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Fundamentals of Electric Aircraft

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:
Acceso en línea:Texto completo

MARC

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100 1 |a Thalin, Pascal,  |e author. 
245 1 0 |a Fundamentals of Electric Aircraft  |c Pascal Thalin, Ravi Rajamani, Jean-Charles Mare, Sven Taubert. 
264 1 |a Warrendale :  |b SAE International,  |c 2018. 
300 |a 1 online resource 
505 0 |a 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 
505 8 |a 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 
505 8 |a 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 
505 8 |a 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 
505 8 |a 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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700 1 |a Rajamani, Ravi,  |e author. 
700 1 |a Mare, Jean-Charles,  |e author. 
700 1 |a Taubert, Sven,  |e author. 
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