作者：周洁敏，陶思钰编著
页数：267页
出版社：北京航空航天大学出版社
出版日期：2024
ISBN：9787512444126
电子书格式：pdf/epub/txt
网盘下载地址：下载现代飞机电气系统
内容简介
本书不仅主要介绍了未来先进飞机的组成、结构和工作原理，还介绍了MEA的技术特性。本书专门面向从事飞行器技术的科研人员和工程人员编写，系统介绍了MEA/AEA的发展概况、MEA/AEA的架构、MEA的供电系统、MEA的配电系统、MEA的电驱动技术、MEA的环境控制系统、MEA的电气照明技术、MEA的制动系统、MEA的热管理和能源优化、MEA的公共核心系统以及MEA电力电子技术的应用等。
本书可作为从事飞机业务的学生学科发展课程的教材，也可作为科研技术人员和工程技术人员的参考书。
目录
Chapter 1 Introduction
1.1 Definition of MEA/AEA and Changes in Power Consumption
1.1.1 Definition of MEA/AEA
1.1.2 Changes in Electric Power Consumption
1.1.3 Advantages of MEA/AEA
1.2 Key Technologies Needed for MEA/AEA
1.3 Current Status of Advanced Aircraft Electrical Technology
1.3.1 Development Status of Aircraft Electrical Technology
1.3.2 The Foundation to Support Technology Requirements
1.4 The Development Trends for the Aircraft
1.5 Summary
1.6 Exercises
Chapter 2 Architecture of MEA/AEA
2.1 Aircraft Primary Energy and Secondary Energy
2.1.1 Aircraft Primary Energy
2.1.2 Energy Demand of Traditional Aircraft
2.2 MEA Engine
2.2.1 Summary
2.2.2 Utilization of Conventional Engine Energy
2.2.3 Energy Utilization of MEE
2.3 Benefits of Secondary Energy Unification
2.3.1 Benefits of Engine Structure Optimization
2.3.2 Simplifies the Internal Structure of the Aircraft
2.3.3 Simplified the Ground Support Equipment
2.4 MEA Hybrid Power System
2.4.1 More-Electric Propulsion System
2.4.2 Introduction to Full Digital Management System for MEA
2.4.3 Aviation Operation Requirements and Environmental Limitations
2.5 Summary
2.6 Exercises
Chapter 3 Power Supply System of MEA
3.1 The Evolution of Power Supply System
3.1.1 Low Voltage Direct Current Aircraft Power Supply System
3.1.2 Constant Frequency AC Power Supply System
3.1.3 Variable Frequency PSS
3.1.4 Future Aircraft PSS
3.2 Introduction to Hybrid Excitation Generator
3.2.1 Mixed Excitation Brushless Aircraft Generator
3.2.2 Overview of B787 More-Electric Generator
3.3 Variable Frequency Power Supply System of MEA
3.3.1 Main Variable Frequency AC Power Supply System
3.3.2 Characteristics of APU Power Supply of Auxiliary Power Unit
3.3.3 Characteristics of Secondary Power Supply
3.3.4 Worth Research Problems
3.3.5 Main Technical Data of B787 Power Supply
3.4 Aviation Battery
3.4.1 Application Overview of Aviation Battery
3.4.2 Lithium-ion Battery
3.4.3 Whether Fuel Cell Can Be Used as Future Aviation Battery
3.5 Summary
3.6 Exercises
Chapter 4 Power Distribution System of MEA
4.1 Electricity Consumption Equipment
4.1.1 Load Classification
4.1.2 Characteristics of MEA Power Equipment
4.1.3 MEA Electric Load
4.2 Structure of MEA Power Distribution System
4.2.1 Requirements for Aircraft Power Grids
4.2.2 Power Distribution Method
4.2.3 Busbar Power Controller Unit
4.2.4 Electrical Load Management Center （ELMC）
4.2.5 Secondary Power Distribution
4.3 Example of MEA Power Distribution
4.3.1 A380 Electrical System
4.3.2 B787 Power Distribution System
……
Chapter 5 Electric Actuating Technology of MEA
Chapter 6 Environmental Control System of MEA
Chapter 7 Electrical Lighting Technology of MEA
Chapter 8 Brake System of MEA
Chapter 9 Thermal Management and Energy Optimization of MEA
Chapter 10 Common Core System of MEA
Chapter 11 Application of Power Electronics Technology of MEA
Appendix
References
1.1 Definition of MEA/AEA and Changes in Power Consumption
1.1.1 Definition of MEA/AEA
1.1.2 Changes in Electric Power Consumption
1.1.3 Advantages of MEA/AEA
1.2 Key Technologies Needed for MEA/AEA
1.3 Current Status of Advanced Aircraft Electrical Technology
1.3.1 Development Status of Aircraft Electrical Technology
1.3.2 The Foundation to Support Technology Requirements
1.4 The Development Trends for the Aircraft
1.5 Summary
1.6 Exercises
Chapter 2 Architecture of MEA/AEA
2.1 Aircraft Primary Energy and Secondary Energy
2.1.1 Aircraft Primary Energy
2.1.2 Energy Demand of Traditional Aircraft
2.2 MEA Engine
2.2.1 Summary
2.2.2 Utilization of Conventional Engine Energy
2.2.3 Energy Utilization of MEE
2.3 Benefits of Secondary Energy Unification
2.3.1 Benefits of Engine Structure Optimization
2.3.2 Simplifies the Internal Structure of the Aircraft
2.3.3 Simplified the Ground Support Equipment
2.4 MEA Hybrid Power System
2.4.1 More-Electric Propulsion System
2.4.2 Introduction to Full Digital Management System for MEA
2.4.3 Aviation Operation Requirements and Environmental Limitations
2.5 Summary
2.6 Exercises
Chapter 3 Power Supply System of MEA
3.1 The Evolution of Power Supply System
3.1.1 Low Voltage Direct Current Aircraft Power Supply System
3.1.2 Constant Frequency AC Power Supply System
3.1.3 Variable Frequency PSS
3.1.4 Future Aircraft PSS
3.2 Introduction to Hybrid Excitation Generator
3.2.1 Mixed Excitation Brushless Aircraft Generator
3.2.2 Overview of B787 More-Electric Generator
3.3 Variable Frequency Power Supply System of MEA
3.3.1 Main Variable Frequency AC Power Supply System
3.3.2 Characteristics of APU Power Supply of Auxiliary Power Unit
3.3.3 Characteristics of Secondary Power Supply
3.3.4 Worth Research Problems
3.3.5 Main Technical Data of B787 Power Supply
3.4 Aviation Battery
3.4.1 Application Overview of Aviation Battery
3.4.2 Lithium-ion Battery
3.4.3 Whether Fuel Cell Can Be Used as Future Aviation Battery
3.5 Summary
3.6 Exercises
Chapter 4 Power Distribution System of MEA
4.1 Electricity Consumption Equipment
4.1.1 Load Classification
4.1.2 Characteristics of MEA Power Equipment
4.1.3 MEA Electric Load
4.2 Structure of MEA Power Distribution System
4.2.1 Requirements for Aircraft Power Grids
4.2.2 Power Distribution Method
4.2.3 Busbar Power Controller Unit
4.2.4 Electrical Load Management Center （ELMC）
4.2.5 Secondary Power Distribution
4.3 Example of MEA Power Distribution
4.3.1 A380 Electrical System
4.3.2 B787 Power Distribution System
……
Chapter 5 Electric Actuating Technology of MEA
Chapter 6 Environmental Control System of MEA
Chapter 7 Electrical Lighting Technology of MEA
Chapter 8 Brake System of MEA
Chapter 9 Thermal Management and Energy Optimization of MEA
Chapter 10 Common Core System of MEA
Chapter 11 Application of Power Electronics Technology of MEA
Appendix
References
