王少萍、唐邁達、劉紅*的《民機液壓系統(tǒng)》是 **本與飛機飛行控制系統(tǒng)相關的民用飛機液壓系統(tǒng)設計、分析和評價的*作，重點講述與飛機飛行控制系統(tǒng)相關的液壓系統(tǒng)工作原理，包括飛機液壓能源系統(tǒng)和作動系統(tǒng)，以及一些新型的飛機電液能源與作動系統(tǒng)新體系結構及相關部件，如2H／2E結構和電靜液作動器(EHA)。本書覆蓋民用飛機液壓系統(tǒng)的*新研究進展和新技術。它還包括相關基礎理論、設計方法和實際實施和應用，是一本既注重理論又面向實際應用的書籍。
本書可供從事飛機液壓系統(tǒng)研究的工程技術人員使用，也可供高校相關專業(yè)的學生參考使用。
Chapter 1 Requirements for the Hydraulic System of a Flight Control System
1.1 The Development of the Hydraulic System Related to the Flight Control
System
1.1.1 Mission Reliability
1.1.2 Quantitative Flight Safety
1.2 The Interface between the FCS and Hydraulic System
1.2.1 Aircraft Control Surfaces
1.2.2 Interface between Flight Controls and Hydraulic Systems
1.3 Actuation Systems
1.3.1 The Actuation System Powered by Centralized Hydraulic
Supply
1.3.2 The Actuation System Powered by Electrical Supply
1.3.3 Commercial Aircraft Implementation
1.4 Requirement of the FCS to the Hydraulic System
1.4.1 System Safety Requirements
1.4.2 Requirement of Airworthiness
1.4.3 Actuation System Performance Criteria
1.4.4 Actuator Modeling
1.4.5 Basic Parameters of Aircraft Hydraulic System
1.5 Conclusions
References
Chapter 2 Aircraft Hydraulic Systems
2.1 Introduction of Aircraft Hydraulic Systems
2.1. l Basic Structure of a Hydraulic System
2.1.2 Hydraulic System of the Boeing Family
2.1.3 Hydraulic System of the Airbus Family
2.2 Basic Parameters of an Aircraft Hydraulic System 73
2.2.1 Hydraulic Fluid
2.2.2 Hydraulic Pressure
2.2.3 Fluid Temperature
2.2.4 Fluid Flow Rate
2.2.5 Hydraulic Pipes
2.2.6 Pressure Pulsation
2.3 Main Components of the Aircraft Hydraulic System
2.3 1 Aircraft Hydraulic Pump
2.3 2 Power Transfer Unit
2.3 3 Priority Valves
2.3 4 Control Valves
2.3 5 Check Valve
2.3 6 Hydraulic Accumulator
2.3 7 Hydraulic Filter
2.3.8 Hydraulic Reservoir
2.3.9 Fluid Cooling System
2.3.10 Hydraulic Actuator
2.3.11 Redundant HAs
2.4 Proof Test
2.5 Conclusions ]17
References
Chapter 3 Comprehensive Reliability Design of Aircraft Hydraulic System
3.1 Quality and Reliability
3.2 Comprehensive Reliability
3.2.1 Development of Aircraft-related Reliability
3.2.2 Definition of Comprehensive Reliability
3.3 Comprehensive Reliability Theory
3.3.1 Reliability Theory of a Nonrepairable System
3.3.2 Reliability Theory of a Repairable System
3.3.3 Conventional Probability Density Function
3.4 Reliability Design of a Hydraulic System
3.4.1 Reliability Design of Electrical Components
3.4.2 Reliability Design of a Mechanical Product
3.4.3 System Reliability Design
3.5 Design for Maintainability
3.6 Safety Assessment Methods
3.6.1 Failure Modes, Effects, and Criticality Analysis
3.6.2 Fault Tree Analysis
3.6.3 Markov Analysis
3.6.4 Common Cause Analysis
3.7 Comprehensive Reliability Evaluation of a Hydraulic System
3.7.1 Reliability Evaluation of Hydraulic Power Supply System
3.7.2 Safety Requirements and Performance Requirements
of the Actuator
3.7.3 Reliability Evaluation of the Hydraulic Actuation System
3.8 Conclusions
References
Chapter 4 New Technology of Aircraft Hydraulic System
4.1 Introduction
4.2 High-Pressure, High-Power Hydraulic Aircraft Power Supply
Systems
4.2.1 Introduction of High Pressure
4.2.2 High Power
4.2.3 The Problem of High-Pressure Hydraulic Systems
4.3 Intelligent Hydraulic Power Supply System
4.3.1 The Requirement of an Intelligent Control Pump
4.3.2 The Structure of an Intelligent Variable Pump
4.3.3 Information Interaction Analysis of an Intelligent Control
Pump
4.3.4 Control of Intelligent Pump
4.4 New Architecture Based on 2H/2E
4.4.1 EHA Principle
4.4.2 EBHA Principle
4.4.3 Dissimilar Redundant Hybrid Actuation System
4.4.4 Electromechanical Principle
4.5 Prognostics and Health Management of Hydraulic Systems
4.5.1 Development of PHM
4.5.2 PHM Structure
4.5.3 PHM Information Acquisition and Fault Feature
Extraction
4.5.4 PHM Hierarchical Intelligent Fault Diagnosis Algorithm
4.5.5 PHM Fault Prediction
4.5.6 Maintenance of PHM
4.5.7 PHM Evaluation
References
Abbreviations
Index
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