現代飛機電氣系統 周潔敏 陶思鈺 9787512444126 【台灣高等教育出版社】

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物品所在地:中國大陸
原出版社:北京航空航天大學
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書名:現代飛機電氣系統
ISBN:9787512444126
出版社:北京航空航天大學
著編譯者:周潔敏 陶思鈺
頁數:267
所在地:中國大陸 *此為代購商品
書號:1677800
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內容簡介

本書不僅主要介紹了未來先進飛機的組成、結構和工作原理,還介紹了MEA的技術特性。本書專門面向從事飛行器技術的科研人員和工程人員編寫,系統介紹了MEA/AEA的發展概況、MEA/AEA的架構、MEA的供電系統、MEA的配電系統、MEA的電驅動技術、MEA的環境控制系統、MEA的電氣照明技術、MEA的制動系統、MEA的熱管理和能源優化、MEA的公共核心系統以及MEA電力電子技術的應用等。 本書可作為從事飛機業務的學生學科發展課程的教材,也可作為科研技術人員和工程技術人員的參考書。

目錄

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
4 4 Summary
4 5 Exercises
Chapter 5 Electric Actuating Technology of MEA
5 1 Introduction
5 2 Application of Electric Actuation Technology
5 2 1 Fly-by-Wire Actuator
5 2 2 Electro-Hydraulic Actuator
5 2 3 Electric Mechanical Actuator
5 2 4 Typical Applications of Flight Control Actuators
5 2 5 Flight Control Actuation Electrical System
5 2 6 Introduction to Motor Drive Technology
5 3 Permanent Magnet Generator and Power Converter for Flight Control
5 3 1 Introduction to Rare Earth Permanent Magnet Materials
5 3 2 Permanent Magnet Generator
5 3 3 Prospect of Permanent Magnet Motor in MEA Application
5 3 4 Development of Rare Earth Permanent Magnet Motor
5 3 5 Dedicated Power Converter for Flight Control and Engine Control
5 4 Summary
5 5 Exercises
Chapter 6 Environmental Control System of MEA
6 1 High Altitude Environment
6 1 1 Atmospheric Physical Properties
6 1 2 Effects of High-Altitude Environment on Human Physiology
6 2 Electric Environmental Control System
6 2 1 Air Conditioning Syste
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