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Aircraft Systems, 3rd Edition is thoroughly revised and expanded from the last edition in 2001, reflecting the significant technological and procedural changes that have occurred in the interim - new aircraft types, increased electronic implementation, developing markets, increased environmental pressures and the emergence of UAVs. Every chapter is updated, and the latest technologies depicted. It offers an essential reference tool for aerospace industry researchers and practitioners such as aircraft designers, fuel specialists, engine specialists, and ground crew maintenance providers, as well as a textbook for senior undergraduate and postgraduate students in systems engineering, aerospace and engineering avionics.
Aircraft Systems, 3rd Edition is thoroughly revised and expanded from the last edition in 2001, reflecting the significant technological and procedural changes that have occurred in the interim - new aircraft types, increased electronic implementation, developing markets, increased environmental pressures and the emergence of UAVs. Every chapter is updated, and the latest technologies depicted. It offers an essential reference tool for aerospace industry researchers and practitioners such as aircraft designers, fuel specialists, engine specialists, and ground crew maintenance providers, as well as a textbook for senior undergraduate and postgraduate students in systems engineering, aerospace and engineering avionics.
Allan Seabridge was until recently the Chief Flight Systems Engineer at BAE Systems at Warton in Lancashire in the UK. In over 30 years in the aerospace industry his work has latterly included the avionics systems on the Nimrod MRA 4 and Lockheed Martin Lightning II (Joint Strike Fighter) as well as a the development of a range of flight and avionics systems on a wide range of fast jets, training aircraft and ground and maritime surveillance projects. Spending much of his time between Europe and the US, Allan is fully aware of systems developments worldwide. he is also keen to encourage a further understanding of integrated engineering systems. An interest in engineering education continues with the design and delivery of systems and engineering courses at a number of UK universities at undergraduate and postgraduate level.
Foreword xvii
Series Preface xix
About the Authors xxi
Acknowledgements xxiii
List of Abbreviations xxv
Introduction xxxv
Systems Integration xxxvi
Systems Interaction xxxix
1 Flight Control Systems 1
1.1 Introduction 1
1.2 Principles of Flight Control 3
1.3 Flight Control Surfaces 4
1.4 Primary Flight Control 5
1.5 Secondary Flight Control 5
1.6 Commercial Aircraft 7
1.6.1 Primary Flight Control 7
1.6.2 Secondary Flight Control 7
1.7 Flight Control Linkage Systems 9
1.7.1 Push-Pull Control Rod System 10
1.7.2 Cable and Pulley System 11
1.8 High Lift Control Systems 13
1.9 Trim and Feel 15
1.9.1 Trim 15
1.9.2 Feel 17
1.10 Flight Control Actuation 18
1.10.1 Simple Mechanical/Hydraulic Actuation 19
1.10.2 Mechanical Actuation with Electrical Signalling 21
1.10.3 Multiple Redundancy Actuation 22
1.10.4 Mechanical Screwjack Actuator 26
1.10.5 Integrated Actuator Package (IAP) 27
1.10.6 Advanced Actuation Implementations 30
1.11 Civil System Implementations 34
1.11.1 Top-Level Comparison 35
1.11.2 Airbus Implementation 36
1.12 Fly-By-Wire Control Laws 40
1.13 A380 Flight Control Actuation 41
1.14 Boeing 777 Implementation 44
1.15 Interrelationship of Flight Control, Guidance and Flight Management 48
2 Engine Control Systems 51
2.1 Introduction 51
2.1.1 Engine/Airframe Interfaces 52
2.2 Engine Technology and Principles of Operation 53
2.3 The Control Problem 55
2.3.1 Fuel Flow Control 56
2.3.2 Air Flow Control 58
2.3.3 Control Systems 59
2.3.4 Control System Parameters 60
2.3.5 Input Signals 60
2.3.6 Output Signals 62
2.4 Example Systems 62
2.5 Design Criteria 71
2.6 Engine Starting 73
2.6.1 Fuel Control 73
2.6.2 Ignition Control 74
2.6.3 Engine Rotation 75
2.6.4 Throttle Levers 77
2.6.5 Starting Sequence 78
2.7 Engine Indications 78
2.8 Engine Oil Systems 81
2.9 Engine Offtakes 81
2.10 Reverse Thrust 83
2.11 Engine Control on Modern Civil Aircraft 84
3 Fuel Systems 87
3.1 Introduction 87
3.2 Characteristics of Fuel Systems 89
3.3 Description of Fuel System Components 90
3.3.1 Fuel Transfer Pumps 90
3.3.2 Fuel Booster Pumps 91
3.3.3 Fuel Transfer Valves 92
3.3.4 Non-Return Valves (NRVs) 93
3.4 Fuel Quantity Measurement 94
3.4.1 Level Sensors 94
3.4.2 Fuel Gauging Probes 96
3.4.3 Fuel Quantity Measurement Basics 96
3.4.4 Tank Shapes 97
3.4.5 Fuel Properties 98
3.4.6 Fuel Quantity Measurement Systems 101
3.4.7 Fokker F50/F100 System 101
3.4.8 Airbus A320 System 103
3.4.9 'Smart' Probes 104
3.4.10 Ultrasonic Probes 105
3.5 Fuel System Operating Modes 105
3.5.1 Pressurisation 106
3.5.2 Engine Feed 106
3.5.3 Fuel Transfer 108
3.5.4 Refuel/Defuel 109
3.5.5 Vent Systems 111
3.5.6 Use of Fuel as a Heat Sink 112
3.5.7 External Fuel Tanks 112
3.5.8 Fuel Jettison 113
3.5.9 In-Flight Refuelling 114
3.6 Integrated Civil Aircraft Systems 116
3.6.1 Bombardier Global Express 117
3.6.2 Boeing 777 119
3.6.3 A340-500/600 Fuel System 120
3.7 Fuel Tank Safety 128
3.7.1 Principles of Fuel Inerting 129
3.7.2 Air Separation Technology 130
3.7.3 Typical Fuel Inerting System 131
3.8 Polar Operations - Cold Fuel Management 133
3.8.1 Minimum Equipment List (MEL) 133
3.8.2 Cold Fuel Characteristics 134
3.8.3 Fuel Temperature Indication 135
4 Hydraulic Systems 137
4.1 Introduction 137
4.2 Hydraulic Circuit Design 138
4.3 Hydraulic Actuation 142
4.4 Hydraulic Fluid 144
4.5 Fluid Pressure 145
4.6 Fluid Temperature 145
4.7 Fluid Flow Rate 146
4.8 Hydraulic Piping 146
4.9 Hydraulic Pumps 147
4.10 Fluid Conditioning 151
4.11 Hydraulic Reservoir 152
4.12 Warnings and Status 152
4.13 Emergency Power Sources 153
4.14 Proof of Design 154
4.15 Aircraft System Applications 155
4.15.1 The Avro RJ Hydraulic System 156
4.15.2 The BAE SYSTEMS Hawk 200 Hydraulic System 161
4.15.3 Tornado Hydraulic System 161
4.16 Civil Transport Comparison 163
4.16.1 Airbus A 320 164
4.16.2 Boeing 767 165
4.17 Landing Gear Systems 167
4.17.1 Nose Gear 167
4.17.2 Main Gear 168
4.17.3 Braking Anti-Skid and Steering 169
4.17.4 Electronic Control 172
4.17.5 Automatic Braking 173
4.17.6 Multi-Wheel Systems 175
4.17.7 Brake Parachute 178
5 Electrical Systems 181
5.1 Introduction 181
5.1.1 Electrical Power Evolution 181
5.2 Aircraft Electrical System 184
5.3 Power Generation 185
5.3.1 DC Power Generation 185
5.3.2 AC Power Generation 186
5.3.3 Power Generation Control 188
5.4 Primary Power Distribution 199
5.5 Power Conversion and Energy Storage 201
5.5.1 Inverters 201
5.5.2 Transformer Rectifier Units (TRUs) 201
5.5.3 Auto-Transformers 202
5.5.4 Battery Chargers 202
5.5.5 Batteries 203
5.6 Secondary Power Distribution 203
5.6.1 Power Switching 203
5.6.2 Load Protection 204
5.7 Typical Aircraft DC System 207
5.8 Typical Civil Transport Electrical System 208
5.9 Electrical Loads 210
5.9.1 Motors and Actuation 210
5.9.2 DC Motors 211
5.9.3 AC Motors 212
5.9.4 Lighting 212
5.9.5 Heating 213
5.9.6 Subsystem Controllers and Avionics Systems 213
5.9.7 Ground Power 214
5.10 Emergency Power Generation 214
5.10.1 Ram Air Turbine 215
5.10.2 Backup Power Converters 215
5.10.3 Permanent Magnet Generators (PMGs) 216
5.11 Recent Systems Developments 218
5.11.1 Electrical Load Management System (ELMS) 218
5.11.2 Variable Speed Constant Frequency (VSCF) 220
5.11.3 270 VDC Systems 227
5.11.4 More-Electric Aircraft (MEA) 227
5.12 Recent Electrical System Developments 228
5.12.1 Airbus A380 Electrical System Overview 229
5.12.2 A400m 234
5.12.3 B787 Electrical Overview 234
5.13 Electrical Systems Displays 237
6 Pneumatic Systems 239
6.1 Introduction 239
6.2 Use of Bleed Air 240
6.3 Engine Bleed Air Control 244
6.4 Bleed Air System Indications 247
6.5 Bleed Air System Users 247
6.5.1 Wing and Engine Anti-Ice 248
6.5.2 Engine Start 250
6.5.3 Thrust Reversers 251
6.5.4 Hydraulic Systems 251
6.6 Pitot Static Systems 252
6.6.1 Innovative Methods of Pitot-Static Measurement 256
7 Environmental Control Systems 259
7.1 Introduction 259
7.2 The Need for a Controlled Environment 260
7.2.1 Kinetic Heating 260
7.2.2 Solar Heating 261
7.2.3 Avionics Heat Loads 262
7.2.4 Airframe System Heat Loads 262
7.2.5 The Need for Cabin Conditioning 262
7.2.6 The Need for Avionics Conditioning 263
7.3 The International Standard Atmosphere (ISA) 263
7.4 Environmental Control System Design 266
7.4.1 Ram Air Cooling 266
7.4.2 Fuel Cooling 267
7.4.3 Engine Bleed 267
7.4.4 Bleed Flow and Temperature Control 269
7.5 Cooling Systems 271
7.5.1 Air Cycle Refrigeration Systems 271
7.5.2 Turbofan System 272
7.5.3 Bootstrap System 272
7.5.4 Reversed Bootstrap 274
7.5.5 Ram Powered Reverse Bootstrap 274
7.5.6 Vapour Cycle Systems 275
7.5.7 Liquid Cooled Systems 276
7.5.8 Expendable Heat Sinks 277
7.6 Humidity Control 278
7.7 The Inefficiency of Present Systems 279
7.8 Air Distribution Systems 279
7.8.1 Avionics Cooling 279
7.8.2 Unconditioned Bays 280
7.8.3 Conditioned Bays 280
7.8.4 Conditioned Bay Equipment Racking 281
7.8.5 Ground Cooling 282
7.8.6 Cabin Distribution Systems 283
7.9 Cabin Noise 284
7.10 Cabin Pressurisation 284
7.11 Hypoxia 287
7.12 Molecular Sieve Oxygen Concentrators 288
7.13 g Tolerance 291
7.14 Rain Dispersal 292
7.15 Anti-Misting and De-Misting 293
7.16 Aircraft Icing 293
8 Emergency Systems 297
8.1 Introduction 297
8.2 Warning Systems 298
8.3 Fire Detection and Suppression 301
8.4 Emergency Power Sources 305
8.5 Explosion Suppression 307
8.6 Emergency Oxygen 308
8.7 Passenger Evacuation 308
8.8 Crew Escape 310
8.9 Computer-Controlled Seats 312
8.10 Ejection System Timing 313
8.11 High Speed Escape 314
8.12 Crash Recorder 314
8.13 Crash Switch 315
8.14 Emergency Landing 315
8.15 Emergency System Testing 317
9 Rotary Wing Systems 319
9.1 Introduction 319
9.2 Special Requirements of Helicopters 320
9.3 Principles of Helicopter Flight 321
9.4 Helicopter Flight Control 324
9.5 Primary Flight Control Actuation 325
9.5.1 Manual Control 326
9.5.2 Auto-Stabilisation 328
9.5.3 Autopilot Modes 330
9.6 Key Helicopter Systems 333
9.6.1 Engine and Transmission System 335
9.6.2 Hydraulic Systems 338
9.6.3 Electrical System 340
9.6.4 Health Monitoring System 341
9.6.5 Specialised Helicopter Systems 342
9.7 Helicopter Auto-Flight Control 343
9.7.1 EH 101 Flight Control System...
| Erscheinungsjahr: | 2008 |
|---|---|
| Fachbereich: | Fertigungstechnik |
| Genre: | Importe, Technik |
| Rubrik: | Naturwissenschaften & Technik |
| Medium: | Buch |
| Inhalt: | 504 S. |
| ISBN-13: | 9780470059968 |
| ISBN-10: | 0470059966 |
| Sprache: | Englisch |
| Herstellernummer: | 14505996000 |
| Einband: | Gebunden |
| Autor: |
Moir, Ian
Seabridge, Allan |
| Redaktion: | Langton, Roy |
| Auflage: | 3rd edition |
| Hersteller: |
Wiley
John Wiley & Sons |
| Verantwortliche Person für die EU: | Wiley-VCH GmbH, Boschstr. 12, D-69469 Weinheim, amartine@wiley-vch.de |
| Maße: | 251 x 176 x 35 mm |
| Von/Mit: | Ian Moir (u. a.) |
| Erscheinungsdatum: | 01.05.2008 |
| Gewicht: | 1,021 kg |
Allan Seabridge was until recently the Chief Flight Systems Engineer at BAE Systems at Warton in Lancashire in the UK. In over 30 years in the aerospace industry his work has latterly included the avionics systems on the Nimrod MRA 4 and Lockheed Martin Lightning II (Joint Strike Fighter) as well as a the development of a range of flight and avionics systems on a wide range of fast jets, training aircraft and ground and maritime surveillance projects. Spending much of his time between Europe and the US, Allan is fully aware of systems developments worldwide. he is also keen to encourage a further understanding of integrated engineering systems. An interest in engineering education continues with the design and delivery of systems and engineering courses at a number of UK universities at undergraduate and postgraduate level.
Foreword xvii
Series Preface xix
About the Authors xxi
Acknowledgements xxiii
List of Abbreviations xxv
Introduction xxxv
Systems Integration xxxvi
Systems Interaction xxxix
1 Flight Control Systems 1
1.1 Introduction 1
1.2 Principles of Flight Control 3
1.3 Flight Control Surfaces 4
1.4 Primary Flight Control 5
1.5 Secondary Flight Control 5
1.6 Commercial Aircraft 7
1.6.1 Primary Flight Control 7
1.6.2 Secondary Flight Control 7
1.7 Flight Control Linkage Systems 9
1.7.1 Push-Pull Control Rod System 10
1.7.2 Cable and Pulley System 11
1.8 High Lift Control Systems 13
1.9 Trim and Feel 15
1.9.1 Trim 15
1.9.2 Feel 17
1.10 Flight Control Actuation 18
1.10.1 Simple Mechanical/Hydraulic Actuation 19
1.10.2 Mechanical Actuation with Electrical Signalling 21
1.10.3 Multiple Redundancy Actuation 22
1.10.4 Mechanical Screwjack Actuator 26
1.10.5 Integrated Actuator Package (IAP) 27
1.10.6 Advanced Actuation Implementations 30
1.11 Civil System Implementations 34
1.11.1 Top-Level Comparison 35
1.11.2 Airbus Implementation 36
1.12 Fly-By-Wire Control Laws 40
1.13 A380 Flight Control Actuation 41
1.14 Boeing 777 Implementation 44
1.15 Interrelationship of Flight Control, Guidance and Flight Management 48
2 Engine Control Systems 51
2.1 Introduction 51
2.1.1 Engine/Airframe Interfaces 52
2.2 Engine Technology and Principles of Operation 53
2.3 The Control Problem 55
2.3.1 Fuel Flow Control 56
2.3.2 Air Flow Control 58
2.3.3 Control Systems 59
2.3.4 Control System Parameters 60
2.3.5 Input Signals 60
2.3.6 Output Signals 62
2.4 Example Systems 62
2.5 Design Criteria 71
2.6 Engine Starting 73
2.6.1 Fuel Control 73
2.6.2 Ignition Control 74
2.6.3 Engine Rotation 75
2.6.4 Throttle Levers 77
2.6.5 Starting Sequence 78
2.7 Engine Indications 78
2.8 Engine Oil Systems 81
2.9 Engine Offtakes 81
2.10 Reverse Thrust 83
2.11 Engine Control on Modern Civil Aircraft 84
3 Fuel Systems 87
3.1 Introduction 87
3.2 Characteristics of Fuel Systems 89
3.3 Description of Fuel System Components 90
3.3.1 Fuel Transfer Pumps 90
3.3.2 Fuel Booster Pumps 91
3.3.3 Fuel Transfer Valves 92
3.3.4 Non-Return Valves (NRVs) 93
3.4 Fuel Quantity Measurement 94
3.4.1 Level Sensors 94
3.4.2 Fuel Gauging Probes 96
3.4.3 Fuel Quantity Measurement Basics 96
3.4.4 Tank Shapes 97
3.4.5 Fuel Properties 98
3.4.6 Fuel Quantity Measurement Systems 101
3.4.7 Fokker F50/F100 System 101
3.4.8 Airbus A320 System 103
3.4.9 'Smart' Probes 104
3.4.10 Ultrasonic Probes 105
3.5 Fuel System Operating Modes 105
3.5.1 Pressurisation 106
3.5.2 Engine Feed 106
3.5.3 Fuel Transfer 108
3.5.4 Refuel/Defuel 109
3.5.5 Vent Systems 111
3.5.6 Use of Fuel as a Heat Sink 112
3.5.7 External Fuel Tanks 112
3.5.8 Fuel Jettison 113
3.5.9 In-Flight Refuelling 114
3.6 Integrated Civil Aircraft Systems 116
3.6.1 Bombardier Global Express 117
3.6.2 Boeing 777 119
3.6.3 A340-500/600 Fuel System 120
3.7 Fuel Tank Safety 128
3.7.1 Principles of Fuel Inerting 129
3.7.2 Air Separation Technology 130
3.7.3 Typical Fuel Inerting System 131
3.8 Polar Operations - Cold Fuel Management 133
3.8.1 Minimum Equipment List (MEL) 133
3.8.2 Cold Fuel Characteristics 134
3.8.3 Fuel Temperature Indication 135
4 Hydraulic Systems 137
4.1 Introduction 137
4.2 Hydraulic Circuit Design 138
4.3 Hydraulic Actuation 142
4.4 Hydraulic Fluid 144
4.5 Fluid Pressure 145
4.6 Fluid Temperature 145
4.7 Fluid Flow Rate 146
4.8 Hydraulic Piping 146
4.9 Hydraulic Pumps 147
4.10 Fluid Conditioning 151
4.11 Hydraulic Reservoir 152
4.12 Warnings and Status 152
4.13 Emergency Power Sources 153
4.14 Proof of Design 154
4.15 Aircraft System Applications 155
4.15.1 The Avro RJ Hydraulic System 156
4.15.2 The BAE SYSTEMS Hawk 200 Hydraulic System 161
4.15.3 Tornado Hydraulic System 161
4.16 Civil Transport Comparison 163
4.16.1 Airbus A 320 164
4.16.2 Boeing 767 165
4.17 Landing Gear Systems 167
4.17.1 Nose Gear 167
4.17.2 Main Gear 168
4.17.3 Braking Anti-Skid and Steering 169
4.17.4 Electronic Control 172
4.17.5 Automatic Braking 173
4.17.6 Multi-Wheel Systems 175
4.17.7 Brake Parachute 178
5 Electrical Systems 181
5.1 Introduction 181
5.1.1 Electrical Power Evolution 181
5.2 Aircraft Electrical System 184
5.3 Power Generation 185
5.3.1 DC Power Generation 185
5.3.2 AC Power Generation 186
5.3.3 Power Generation Control 188
5.4 Primary Power Distribution 199
5.5 Power Conversion and Energy Storage 201
5.5.1 Inverters 201
5.5.2 Transformer Rectifier Units (TRUs) 201
5.5.3 Auto-Transformers 202
5.5.4 Battery Chargers 202
5.5.5 Batteries 203
5.6 Secondary Power Distribution 203
5.6.1 Power Switching 203
5.6.2 Load Protection 204
5.7 Typical Aircraft DC System 207
5.8 Typical Civil Transport Electrical System 208
5.9 Electrical Loads 210
5.9.1 Motors and Actuation 210
5.9.2 DC Motors 211
5.9.3 AC Motors 212
5.9.4 Lighting 212
5.9.5 Heating 213
5.9.6 Subsystem Controllers and Avionics Systems 213
5.9.7 Ground Power 214
5.10 Emergency Power Generation 214
5.10.1 Ram Air Turbine 215
5.10.2 Backup Power Converters 215
5.10.3 Permanent Magnet Generators (PMGs) 216
5.11 Recent Systems Developments 218
5.11.1 Electrical Load Management System (ELMS) 218
5.11.2 Variable Speed Constant Frequency (VSCF) 220
5.11.3 270 VDC Systems 227
5.11.4 More-Electric Aircraft (MEA) 227
5.12 Recent Electrical System Developments 228
5.12.1 Airbus A380 Electrical System Overview 229
5.12.2 A400m 234
5.12.3 B787 Electrical Overview 234
5.13 Electrical Systems Displays 237
6 Pneumatic Systems 239
6.1 Introduction 239
6.2 Use of Bleed Air 240
6.3 Engine Bleed Air Control 244
6.4 Bleed Air System Indications 247
6.5 Bleed Air System Users 247
6.5.1 Wing and Engine Anti-Ice 248
6.5.2 Engine Start 250
6.5.3 Thrust Reversers 251
6.5.4 Hydraulic Systems 251
6.6 Pitot Static Systems 252
6.6.1 Innovative Methods of Pitot-Static Measurement 256
7 Environmental Control Systems 259
7.1 Introduction 259
7.2 The Need for a Controlled Environment 260
7.2.1 Kinetic Heating 260
7.2.2 Solar Heating 261
7.2.3 Avionics Heat Loads 262
7.2.4 Airframe System Heat Loads 262
7.2.5 The Need for Cabin Conditioning 262
7.2.6 The Need for Avionics Conditioning 263
7.3 The International Standard Atmosphere (ISA) 263
7.4 Environmental Control System Design 266
7.4.1 Ram Air Cooling 266
7.4.2 Fuel Cooling 267
7.4.3 Engine Bleed 267
7.4.4 Bleed Flow and Temperature Control 269
7.5 Cooling Systems 271
7.5.1 Air Cycle Refrigeration Systems 271
7.5.2 Turbofan System 272
7.5.3 Bootstrap System 272
7.5.4 Reversed Bootstrap 274
7.5.5 Ram Powered Reverse Bootstrap 274
7.5.6 Vapour Cycle Systems 275
7.5.7 Liquid Cooled Systems 276
7.5.8 Expendable Heat Sinks 277
7.6 Humidity Control 278
7.7 The Inefficiency of Present Systems 279
7.8 Air Distribution Systems 279
7.8.1 Avionics Cooling 279
7.8.2 Unconditioned Bays 280
7.8.3 Conditioned Bays 280
7.8.4 Conditioned Bay Equipment Racking 281
7.8.5 Ground Cooling 282
7.8.6 Cabin Distribution Systems 283
7.9 Cabin Noise 284
7.10 Cabin Pressurisation 284
7.11 Hypoxia 287
7.12 Molecular Sieve Oxygen Concentrators 288
7.13 g Tolerance 291
7.14 Rain Dispersal 292
7.15 Anti-Misting and De-Misting 293
7.16 Aircraft Icing 293
8 Emergency Systems 297
8.1 Introduction 297
8.2 Warning Systems 298
8.3 Fire Detection and Suppression 301
8.4 Emergency Power Sources 305
8.5 Explosion Suppression 307
8.6 Emergency Oxygen 308
8.7 Passenger Evacuation 308
8.8 Crew Escape 310
8.9 Computer-Controlled Seats 312
8.10 Ejection System Timing 313
8.11 High Speed Escape 314
8.12 Crash Recorder 314
8.13 Crash Switch 315
8.14 Emergency Landing 315
8.15 Emergency System Testing 317
9 Rotary Wing Systems 319
9.1 Introduction 319
9.2 Special Requirements of Helicopters 320
9.3 Principles of Helicopter Flight 321
9.4 Helicopter Flight Control 324
9.5 Primary Flight Control Actuation 325
9.5.1 Manual Control 326
9.5.2 Auto-Stabilisation 328
9.5.3 Autopilot Modes 330
9.6 Key Helicopter Systems 333
9.6.1 Engine and Transmission System 335
9.6.2 Hydraulic Systems 338
9.6.3 Electrical System 340
9.6.4 Health Monitoring System 341
9.6.5 Specialised Helicopter Systems 342
9.7 Helicopter Auto-Flight Control 343
9.7.1 EH 101 Flight Control System...
| Erscheinungsjahr: | 2008 |
|---|---|
| Fachbereich: | Fertigungstechnik |
| Genre: | Importe, Technik |
| Rubrik: | Naturwissenschaften & Technik |
| Medium: | Buch |
| Inhalt: | 504 S. |
| ISBN-13: | 9780470059968 |
| ISBN-10: | 0470059966 |
| Sprache: | Englisch |
| Herstellernummer: | 14505996000 |
| Einband: | Gebunden |
| Autor: |
Moir, Ian
Seabridge, Allan |
| Redaktion: | Langton, Roy |
| Auflage: | 3rd edition |
| Hersteller: |
Wiley
John Wiley & Sons |
| Verantwortliche Person für die EU: | Wiley-VCH GmbH, Boschstr. 12, D-69469 Weinheim, amartine@wiley-vch.de |
| Maße: | 251 x 176 x 35 mm |
| Von/Mit: | Ian Moir (u. a.) |
| Erscheinungsdatum: | 01.05.2008 |
| Gewicht: | 1,021 kg |
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