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Commercial aircraft hydraulic systems : Shanghai Jiao Tong University Press aerospace series /
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...
| Clasificación: | Libro Electrónico |
|---|---|
| Autores principales: | , , |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Waltham, MA :
Academic Press is an imprint of Elsevier,
[2015]
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| Colección: | Shanghai Jiao Tong University Press aerospace series
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| Temas: | |
| Acceso en línea: | Texto completo |
Tabla de Contenidos:
- Front Cover; Acknowledgement; Commercial Aircraft Hydraulic Systems; Copyright; Contents; Foreword; Preface; 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]; 1.1.1 Mission Reliability [3]; 1.1.2 Quantitative Flight Safety [4]; 1.2 THE INTERFACE BETWEEN THE FCS AND HYDRAULIC SYSTEM; 1.2.1 Aircraft Control Surfaces [6]; 1.2.1.1 Primary Flight Controls [7]; 1.2.1.2 Secondary Flight Controls [8]; 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 [6,10,13]1.3.1.1 Mechanical/Hydraulic Actuator [15,16]; 1.3.1.2 Electrical Signaled Actuator; 1.3.1.3 Multiple Redundancy Actuation System; 1.3.1.4 Mechanical Screwjack Actuator [17]; 1.3.2 The Actuation System Powered by Electrical Supply[6,18,19]; 1.3.2.1 Electrohydrostatic Actuator [6,20]; 1.3.2.2 Electromechanical Actuator [6]; 1.3.3 Commercial Aircraft Implementation; 1.3.3.1 The Flight Controls-Level Comparison [6,21,22]; 1.3.3.2 Airbus Architecture [6]; 1.3.3.3 Boeing 777 Implementation [6]
- 1.4 REQUIREMENT OF THE FCS TO THE HYDRAULIC SYSTEM [23]1.4.1 System Safety Requirements [4,24-27]; 1.4.2 Requirement of Airworthiness [14,28,29]; 1.4.2.1 Element Design [6]; 1.4.2.2 System Design [6]; 1.4.2.3 Tests [6]; 1.4.3 Actuation System Performance Criteria [31]; 1.4.3.1 Basic Data of an Actuation System; 1.4.3.2 The Static Requirements of the Hydraulic Servo Actuator [7]; 1.4.3.2.1 Stall Load; 1.4.3.2.2 Maximum Stroke; 1.4.3.2.3 Maximum Rate Capability [16]; 1.4.3.2.4 Dead Zone [6]; 1.4.3.2.5 Hysteresis; 1.4.3.2.6 Force Coupling
- 1.4.3.2.7 Mechanical Manipulating Force of the Hydraulic Actuator1.4.3.2.8 Restricted Load of the Hydraulic Actuator; 1.4.3.2.9 Maximum Load of Hydraulic Actuator; 1.4.3.3 The Dynamic Requirements of the Hydraulic Servo Actuator [7]; 1.4.3.3.1 Time Response; 1.4.3.3.2 Frequency Response; 1.4.3.3.3 Dynamic Stiffness; 1.4.3.3.4 Failure Transients [7]; 1.4.4 Actuator Modeling [7]; 1.4.5 Basic Parameters of Aircraft Hydraulic System; 1.5 CONCLUSIONS; REFERENCES; 2
- Aircraft Hydraulic Systems; 2.1 INTRODUCTION OF AIRCRAFT HYDRAULIC SYSTEMS; 2.1.1 Basic Structure of a Hydraulic System
- 2.1.1.1 Single Hydraulic System2.1.1.2 Dual-Redundant Hydraulic System; 2.1.2 Hydraulic System of the Boeing Family [6,30,32]; 2.1.2.1 Boeing 737 Hydraulic System; 2.1.2.2 Boeing 777 Hydraulic System; 2.1.3 Hydraulic System of the Airbus Family; 2.1.3.1 A320 Aircraft Hydraulic System [1,7]; 2.1.3.2 A340 Aircraft Hydraulic System [8]; 2.1.3.3 A380 Hydraulic System [1]; 2.2 BASIC PARAMETERS OF AN AIRCRAFT HYDRAULIC SYSTEM; 2.2.1 Hydraulic Fluid; 2.2.2 Hydraulic Pressure; 2.2.3 Fluid Temperature [1]; 2.2.4 Fluid Flow Rate [1]; 2.2.5 Hydraulic Pipes [1]; 2.2.6 Pressure Pulsation [1]