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Commercial Aircraft Hydraulic Systems: Shanghai Jiao Tong University Press Aerospace Series [Hardback]

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(Professor, School of Automation Science and Electrical Engineering, Beihang University, Beijing, China), (Professor, Department of Engineering and Technology, Old Dominion University, VA, USA), (AVIC The First Aircraft Institute)
  • Formāts: Hardback, 276 pages, height x width: 229x152 mm, weight: 610 g, 80 illustrations (20 in full color); Illustrations, unspecified
  • Sērija : Aerospace Engineering
  • Izdošanas datums: 15-Oct-2015
  • Izdevniecība: Academic Press Inc
  • ISBN-10: 0124199720
  • ISBN-13: 9780124199729
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Commercial Aircraft Hydraulic Systems: Shanghai Jiao Tong University Press Aerospace SeriesPalielināt
  • Formāts: Hardback, 276 pages, height x width: 229x152 mm, weight: 610 g, 80 illustrations (20 in full color); Illustrations, unspecified
  • Sērija : Aerospace Engineering
  • Izdošanas datums: 15-Oct-2015
  • Izdevniecība: Academic Press Inc
  • ISBN-10: 0124199720
  • ISBN-13: 9780124199729
Citas grāmatas par šo tēmu:
Permanent link: https://www.kriso.lv/db/9780124199729.html
Keywords:

Commercial Aircraft Hydraulic Systems: Shanghai Jiao Tong University Press Aerospace Series focuses on the operational principles and design technology of aircraft hydraulic systems, including the hydraulic power supply and actuation system and describing new types of structures and components such as the 2H/2E structure design method and the use of electro hydrostatic actuators (EHAs).

Based on the commercial aircraft hydraulic system, this is the first textbook that describes the whole lifecycle of integrated design, analysis, and assessment methods and technologies, enabling readers to tackle challenging high-pressure and high-power hydraulic system problems in university research and industrial contexts.

Commercial Aircraft Hydraulic Systems is the latest in a series published by the Shanghai Jiao Tong University Press Aerospace Series that covers the latest advances in research and development in aerospace. Its scope includes theoretical studies, design methods, and real-world implementations and applications. The readership for the series is broad, reflecting the wide range of aerospace interest and application. Titles within the series include Reliability Analysis of Dynamic Systems, Wake Vortex Control, Aeroacoustics: Fundamentals and Applications in Aeropropulsion Systems, Computational Intelligence in Aerospace Engineering, and Unsteady Flow and Aeroelasticity in Turbomachinery.

  • Presents the first book to describe the interface between the hydraulic system and the flight control system in commercial aircraft
  • Focuses on the operational principles and design technology of aircraft hydraulic systems, including the hydraulic power supply and actuation system
  • Includes the most advanced methods and technologies of hydraulic systems
  • Describes the interaction between hydraulic systems and other disciplines

Papildus informācija

This book focuses on the operational principles and design technology of aircraft hydraulic systems, including the hydraulic power supply and actuation system and a description of the new types of structures and components such as the 2H/2E structure design method and the use of electro hydrostatic actuators (EHAs), amongst other topics.
Foreword ix
Preface xi
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(7)
1.1.1 Mission Reliability
6(1)
1.1.2 Quantitative Flight Safety
7(1)
1.2 The Interface between the FCS and Hydraulic System
8(5)
1.2.1 Aircraft Control Surfaces
8(3)
1.2.2 Interface between Flight Controls and Hydraulic Systems
11(2)
1.3 Actuation Systems
13(20)
1.3.1 The Actuation System Powered by Centralized Hydraulic Supply
14(10)
1.3.2 The Actuation System Powered by Electrical Supply
24(3)
1.3.3 Commercial Aircraft Implementation
27(6)
1.4 Requirement of the FCS to the Hydraulic System
33(17)
1.4.1 System Safety Requirements
34(2)
1.4.2 Requirement of Airworthiness
36(2)
1.4.3 Actuation System Performance Criteria
38(8)
1.4.4 Actuator Modeling
46(2)
1.4.5 Basic Parameters of Aircraft Hydraulic System
48(2)
1.5 Conclusions
50(3)
References
51(2)
2 Aircraft Hydraulic Systems
2.1 Introduction of Aircraft Hydraulic Systems
53(16)
2.1.1 Basic Structure of a Hydraulic System
55(5)
2.1.2 Hydraulic System of the Boeing Family
60(2)
2.1.3 Hydraulic System of the Airbus Family
62(7)
2.2 Basic Parameters of an Aircraft Hydraulic System
69(3)
2.2.1 Hydraulic Fluid
69(1)
2.2.2 Hydraulic Pressure
70(1)
2.2.3 Fluid Temperature
71(1)
2.2.4 Fluid Flow Rate
71(1)
2.2.5 Hydraulic Pipes
72(1)
2.2.6 Pressure Pulsation
72(1)
2.3 Main Components of the Aircraft Hydraulic System
72(39)
2.3.1 Aircraft Hydraulic Pump
72(11)
2.3.2 Power Transfer Unit
83(4)
2.3.3 Priority Valves
87(1)
2.3.4 Control Valves
88(1)
2.3.5 Check Valve
89(1)
2.3.6 Hydraulic Accumulator
90(2)
2.3.7 Hydraulic Filter
92(1)
2.3.8 Hydraulic Reservoir
93(1)
2.3.9 Fluid Cooling System
94(1)
2.3.10 Hydraulic Actuator
95(13)
2.3.11 Redundant HAs
108(3)
2.4 Proof Test
111(1)
2.5 Conclusions
112(3)
References
112(3)
3 Comprehensive Reliability Design of Aircraft Hydraulic System
3.1 Quality and Reliability
115(1)
3.2 Comprehensive Reliability
116(2)
3.2.1 Development of Aircraft-related Reliability
116(1)
3.2.2 Definition of Comprehensive Reliability
117(1)
3.3 Comprehensive Reliability Theory
118(8)
3.3.1 Reliability Theory of a Nonrepairable System
118(4)
3.3.2 Reliability Theory of a Repairable System
122(1)
3.3.3 Conventional Probability Density Function
123(3)
3.4 Reliability Design of a Hydraulic System
126(19)
3.4.1 Reliability Design of Electrical Components
127(2)
3.4.2 Reliability Design of a Mechanical Product
129(9)
3.4.3 System Reliability Design
138(7)
3.5 Design for Maintainability
145(5)
3.6 Safety Assessment Methods
150(6)
3.6.1 Failure Modes, Effects, and Criticality Analysis
150(1)
3.6.2 Fault Tree Analysis
151(4)
3.6.3 Markov Analysis
155(1)
3.6.4 Common Cause Analysis
156(1)
3.7 Comprehensive Reliability Evaluation of a Hydraulic System
156(12)
3.7.1 Reliability Evaluation of Hydraulic Power Supply System
156(2)
3.7.2 Safety Requirements and Performance Requirements of the Actuator
158(1)
3.7.3 Reliability Evaluation of the Hydraulic Actuation System
159(9)
3.8 Conclusions
168(3)
References
168(3)
4 New Technology of Aircraft Hydraulic System
4.1 Introduction
171(1)
4.2 High-Pressure, High-Power Hydraulic Aircraft Power Supply Systems
172(9)
4.2.1 Introduction of High Pressure
172(3)
4.2.2 High Power
175(1)
4.2.3 The Problem of High-Pressure Hydraulic Systems
175(6)
4.3 Intelligent Hydraulic Power Supply System
181(16)
4.3.1 The Requirement of an Intelligent Control Pump
183(5)
4.3.2 The Structure of an Intelligent Variable Pump
188(2)
4.3.3 Information Interaction Analysis of an Intelligent Control Pump
190(2)
4.3.4 Control of Intelligent Pump
192(5)
4.4 New Architecture Based on 2H/2E
197(18)
4.4.1 EHA Principle
200(8)
4.4.2 EBHA Principle
208(3)
4.4.3 Dissimilar Redundant Hybrid Actuation System
211(1)
4.4.4 Electromechanical Principle
212(3)
4.5 Prognostics and Health Management of Hydraulic Systems
215(38)
4.5.1 Development of PHM
215(2)
4.5.2 PHM Structure
217(2)
4.5.3 PHM Information Acquisition and Fault Feature Extraction
219(1)
4.5.4 PHM Hierarchical Intelligent Fault Diagnosis Algorithm
220(20)
4.5.5 PHM Fault Prediction
240(5)
4.5.6 Maintenance of PHM
245(1)
4.5.7 PHM Evaluation
246(2)
References
248(5)
Abbreviations 253(2)
Notation and Symbols 255(4)
Index 259
With more than 20 years of research experience in hydraulic system and reliability of aircraft, Professor Wang currently leads the Reliability Society in Operation Society of China. Her work is supported by the National Natural Science Foundation of China, Ministry of Science and Technology and the industry. Professor Tomivic worked as vice director of American Foundry Society, American Society of Mechanical Engineering and American Society of Engineering Education and has 25 years experience on product lifecycle management Hong Liu is the researcher of AVIC The First Aircraft Institute, Xi'an. Her research interests include aircraft hydraulic system design, system safety and reliability design, system integrated control and management , hydraulic system test.