《Aircraft Electrical and Electronic Systems：Principles, operation and mai...
《Aircraft Electrical and Electronic Systems：Principles, operation and maintenance》飞机电气和电子系统：原理、操作和维护
作者：Mike Tooley and David Wyatt
出版社：BH
出版时间：2009年
目录
Preface x
Acknowledgements xvi
Chapter 1 Electrical fundamentals 1
1.1 Electron theory 1
1.2 Electrostatics and capacitors 3
1.3 Direct current 6
1.4 Current, voltage and resistance 7
1.5 Power and energy 12
1.6 Electromagnetism and inductors 14
1.7 Alternating current and transformers 19
1.8 Safety 32
1.9 Multiple choice questions 33
Chapter 2 Electronic fundamentals 35
2.1 Semiconductor theory 35
2.2 Diodes 38
2.3 Transistors 49
2.4 Integrated circuits 55
2.5 Multiple choice questions 56
Chapter 3 Digital fundamentals 59
3.1 Logic gates 59
3.2 Combinational logic systems 60
3.3 Monostable devices 63
3.4 Bistable devices 65
3.5 Decoders 66
3.6 Encoders 69
3.7 Multiplexers 70
3.8 Bus systems 72
3.9 Computers 76
3.10 Multiple choice questions 78
Chapter 4 Generators and Motors 81
4.1 Generator and motor principles 81
4.2 AC generators 89
4.3 Three-phase generation and distribution 93
4.4 AC motors 95
vi Contents
4.5 Practical aircraft generating systems 104
4.6 Multiple choice questions 109
Chapter 5 Batteries 111
5.1 Overview 111
5.2 Storage cells 112
5.3 Lead-acid batteries 113
5.4 Nickel-cadmium batteries 117
5.5 Lithium batteries 120
5.6 Nickel-metal hydride batteries 120
5.7 Battery locations 122
5.8 Battery venting 122
5.9 Battery connections 122
5.10 Multiple choice questions 125
Chapter 6 Power supplies 127
6.1 Regulators 127
6.2 External power 131
6.3 Inverters 131
6.4 Transformer rectifi er units 133
6.5 Transformers 133
6.6 Auxiliary power unit (APU) 134
6.7 Emergency power 136
6.8 Multiple choice questions 136
Chapter 7 Wiring and circuit protection 137
7.1 Overview 137
7.2 Construction and materials 138
7.3 Specifi cations 139
7.4 Shielding/screening 140
7.5 Circuit protection 142
7.6 Multiple choice questions 146
Chapter 8 Distribution of power supplies 147
8.1 Single engine/general aviation 147
8.2 Twin engine general aviation aircraft 151
8.3 Larger aircraft systems 152
8.4 Split bus system 153
8.5 Parallel bus system 155
8.6 Split/parallel bus system 155
8.7 Standby and essential power 155
8.8 Battery charging 156
8.9 Control and protection 157
8.10 Load shedding 159
8.11 Multiple choice questions 163
vii
Chapter 9 Controls and transducers 165
9.1 Switches 165
9.2 Relays and contactors 168
9.3 Variable resistors 170
9.4 Linear displacement transducers 171
9.5 Fluid pressure transducers 174
9.6 Temperature transducers 175
9.7 Strain transducers 179
9.8 Rotary position transducers 180
9.9 Multiple choice questions 182
Chapter 10 Engine systems 185
10.1 Starting and ignition 185
10.2 Indicating systems overview 195
10.3 Primary indicating systems 195
10.4 Secondary indicating systems 205
10.5 Electronic indicating systems 206
10.6 Multiple choice questions 210
Chapter 11 Fuel management 213
11.1 Storage overview 213
11.2 Fuel quantity measurement and indication 213
11.3 Fuel feed and distribution 218
11.4 Fuel transfer 220
11.5 Refuelling and defuelling 221
11.6 Fuel jettison 221
11.7 Fuel system venting 221
11.8 Fuel tank inerting 221
11.9 Multiple choice questions 223
Chapter 12 Lights 225
12.1 Lighting technologies 225
12.2 Flight compartment lights 226
12.3 Passenger cabin lights 230
12.4 Exterior lights 232
12.5 Multiple choice questions 238
Chapter 13 Cabin systems 241
13.1 Passenger address system 241
13.2 Galley equipment 243
13.3 In-fl ight entertainment (IFE) 243
13.4 Satellite communications 244
13.5 Multiplexing 247
13.6 Fibre optics 248
13.7 Air conditioning 249
13.8 Pressurization 252
13.9 Airstairs 254
13.10 Multiple choice questions 254
Contents
viii Contents
Chapter 14 Airframe control and indicating systems 257
14.1 Landing gear 257
14.2 Trailing edge fl aps 260
14.3 Control surfaces 261
14.4 Electronic indicating systems 262
14.5 Multiple choice questions 264
Chapter 15 Warning and protection systems 265
15.1 Stall warning and protection 265
15.2 Airframe ice and rain protection 271
15.3 Windscreen ice and rain protection 275
15.4 Anti-skid 277
15.5 Confi guration warnings 279
15.6 Aural warnings 281
15.7 Multiple choice questions 282
Chapter 16 Fire and overheat protection 283
16.1 Overview 283
16.2 Engine/APU fi re detection 284
16.3 Cargo bay/baggage area 291
16.4 Fire extinguishing 294
16.5 Multiple choice questions 298
Chapter 17 Terrain awareness warning systems (TAWS) 299
17.1 System overview 299
17.2 System warnings and protection 301
17.3 External references 303
17.4 Ground proximity modes 306
17.5 Forward looking terrain awareness (FLTA) 313
17.6 Rotorcraft TAWS 316
17.7 Architecture and confi gurations 317
17.8 Future developments 318
17.9 Multiple choice questions 318
Chapter 18 Flight data and cockpit voice recorders 321
18.1 Flight data recorder history 321
18.2 Mandatory equipment requirements 323
18.3 Flight data recorder (FDR) specifi cations 326
18.4 Cockpit voice recorders 332
18.5 Health and usage monitoring system (HUMS) 334
18.6 Multiple choice questions 334
Chapter 19 Electrical and magnetic fi elds 337
19.1 Electromagnetic interference 337
19.2 EMI reduction 342
19.3 High-intensity/energy radiated fi elds 343
ix
19.4 Lightning 344
19.5 Grounding and bonding 347
19.6 Electrostatic sensitive devices (ESSD) 348
19.7 Multiple choice questions 351
Chapter 20 Continuing airworthiness 353
20.1 Wire and cable installations 353
20.2 Bonding 359
20.3 Static charges 360
20.4 Earth returns 361
20.5 Aircraft manuals 362
20.6 Circuit testing 363
20.7 Automatic test equipment 366
20.8 On-board diagnostic equipment 366
20.9 Multiple choice questions 368
Appendix 1: Abbreviations and acronyms 369
Appendix 2: Revision papers 373
Appendix 3: Answers to multiple choice questions 379
Appendix 4: Electrical quantities, symbols and units 383
Appendix 5: Electrical formulae 385
Appendix 6: Decibels 387
Appendix 7: Wire and cable sizes 389
Appendix 8: ATA chapter/subsystem list 391
Appendix 9: Electrical and electronic symbols 395
Appendix 10: Wire numbering/coding 399
Index 401
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