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ویرایش:
نویسندگان: Pascal Thalin
سری:
ISBN (شابک) : 2023943026, 9781468606515
ناشر: SAE International
سال نشر: 2023
تعداد صفحات: 294
زبان: English
فرمت فایل : PDF (درصورت درخواست کاربر به PDF، EPUB یا AZW3 تبدیل می شود)
حجم فایل: 12 مگابایت
در صورت تبدیل فایل کتاب Fundamentals of Electric Aircraft Revised Edition (2023) [Team-IRA] به فرمت های PDF، EPUB، AZW3، MOBI و یا DJVU می توانید به پشتیبان اطلاع دهید تا فایل مورد نظر را تبدیل نمایند.
توجه داشته باشید کتاب نسخه اصلاح شده مبانی هواپیماهای الکتریکی (2023) [تیم-IRA] نسخه زبان اصلی می باشد و کتاب ترجمه شده به فارسی نمی باشد. وبسایت اینترنشنال لایبرری ارائه دهنده کتاب های زبان اصلی می باشد و هیچ گونه کتاب ترجمه شده یا نوشته شده به فارسی را ارائه نمی دهد.
Front Cover Title Page Copyright Page Contents 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 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 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 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 6.3.2.4 Materials 6.3.2.5 Superconducting Electrical Systems 6.3.2.6 Fuel Cells 6.3.2.7 Batteries 6.4 Conclusion References Chapter 7: Aircraft Applications—Part I 7.1 Battery Electric Propulsion—Small General Aviation 7.2 Urban Air Transportation 7.3 Fuel Cell Electric Propulsion—Commuter Aircraft 7.4 Battery Electric Propulsion—Regional Aircraft 7.5 Battery Electric Propulsion— Short-Range Aircraft 7.6 Electric Taxiing—Short-Range Aircraft 7.6.1 Operation 7.6.2 System Configurations and Performance 7.6.3 Nose Landing Gear Actuation 7.6.4 Main Landing Gear Actuation 7.6.5 Business Models 7.7 Conclusions References Chapter 8: Aircraft Applications—Part II 8.1 Fuel Cell Parallel HEP: Commuter Aircraft 8.2 Battery Series HEP: Commuter Aircraft 8.3 Battery Parallel HEP: Short-Range Aircraft 8.4 Battery Series HEP: Short-Range Aircraft 8.5 Battery Distributed HEP: Commuter Aircraft 8.6 Battery Distributed HEP: Regional Aircraft 8.7 Distributed HEP: Short-Range Aircraft 8.7.1 No-Battery Partial Turboelectric DHEP 8.7.2 Fuel Cell Partial Turboelectric DHEP 8.7.3 No-Battery Total Turboelectric DHEP 8.7.4 Battery Total Turboelectric DHEP 8.8 SMES Total Turboelectric DHEP: Long-Range Aircraft 8.9 Conclusions References Chapter 9: Maintainability and Operational Overview 9.1 Ground Operations 9.1.1 Maintenance—State of the Art 9.1.1.1 Maintenance Planning 9.1.1.1.1 A Check. 9.1.1.1.2 B Check. 9.1.1.1.3 C Check. 9.1.1.1.4 3C Check. 9.1.1.1.5 D Check. 9.1.1.2 Maintenance Prediction—Condition Monitoring 9.1.1.2.1 Condition-Based Maintenance (CBM) and Predictive Maintenance (PdM). 9.1.2 Changes for More Electric Aircraft 9.1.3 Changes for an Electric Aircraft 9.1.4 Airport Operations 9.1.4.1 Infrastructure 9.1.4.2 Aircraft Handling 9.1.4.3 Refueling/Recharging 9.1.4.4 Pushback/Taxiing 9.2 In-Flight Operations 9.2.1 Flight Deck Operations 9.2.1.1 Complex Configurations/Licenses 9.2.2 Single Pilot Operations 9.2.3 Autonomous Flight 9.2.4 Pilots as Drone Operators 9.2.5 Cabin Operations References Chapter 10: Performance and Business Value of Electric Aircraft 10.1 Airline Cost Structure 10.2 Aircraft Fuel Costs 10.3 Airline Fuel Efficiency 10.4 Business Aviation 10.5 Short-Range Aircraft 10.6 Long-Range Aircraft 10.7 Regional Aircraft 10.8 General Aviation 10.9 Cost of Ownership 10.10 Environmental Footprint References Conclusion Index About the Authors Back Cover