BS 2G 134-1970 Specification for d c generators《直流发电机规范》.pdf
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1、BRITISH STANDARD AEROSPACE SERIES BS2G134: 1970 Specification for D.C. generators UDC 629.7.06:621.313.28BS2G 134:1970 This British Standard, having been approved by the AerospaceIndustry StandardsCommittee, waspublished under the authorityof the Executive Boardof the Institution on 23 October1970 B
2、SI 12-1999 The following BSI references relate to the work on this standard: Committee reference ACE/42 Draft for comment 67/28210 ISBN 0 580 06044 6 Foreword This revision of BSG134:1951, has been prepared as part of a programme of work to bring the Aerospace Series of British Standards for rotatin
3、g machines up to date in relation to present-day and probable future requirements, and in relation to experience gained in working on earlier issues of these standards. Reference is made in this standard to the following British Standards: BS2G100, General requirements for electrical equipment and i
4、ndicating instruments for aircraft Part1: Identification, declaration and construction Part2: Environmental and operating conditions Section2:Radio interference Part3: Characteristics of aircraft electrical systems. BS3G100, General requirements for aircraft equipment Part2: All equipment. BS3G100-3
5、, Environmental conditions Section3.1: Vibration Section3.2: Temperature-pressure requirements 1) . BSG102, General requirements for rotating electrical machinery 1) . BSSP20, Panel type air filter elements for use with internal combustion engines and compressors on aircraft. NOTEInformation regardi
6、ng metric (SI) units is given in BS350, “Conversion factors and tables”, and PD5686, “The use of SI units”. 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. Compliance with a British S
7、tandard does not of itself confer immunity from legal obligations. Summary of pages This document comprises a front cover, an inside front cover, pages i and ii, pages1 to9 and a back cover. This standard has been updated (see copyright date) and may have had amendments incorporated. This will be in
8、dicated in the amendment table on the inside front cover. 1) In course of preparation. Amendments issued since publication Amd. No. Date CommentsBS2G 134:1970 BSI 12-1999 i Contents Page Foreword Inside front cover 1 General 1.1 Scope 1 1.2 Design and construction 1 1.3 Standard voltage 1 1.4 Coolin
9、g arrangements 1 1.5 Mounting and drive 1 1.6 Electrical connection 1 1.7 Radio interference suppression 1 1.8 Rating and overload requirements 1 1.9 Efficiency 1 1.10 Excitation 1 1.11 Overspeed 1 1.12 Environmental conditions 2 1.13 Declaration of performance 2 1.14 Nameplate 2 2 Tests 2.1 General
10、 2 2.2 Test conditions 2 2.3 Type tests 2 2.3.1 Weight, centre of gravity and rotor inertia 2 2.3.2 Initial check 2 2.3.3 Cold resistance of windings 2 2.3.4 Commutation 2 2.3.5 Magnetization characteristics 3 2.3.6 Ripple voltage 3 2.3.7 Brush performance at altitude 3 2.3.8 Temperature 3 2.3.9 Tem
11、perature (shortened standard test) 3 2.3.10 Insulation resistance 4 2.3.11 Overspeed 4 2.3.12 Containment 4 2.3.13 Endurance, overload and radio interference suppression 4 2.3.14 Vibration 4 2.3.15 Acceleration 4 2.3.16 Temperature-pressure 4 2.3.17 Mould growth 4 2.3.18 Compass interference 4 2.3.1
12、9 Waterproofness 5 2.3.20 Salt corrosion 5 2.3.21 Dust and sand 5 2.3.22 Fluid contamination 5 2.4 Production routine tests 5 2.4.1 Component check 5 2.4.2 Resistance of windings 5 2.4.3 Brush bedding and adjustment 5 2.4.4 Temperature 5 2.4.5 Overspeed 5BS2G 134:1970 ii BSI 12-1999 Page 2.4.6 Loadi
13、ng 5 2.4.7 Insulation 5 2.5 Production quality tests 5 2.5.1 Selection of samples 5 2.5.2 Testing 6 Appendix A Salt corrosion test 7 Appendix B Dust and sand test 7 Appendix C Fluid contamination test 9 Figure 1 Measuring device for dust and sand test 8BS2G 134:1970 BSI 12-1999 1 1 General 1.1 Scope
14、 This British Standard applies to generators for aircraft d.c.power supply. It is intended to be read in conjunction with the relevant parts of BS2G100 or BS3G100, and BSG102. 1.2 Design and construction 1.2.1 Unless otherwise stated the design and construction of the machine shall comply with the r
15、elevant requirements of BS2G100 or BS3G100, and BSG102. 1.2.2 The design aim should be to achieve3000 (aircraft) hours operation of the machine before maintenance is necessary. 1.3 Standard voltage The terminal voltage shall be compatible with the requirements of BS2G100-3. 1.4 Cooling arrangements
16、1.4.1 The cooling arrangements shall be as agreed between the manufacturer and the purchaser. 1.4.2 Cooling connections shall comply with the requirements of BSG102. 1.5 Mounting and drive The mounting and drive of the machine shall comply with the requirements of BSG102. 1.6 Electrical connection 1
17、.6.1 The electrical connections shall comply with the requirements of BS2G100-1. 1.6.2 Terminals shall be provided for both positive and negative leads and also for the open end of the excitation winding and other connections as specified. 1.6.3 Provision may be made in the terminal box for changes
18、in the direction of rotation. When this is done a clear and permanent indication shall be provided in the terminal box, showing the correct connections to suit the two directions of rotation. 1.7 Radio interference suppression If specified in the relevant individual specification, provision shall be
19、 made for internal suppression, or alternatively the machine shall be provided with attachments suitable for screened cable connections. 1.8 Rating and overload requirements 1.8.1 The manufacturer shall declare the continuous rated output of the machine under declared conditions of speed, altitude a
20、nd cooling, as required by the design specification. 1.8.2 Following normal rated-load operation at steady temperature conditions, the generator shall be capable of: 1) maintaining125% rated-load current at rated voltage and125% of minimum speed for a period of5 minutes; 2) producing at least200% ra
21、ted current for5seconds. 1.9 Efficiency The manufacturer shall declare the power required to drive the machine at rated voltage and current over the speed range when at stabilized temperature conditions with cooling at rated air flow appropriate to sea level conditions, and when being controlled by
22、the appropriate voltage regulator. 1.10 Excitation 1.10.1 The excitation system shall be independent of any external electrical supply and shall be capable of initial build up without reference to any other supply. Supplementary excitation may be employed by agreement between the manufacturer and th
23、e purchaser. 1.10.2 To assist in limiting radio noise any windings connected in series with the armature should preferably be disposed symmetrically in the armature circuit. 1.11 Overspeed Consideration should be given to the highest speed at which the machine could be driven, in the applications fo
24、r which it is intended, if all overspeed protection devices fail. If this speed is more than120% of the maximum rated speed, the machine shall be designed either to withstand the highest speed or to fail at a lower speed of not less than120% of the maximum rated speed and to contain all its parts wi
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