Fundamentals of Electric Aircraft

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Detalles Bibliográficos
Clasificación:Libro Electrónico
Autores principales: Thalin, Pascal (Autor), Rajamani, Ravi (Autor), Mare, Jean-Charles (Autor), Taubert, Sven (Autor)
Formato: eBook
Idioma:Inglés
Publicado: Warrendale : SAE International, 2018.
Temas:
Electric airplanes.
Electric airplanes
Acceso en línea:Texto completo
Tabla de Contenidos:
  • Cover
  • Table of contents
  • Preface
  • CHAPTER 1 Introduction and a Brief History of Electric Aircraft
  • 1.1 Background
  • 1.2 Electrification Trend
  • 1.3 Early Electric Flights
  • 1.4 The Solar Years
  • 1.5 All-Electric and Hybrid-Electric
  • 1.6 Way Forward
  • 1.7 Book Structure
  • References
  • CHAPTER 2 The Electric Aircraft Paradigm
  • 2.1 Scope and Stakes
  • 2.2 Route to Electric Aircraft
  • 2.3 Electrical Chain Breakdown
  • 2.4 Technology Stakes
  • 2.5 Conclusion
  • References
  • CHAPTER 3 Electrification of Aircraft Systems-Part I: Power Generation and Distribution, Electrical Networks and Architectures
  • 3.1 Conventional Aircraft and Engine Systems
  • 3.2 More Electric Engine (MEE) Systems
  • 3.3 More Electric Aircraft (MEA) Systems
  • 3.3.1 Electrical Power Generation and Distribution
  • References
  • CHAPTER 4 Electrification of Aircraft Systems-Part II: Replacement of Pneumatics, Enabling Technologies
  • 4.1 Pneumatic Power Generation
  • 4.2 Environmental Control System
  • 4.2.1 Conventional ECS
  • 4.2.2 Electric ECS
  • 4.3 Wing Ice Protection System
  • 4.4 Enabling Technologies
  • 4.4.1 Motors
  • 4.4.2 Power Electronics
  • 4.5 Conclusions
  • References
  • CHAPTER 5 Electrification of Aircraft Systems-Part III: Shift from Hydraulic to Electric-Powered Actuation
  • 5.1 Actuation Needs for Power Transmission and Control
  • 5.2 General Considerations for PbW Actuation
  • 5.2.1 From Power by Pipe Towards Hydraulic-Less PbW
  • 5.2.2 PbW Actuator Interface to Electric Power Networks
  • 5.2.3 Power Control in PbW Actuators
  • 5.2.4 Reliability
  • 5.2.5 Integration and Mutualization in PbW Actuation
  • 5.3 Local Generation of Hydraulic Power for Actuation
  • 5.4 Electrohydrostatic Actuators
  • 5.4.1 Functional and Architectural View
  • 5.4.2 In-Service EHAs
  • 5.4.3 Main Issues for Extensive Use of EHAs
  • 5.5 Electromechanical Actuators
  • 5.5.1 Functional and Architectural Aspects
  • 5.5.2 In-Service EMAs
  • 5.5.3 Imperfections of Technological Realization
  • 5.5.4 Maturation of EMAs
  • 5.6 Challenges with Generalization of PbW Actuation
  • 5.6.1 Important Considerations for Use of PbW Actuation
  • 5.6.2 Evolution Towards All-PbW Actuation
  • References
  • SAE- and ISO-Related Documents
  • Acronyms
  • CHAPTER 6 Propulsion Options for the Electric Aircraft
  • 6.1 Conventional Engines
  • 6.1.1 Gas Turbine
  • 6.1.2 Turboprop Engine
  • 6.1.3 Turbofan Engine
  • 6.1.4 Efficiency
  • 6.1.5 Noise
  • 6.2 Bleedless Engines for the More Electric Aircraft
  • 6.3 Propulsion Systems for the Electric Aircraft
  • 6.3.1 Enabling Architectures
  • 6.3.1.1 Electric Propulsion
  • 6.3.1.2 Hybrid-Electric Propulsion
  • 6.3.1.3 Distributed Electric Propulsion (DEP)
  • 6.3.2 Enabling Technologies
  • 6.3.2.1 Motors
  • 6.3.2.2 Motor Controls
  • 6.3.2.3 Motor and Motor Control Demonstrators

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