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E-raamat: Aircraft Electrical and Electronic Systems 2nd edition [Taylor & Francis e-raamat]

(Gama Aviation, UK), (Brooklands College, UK)
  • Formaat: 420 pages, 24 Tables, black and white; 505 Line drawings, black and white; 113 Halftones, black and white; 618 Illustrations, black and white
  • Ilmumisaeg: 29-May-2018
  • Kirjastus: Routledge
  • ISBN-13: 9780429504228
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  • Taylor & Francis e-raamat
  • Hind: 216,96 €*
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Aircraft Electrical and Electronic Systems 2nd editionSuurem pilt
  • Formaat: 420 pages, 24 Tables, black and white; 505 Line drawings, black and white; 113 Halftones, black and white; 618 Illustrations, black and white
  • Ilmumisaeg: 29-May-2018
  • Kirjastus: Routledge
  • ISBN-13: 9780429504228
Teised raamatud teemal:
Taylor & Francis e-raamatudRohkem infot Taylor & Francis e-raamatute kohta
Raamatu kodulehekülg: https://www.taylorfrancis.com/books/9780429504228
Introducing the principles of aircraft electrical and electronic systems, this book is written for anyone pursuing a career in aircraft maintenance engineering or a related aerospace engineering discipline, and in particular will be suitable for those studying for licensed aircraft maintenance engineer status. It systematically addresses the relevant sections of modules 11 and 13 of part-66 of the EASA syllabus, and is ideal for anyone studying as part of an EASA and FAR-147 approved course in aerospace engineering.











Delivers the essential principles and knowledge base required by Airframe and Propulsion (A&P) Mechanics for Modules 11 and 13 of the EASA Part-66 syllabus and BTEC National awards in aerospace engineering





Supports Mechanics, Technicians and Engineers studying for a Part-66 qualification





Comprehensive and accessible, with self-test questions, exercises and multiple choice questions to enhance learning for both independent and tutor-assisted study

This second edition has been updated to incorporate: complex notation for the analysis of alternating current (AC) circuits; an introduction to the "all electric aircraft" utilising new battery technologies; updated sensor technology using integrated solid-state technology micro-electrical-mechanical sensors (MEMS); an expanded section on helicopter/rotary wing health usage monitoring systems (HUMS).
Preface to the second edition x
Preface xii
Acknowledgements xviii
Chapter 1 Electrical fundamentals
1(38)
1.1 Electron theory
1(2)
1.2 Electrostatics and capacitors
3(3)
1.3 Direct current
6(1)
1.4 Current, voltage and resistance
7(5)
1.5 Power and energy
12(2)
1.6 Electromagnetism and inductors
14(5)
1.7 Alternating current and transformers
19(17)
1.8 Safety
36(1)
1.9 Multiple choice questions
37(2)
Chapter 2 Electronic fundamentals
39(26)
2.1 Semiconductor theory
39(3)
2.2 Diodes
42(11)
2.3 Transistors
53(6)
2.4 Integrated circuits
59(1)
2.5 Sensors and transducers
60(2)
2.6 Multiple choice questions
62(3)
Chapter 3 Digital fundamentals
65(22)
3.1 Logic gates
65(1)
3.2 Combinational logic systems
66(3)
3.3 Monostable devices
69(2)
3.4 Bistable devices
71(1)
3.5 Decoders
72(3)
3.6 Encoders
75(1)
3.7 Multiplexers
76(2)
3.8 Bus systems
78(4)
3.9 Computers
82(2)
3.10 Multiple choice questions
84(3)
Chapter 4 Generators and motors
87(30)
4.1 Generator and motor principles
87(8)
4.2 AC generators
95(4)
4.3 Three-phase generation and distribution
99(2)
4.4 AC motors
101(9)
4.5 Practical aircraft generating systems
110(5)
4.6 Multiple choice questions
115(2)
Chapter 5 Batteries
117(16)
5.1 Overview
117(1)
5.2 Storage cells
118(1)
5.3 Lead-acid batteries
119(4)
5.4 Nickel-cadmium batteries
123(3)
5.5 Lithium batteries
126(1)
5.6 Nickel-metal hydride batteries
126(2)
5.7 Battery locations
128(1)
5.8 Battery venting
128(1)
5.9 Battery connections
129(2)
5.10 Multiple choice questions
131(2)
Chapter 6 Power supplies
133(10)
6.1 Regulators
133(4)
6.2 External power
137(1)
6.3 Inverters
137(2)
6.4 Transformer rectifier units
139(1)
6.5 Transformers
139(1)
6.6 Auxiliary power unit (APU)
140(2)
6.7 Emergency power
142(1)
6.8 Multiple choice questions
142(1)
Chapter 7 Wiring and circuit protection
143(10)
7.1 Overview
143(1)
7.2 Construction and materials
144(1)
7.3 Specifications
145(1)
7.4 Shielding/screening
146(2)
7.5 Circuit protection
148(4)
7.6 Multiple choice questions
152(1)
Chapter 8 Distribution of power supplies
153(18)
8.1 Single engine/general aviation aircraft
153(4)
8.2 Twin engine general aviation aircraft
157(1)
8.3 Larger aircraft systems
158(1)
8.4 Split bus system
159(2)
8.5 Parallel bus system
161(1)
8.6 Split/parallel bus system
161(1)
8.7 Standby and essential power
161(1)
8.8 Battery charging
162(1)
8.9 Control and protection
163(2)
8.10 Load-shedding
165(4)
8.11 Multiple choice questions
169(2)
Chapter 9 Controls and transducers
171(22)
9.1 Switches
171(3)
9.2 Relays and contactors
174(2)
9.3 Variable resistors
176(1)
9.4 Linear displacement transducers
177(3)
9.5 Fluid pressure transducers
180(1)
9.6 Temperature transducers
181(4)
9.7 Strain transducers
185(1)
9.8 Rotary position transducers
186(2)
9.9 Accelerometers
188(1)
9.10 Solid state technology
189(1)
9.11 Multiple choice questions
189(4)
Chapter 10 Engine systems
193(28)
10.1 Starting and ignition
193(10)
10.2 Indicating systems overview
203(1)
10.3 Primary indicating systems
203(10)
10.4 Secondary indicating systems
213(1)
10.5 Electronic indicating systems
214(4)
10.6 Multiple choice questions
218(3)
Chapter 11 Fuel management
221(12)
11.1 Storage overview
221(1)
11.2 Fuel quantity measurement and indication
221(5)
11.3 Fuel feed and distribution
226(2)
11.4 Fuel transfer
228(1)
11.5 Refuelling and defuelling
229(1)
11.6 Fuel jettison
229(1)
11.7 Fuel tank venting
229(1)
11.8 Fuel tank inerting
229(2)
11.9 Multiple choice questions
231(2)
Chapter 12 Lights
233(16)
12.1 Lighting technologies
233(1)
12.2 Flight compartment lights
234(4)
12.3 Passenger cabin lights
238(2)
12.4 Exterior lights
240(6)
12.5 Multiple choice questions
246(3)
Chapter 13 Cabin systems
249(16)
13.1 Passenger address system
249(2)
13.2 Galley equipment
251(1)
13.3 In-flight entertainment (IFE)
251(1)
13.4 Satellite communications
252(3)
13.5 Multiplexing
255(1)
13.6 Fibre optics
256(1)
13.7 Air conditioning
257(3)
13.8 Pressurization
260(2)
13.9 Airstairs
262(1)
13.10 Multiple choice questions
262(3)
Chapter 14 Airframe monitoring, control and indicating systems
265(8)
14.1 Landing gear
265(3)
14.2 Trailing edge flaps
268(1)
14.3 Control surfaces
269(1)
14.4 Electronic indicating systems
270(2)
14.5 Multiple choice questions
272(1)
Chapter 15 Warning and protection systems
273(18)
15.1 Stall warning and protection
273(6)
15.2 Airframe ice and rain protection
279(4)
15.3 Windscreen ice and rain protection
283(2)
15.4 Anti-skid
285(2)
15.5 Configuration warning
287(2)
15.6 Aural warnings
289(1)
15.7 Multiple choice questions
290(1)
Chapter 16 Fire and overheat protection
291(16)
16.1 Overview
291(1)
16.2 Engine/APU fire detection
292(7)
16.3 Cargo bay/baggage area
299(3)
16.4 Fire extinguishing
302(4)
16.5 Multiple choice questions
306(1)
Chapter 17 Terrain awareness warning system (TAWS)
307(22)
17.1 System overview
307(2)
17.2 System warnings and protection
309(2)
17.3 External references
311(4)
17.4 Ground proximity modes
315(6)
17.5 Forward-looking terrain avoidance (FLTA)
321(3)
17.6 Rotorcraft TAWS
324(1)
17.7 Architecture and configurations
325(1)
17.8 Future developments
326(1)
17.9 Multiple choice questions
326(3)
Chapter 18 Flight data and cockpit voice recorders
329(18)
18.1 Flight data recorder history
329(2)
18.2 Mandatory equipment requirements
331(3)
18.3 Flight data recorder (FDR) specifications
334(6)
18.4 Cockpit voice recorders
340(2)
18.5 Health and usage monitoring system (HUMS)
342(2)
18.6 Multiple choice questions
344(3)
Chapter 19 Electrical and magnetic fields
347(14)
19.1 Electromagnetic interference
347(5)
19.2 EMI reduction
352(1)
19.3 High-intensity/energy radiated fields
353(1)
19.4 Lightning
354(3)
19.5 Grounding and bonding
357(1)
19.6 Multiple choice questions
358(3)
Chapter 20 Continuing airworthiness
361(20)
20.1 Wire and cable installations
361(6)
20.2 Bonding
367(1)
20.3 Static charges
368(1)
20.4 Earth returns
369(1)
20.5 Aircraft manuals
370(1)
20.6 Circuit testing
371(3)
20.7 Automatic test equipment
374(1)
20.8 On-board diagnostic equipment
374(2)
20.9 Electrostatic sensitive devices (ESSDs)
376(2)
20.10 Multiple choice questions
378(3)
Appendix 1 Abbreviations and acronyms 381(6)
Appendix 2 Revision papers 387(6)
Appendix 3 Answers to multiple choice questions 393(4)
Appendix 4 Electrical quantities, symbols and units 397(2)
Appendix 5 Electrical formulae 399(2)
Appendix 6 Decibels 401(2)
Appendix 7 Wire and cable sizes 403(2)
Appendix 8 ATA chapter/subsystem list 405(4)
Appendix 9 Electrical and electronic symbols 409(4)
Appendix 10 Wire numbering/coding 413(2)
Index 415
David Wyatt has over 45 years experience in the aviation industry. This is founded on a technician apprenticeship with BOAC, progressing onto a development engineer in technical services. He then held various positions after leaving BA, including product support engineer, key account manager and FE lecturer in avionics engineering. These roles covered a range of avionic systems including: flight management systems, auto flight control systems, flight instruments, engine sensors and fire protection systems. David's final role was Head of Airworthiness in the design office at Gama Aviation.

Mike Tooley has over 30 years of teaching electronic principles, electronics and avionics to engineers and technicians, previously as Head of Department of Engineering and Vice Principal at Brooklands College in Surrey, UK, and currently works as a consultant and freelance technical author.
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