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Turboelectric Propulsion Systems: Integrating Gas Turbines, Generators, Electrical Distribution, Power Electronics, Motors, and Propulsors for Advanced Aircraft - Couverture souple
Synopsis
A practical, aircraft-level guide to the technologies and design decisions behind advanced turboelectric propulsion. This book explains how gas turbines, high-speed generators, electrical networks, power converters, motors, thermal systems, controls, and propulsors operate as one coordinated powertrain.
Rather than treating each subsystem in isolation, the book follows the complete path from fuel energy to useful thrust. It introduces the principal series, parallel, and partial turboelectric architectures, then connects mission requirements with propulsion performance, electrical loading, mass, volume, efficiency, thermal limits, and power quality.
What the book covers
- System fundamentals: definitions, boundaries, energy-conversion paths, aircraft architectures, and propulsion trade studies.
- Mission and performance analysis: flight phases, thrust and shaft-power requirements, fuel burn, electrical load analysis, and representative aircraft power budgets.
- Prime movers and generators: turboshaft and turbofan cores, part-load behavior, transient operation, generator topologies, electromagnetic losses, insulation, bearings, and engine-generator matching.
- Distribution and power electronics: AC, DC, and variable-frequency networks, bus structures, protection, voltage selection, rectifiers, inverters, switching devices, harmonics, filters, packaging, and converter losses.
- Motors and propulsors: machine selection, torque-speed operation, field-oriented control, cooling, demagnetization limits, propeller and fan performance, blade constraints, noise, and airframe integration.
- Thermal and control systems: heat-source identification, cooling methods, heat-exchanger trade-offs, component derating, hierarchical control, load sharing, bus regulation, power limiting, and transient coordination.
- Safety and validation: functional hazard assessment, failure analysis, redundancy, high-voltage protection, arc-fault control, requirements management, simulation, hardware-in-the-loop testing, instrumentation, and integrated verification.
Designed for engineering application
Five focused examples in each chapter show how the concepts support real design work, including power-flow evaluation, aircraft power budgeting, engine-generator sizing, fault isolation, converter loss analysis, motor-drive matching, propulsor mapping, thermal balance, thrust-transient control, safety allocation, and system verification.
With its integrated treatment of propulsion, electrical engineering, aerodynamics, thermal management, control, and certification, this reference is suited to aerospace engineers, propulsion and power-system specialists, researchers, graduate students, and multidisciplinary teams developing hybrid-electric or distributed-propulsion aircraft.
Les informations fournies dans la section « Synopsis » peuvent faire référence à une autre édition de ce titre.
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Turboelectric Propulsion Systems (Paperback)
impression à la demandeVendeur : Grand Eagle Retail, Bensenville, IL, Etats-Unis
Évaluation du vendeur 5 sur 5 étoiles
Paperback. Etat : new. Paperback. A practical, aircraft-level guide to the technologies and design decisions behind advanced turboelectric propulsion. This book explains how gas turbines, high-speed generators, electrical networks, power converters, motors, thermal systems, controls, and propulsors operate as one coordinated powertrain.Rather than treating each subsystem in isolation, the book follows the complete path from fuel energy to useful thrust. It introduces the principal series, parallel, and partial turboelectric architectures, then connects mission requirements with propulsion performance, electrical loading, mass, volume, efficiency, thermal limits, and power quality.What the book coversSystem fundamentals: definitions, boundaries, energy-conversion paths, aircraft architectures, and propulsion trade studies.Mission and performance analysis: flight phases, thrust and shaft-power requirements, fuel burn, electrical load analysis, and representative aircraft power budgets.Prime movers and generators: turboshaft and turbofan cores, part-load behavior, transient operation, generator topologies, electromagnetic losses, insulation, bearings, and engine-generator matching.Distribution and power electronics: AC, DC, and variable-frequency networks, bus structures, protection, voltage selection, rectifiers, inverters, switching devices, harmonics, filters, packaging, and converter losses.Motors and propulsors: machine selection, torque-speed operation, field-oriented control, cooling, demagnetization limits, propeller and fan performance, blade constraints, noise, and airframe integration.Thermal and control systems: heat-source identification, cooling methods, heat-exchanger trade-offs, component derating, hierarchical control, load sharing, bus regulation, power limiting, and transient coordination.Safety and validation: functional hazard assessment, failure analysis, redundancy, high-voltage protection, arc-fault control, requirements management, simulation, hardware-in-the-loop testing, instrumentation, and integrated verification.Designed for engineering applicationFive focused examples in each chapter show how the concepts support real design work, including power-flow evaluation, aircraft power budgeting, engine-generator sizing, fault isolation, converter loss analysis, motor-drive matching, propulsor mapping, thermal balance, thrust-transient control, safety allocation, and system verification.With its integrated treatment of propulsion, electrical engineering, aerodynamics, thermal management, control, and certification, this reference is suited to aerospace engineers, propulsion and power-system specialists, researchers, graduate students, and multidisciplinary teams developing hybrid-electric or distributed-propulsion aircraft. This item is printed on demand. Shipping may be from multiple locations in the US or from the UK, depending on stock availability. N° de réf. du vendeur 9798171091446
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EUR 21,12
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Expédition nationale : Etats-Unis
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Turboelectric Propulsion Systems: Integrating Gas Turbines, Generators, Electrical Distribution, Power Electronics, Motors, and Propulsors for Advanced Aircraft
impression à la demandeVendeur : California Books, Miami, FL, Etats-Unis
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Etat : New. Print on Demand. N° de réf. du vendeur I-9798171091446
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Turboelectric Propulsion Systems
Vendeur : PBShop.store US, Wood Dale, IL, Etats-Unis
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PAP. Etat : New. New Book. Shipped from UK. Established seller since 2000. N° de réf. du vendeur L2-9798171091446
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Turboelectric Propulsion Systems
Vendeur : PBShop.store UK, Fairford, GLOS, Royaume-Uni
Évaluation du vendeur 5 sur 5 étoiles
PAP. Etat : New. New Book. Shipped from UK. Established seller since 2000. N° de réf. du vendeur L2-9798171091446
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Turboelectric Propulsion Systems : Integrating Gas Turbines, Generators, Electrical Distribution, Power Electronics, Motors, and Propulsors for Advanced Aircraft
Vendeur : AHA-BUCH GmbH, Einbeck, Allemagne
Évaluation du vendeur 5 sur 5 étoiles
Taschenbuch. Etat : Neu. Neuware - A practical, aircraft-level guide to the technologies and design decisions behind advanced turboelectric propulsion. This book explains how gas turbines, high-speed generators, electrical networks, power converters, motors, thermal systems, controls, and propulsors operate as one coordinated powertrain.Rather than treating each subsystem in isolation, the book follows the complete path from fuel energy to useful thrust. It introduces the principal series, parallel, and partial turboelectric architectures, then connects mission requirements with propulsion performance, electrical loading, mass, volume, efficiency, thermal limits, and power quality.What the book covers- System fundamentals: definitions, boundaries, energy-conversion paths, aircraft architectures, and propulsion trade studies.- Mission and performance analysis: flight phases, thrust and shaft-power requirements, fuel burn, electrical load analysis, and representative aircraft power budgets.- Prime movers and generators: turboshaft and turbofan cores, part-load behavior, transient operation, generator topologies, electromagnetic losses, insulation, bearings, and engine-generator matching.- Distribution and power electronics: AC, DC, and variable-frequency networks, bus structures, protection, voltage selection, rectifiers, inverters, switching devices, harmonics, filters, packaging, and converter losses.- Motors and propulsors: machine selection, torque-speed operation, field-oriented control, cooling, demagnetization limits, propeller and fan performance, blade constraints, noise, and airframe integration.- Thermal and control systems: heat-source identification, cooling methods, heat-exchanger trade-offs, component derating, hierarchical control, load sharing, bus regulation, power limiting, and transient coordination.- Safety and validation: functional hazard assessment, failure analysis, redundancy, high-voltage protection, arc-fault control, requirements management, simulation, hardware-in-the-loop testing, instrumentation, and integrated verification.Designed for engineering applicationFive focused examples in each chapter show how the concepts support real design work, including power-flow evaluation, aircraft power budgeting, engine-generator sizing, fault isolation, converter loss analysis, motor-drive matching, propulsor mapping, thermal balance, thrust-transient control, safety allocation, and system verification.With its integrated treatment of propulsion, electrical engineering, aerodynamics, thermal management, control, and certification, this reference is suited to aerospace engineers, propulsion and power-system specialists, researchers, graduate students, and multidisciplinary teams developing hybrid-electric or distributed-propulsion aircraft. N° de réf. du vendeur 9798171091446
Acheter neuf
EUR 26
Expédition à EUR 35
Expédition depuis Allemagne vers Etats-Unis
Expédition depuis Allemagne vers Etats-Unis
Quantité disponible : 2 disponible(s)
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Turboelectric Propulsion Systems (Paperback)
impression à la demandeVendeur : CitiRetail, Stevenage, Royaume-Uni
Évaluation du vendeur 5 sur 5 étoiles
Paperback. Etat : new. Paperback. A practical, aircraft-level guide to the technologies and design decisions behind advanced turboelectric propulsion. This book explains how gas turbines, high-speed generators, electrical networks, power converters, motors, thermal systems, controls, and propulsors operate as one coordinated powertrain.Rather than treating each subsystem in isolation, the book follows the complete path from fuel energy to useful thrust. It introduces the principal series, parallel, and partial turboelectric architectures, then connects mission requirements with propulsion performance, electrical loading, mass, volume, efficiency, thermal limits, and power quality.What the book coversSystem fundamentals: definitions, boundaries, energy-conversion paths, aircraft architectures, and propulsion trade studies.Mission and performance analysis: flight phases, thrust and shaft-power requirements, fuel burn, electrical load analysis, and representative aircraft power budgets.Prime movers and generators: turboshaft and turbofan cores, part-load behavior, transient operation, generator topologies, electromagnetic losses, insulation, bearings, and engine-generator matching.Distribution and power electronics: AC, DC, and variable-frequency networks, bus structures, protection, voltage selection, rectifiers, inverters, switching devices, harmonics, filters, packaging, and converter losses.Motors and propulsors: machine selection, torque-speed operation, field-oriented control, cooling, demagnetization limits, propeller and fan performance, blade constraints, noise, and airframe integration.Thermal and control systems: heat-source identification, cooling methods, heat-exchanger trade-offs, component derating, hierarchical control, load sharing, bus regulation, power limiting, and transient coordination.Safety and validation: functional hazard assessment, failure analysis, redundancy, high-voltage protection, arc-fault control, requirements management, simulation, hardware-in-the-loop testing, instrumentation, and integrated verification.Designed for engineering applicationFive focused examples in each chapter show how the concepts support real design work, including power-flow evaluation, aircraft power budgeting, engine-generator sizing, fault isolation, converter loss analysis, motor-drive matching, propulsor mapping, thermal balance, thrust-transient control, safety allocation, and system verification.With its integrated treatment of propulsion, electrical engineering, aerodynamics, thermal management, control, and certification, this reference is suited to aerospace engineers, propulsion and power-system specialists, researchers, graduate students, and multidisciplinary teams developing hybrid-electric or distributed-propulsion aircraft. This item is printed on demand. Shipping may be from our UK warehouse or from our Australian or US warehouses, depending on stock availability. N° de réf. du vendeur 9798171091446
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EUR 23,68
Expédition à EUR 43,65
Expédition depuis Royaume-Uni vers Etats-Unis
Expédition depuis Royaume-Uni vers Etats-Unis
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