曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專營(yíng)店坑蒙拐騙欺詐消費(fèi)者

About the Authors
Acknowledgements
List of Abbreviations
Introduction
Systems Integration
Systems Interaction
1 Flight Control Systems
1.1 Introduction
1.2 Principles of Flight Control
1.3 Flight Control Surfaces
1.4 Primary Flight Control
1.5 Secondary Flight Control
1.6 Commercial Aircraft
1.6.1 Primary Flight Control
1.6.2 Secondary Flight Control
1.7 Flight Control Linkage Systems
1.7.1 Push-Pull Control Rod System
1.7.2 Cable and Pulley System
1.8 High Lift Control Systems
1.9 Trim and Feel
1.9.1 Trim
1.9.2 Feel
1.10 Flight Control Actuation
1.10.1 Simple Mechanical/Hydraulic Actuation
1.10.2 Mechanical Actuation with Electrical Signalling
1.10.3 Multiple Redundancy Actuation
1.10.4 Mechanical Screwjack Actuator
1.10.5 Integrated Actuator Package (IAP)
1.10.6 Advanced Actuation Implementations
1.11 Civil System Implementations
1.11.1 Top-Level Comparison
1.11.2 Airbus Implementation
1.12 Fly-By-Wire Control Laws
1.13 A380 Flight Control Actuation
1.14 Boeing 777 Implementation
1.15 Interrelationship of Flight Control, Guidance and Flight
Management
2 Engine Control Systems
2.1 Introduction
2.1.1 Engine/Airframe Interfaces
2.2 Engine Technology and Principles of Operation
2.3 The Control Problem
2.3.1 Fuel Flow Control
2.3.2 Air Flow Control
2.3.3 Control Systems
2.3.4 Control System Parameters
2.3.5 Input Signals
2.3.6 Output Signals
2.4 Example Systems
2.5 Design Criteria
2.6 Engine Starting
2.6.1 Fuel Control
2.6.2 Ignition Control
2.6.3 Engine Rotation
2.6.4 Throttle Levers
2.6.5 Starting Sequence
2.7 Engine Indications
2.8 Engine Oil Systems
2.9 Engine Offtakes
2.10 Reverse Thrust
2.11 Engine Control on Modern Civil Aircraft
3 Fuel Systems
3.1 Introduction
3.2 Characteristics of Fuel Systems
3.3 Description of Fuel System Components
3.3.1 Fuel Transfer Pumps
3.3.2 Fuel Booster Pumps
3.3.3 Fuel Transfer Valves
3.3.4 Non-Return Valves (NRVs)
3.4 Fuel Quantity Measurement
3.4.1 Level Sensors
3.4.2 Fuel Gauging Probes
3.4.3 Fuel Quantity Measurement Basics
3.4.4 Tank Shapes
3.4.5 Fuel Properties
3.4.6 Fuel Quantity Measurement Systems
3.4.7 Fokker F50/F100 System
3.4.8 Airbus A320 System
3.4.9 ‘Smart' Probes
3.4.10 Ultrasonic Probes
3.5 Fuel System Operating Modes
3.5.1 Pressurisation
3.5.2 Engine Feed
3.5.3 Fuel Transfer
3.5.4 Refuel/Defuel
3.5.5 Vent Systems
3.5.6 Use of Fuel as a Heat Sink
3.5.7 External Fuel Tanks
3.5.8 Fuel Jettison
3.5.9 In-Flight Refuelling
3.6 Integrated Civil Aircraft Systems
3.6.1 Bombardier Global Express
3.6.2 Boeing 777
3.6.3 A340-500/600 Fuel System
3.7 Fuel Tank Safety
3.7.1 Principles of Fuel Inerting
3.7.2 Air Separation Technology
3.7.3 Typical Fuel Inerting System
3.8 Polar Operations – Cold Fuel Management
3.8.1 Minimum Equipment List (MEL)
3.8.2 Cold Fuel Characteristics
3.8.3 Fuel Temperature Indication
4 Hydraulic Systems
4.1 Introduction
4.2 Hydraulic Circuit Design
4.3 Hydraulic Actuation
4.4 Hydraulic Fluid
4.5 Fluid Pressure
4.6 Fluid Temperature
4.7 Fluid Flow Rate
4.8 Hydraulic Piping
4.9 Hydraulic Pumps
4.10 Fluid Conditioning
4.11 Hydraulic Reservoir
4.12 Warnings and Status
4.13 Emergency Power Sources
4.14 Proof of Design
4.15 Aircraft System Applications
4.15.1 The Avro RJ Hydraulic System
4.15.2 The BAE SYSTEMS Hawk 200 Hydraulic System
4.15.3 Tornado Hydraulic System
4.16 Civil Transport Comparison
4.16.1 Airbus A320
4.16.2 Boeing 767
4.17 Landing Gear Systems
4.17.1 Nose Gear
4.17.2 Main Gear
4.17.3 Braking Anti-Skid and Steering
4.17.4 Electronic Control
4.17.5 Automatic Braking
4.17.6 Multi-Wheel Systems
4.17.7 Brake Parachute
5 Electrical Systems
5.1 Introduction
5.1.1 Electrical Power Evolution
5.2 Aircraft Electrical System
5.3 Power Generation
5.3.1 DC Power Generation
5.3.2 AC Power Generation
5.3.3 Power Generation Control
5.4 Primary Power Distribution
5.5 Power Conversion and Energy Storage
5.5.1 Inverters
5.5.2 Transformer Rectifier Units (TRUs)
5.5.3 Auto-Transformers
5.5.4 Battery Chargers
5.5.5 Batteries
5.6 Secondary Power Distribution
5.6.1 Power Switching
5.6.2 Load Protection
5.7 Typical Aircraft DC System
　
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