase in output function is required to bring the actual output signal up to the desired signal. 5 Reference voltage (A.C. or D.C
18、.) a) The reference voltage shall be the standard to which other voltages in the system shall be referred in respect of phase and magnitude. b) The reference voltage shall be the voltage between two lines, or a line to neutral, of the power supply to the system. c) The reference voltage shall be sta
19、ted and should preferably be phase AB. NOTE 1This reference voltage should not be confused with the motor fixed field voltage often referred to in text books as the Motor reference voltage. NOTE 2Any a.c. data transmission device should receive its excitation from the circuit employing the receiving
20、 device. Section 2. Signal polarities of synchros 6 Synchro types and circuits a) The symbols and functions of synchros in common use are shown in Figure 1. b) Coarse-fine synchros shall be treated as two separate devices. 7 Pin (or terminal) lettering It is not possible to use for this purpose the
21、letters marked on the synchro terminals because these are associated with a standard direction of rotation which may not obtain in the equipment. The equipment terminals shall be lettered from P to Z (omitting V). This convention is the same as that suggested in the E.E.A. manual. In the ARINC syste
22、m H is equivalent to P and C to Q. Table 1 shows the equivalent connections for a synchro at electrical zero which have the same characteristic as a standard synchro zeroed by the method described in the Appendix. BS G 183:1963 2 BSI 03-2000 Function Abbreviations Alternative symbols Function Abbrev
23、iations Alternative symbols A Torque transmitter Control transmitter Torque receiver TX, TXB CX, CXB TR, TRB F Resolver differential or computing 7 terminals RS B Torque differential transmitter Control differential transmitter Torque differential receiver TDX, CDX, CDXB TDR, G Resolver control tran
24、sformer RS C Control transformer CT, CTB H Resolver control transmitter RS D Resolver differential or computing 8 terminals RS J Feedback resolver RSF E Resolver differential or computing 6 terminals RS NOTETerminals marked “R” refer to the rotor; those marked “S” refer to the stator. Figure 1 Funct
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