Development of power converter for aerospace applications

More Electrical Aircraft (MEA) are becoming increasingly popular, as they offer a number of advantages over traditional aircraft, such as reduced weight, improved fuel efficiency, and lower emissions. Hybrid electric aircraft (HEA) are a type of MEA that use both electric and conventional engines to...

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Main Author: Tan, Melvin Yu Fei
Other Authors: Josep Pou
Format: Final Year Project
Language:English
Published: Nanyang Technological University 2023
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Online Access:https://hdl.handle.net/10356/172757
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-1727572023-12-22T15:44:03Z Development of power converter for aerospace applications Tan, Melvin Yu Fei Josep Pou School of Electrical and Electronic Engineering Rolls-Royce@NTU Corporate Lab j.pou@ntu.edu.sg Engineering::Electrical and electronic engineering::Electronic systems More Electrical Aircraft (MEA) are becoming increasingly popular, as they offer a number of advantages over traditional aircraft, such as reduced weight, improved fuel efficiency, and lower emissions. Hybrid electric aircraft (HEA) are a type of MEA that use both electric and conventional engines to generate power. This allows for a more flexible and efficient use of energy, and can lead to significant reductions in fuel consumption and emissions. One of the key challenges in designing HEA is the optimization of the power chain. The power chain includes all of the components that are involved in converting engine power into electrical power, and then converting that electrical power back into mechanical propulsion power. The optimization of the power chain is critical in terms of reducing weight and improving reliability. This project aims to focus on the power chain of MEA, including the shaft-rectifier-generator-inverter-motor system. The project will explore both component level and system level solutions to optimize the power chain for weight and reliability. Development of new materials and designs for generators, inverters, and motors that are lighter and more efficient. Development of new control algorithms for power electronics components that improve efficiency and reliability. Development of new system architectures for power chains that are more efficient and reliable. Integration of the power chain with other aircraft systems, such as the flight control system and the energy management system. Development of new tools and methodologies for the design and optimization of power chains. The project is expected to make significant contributions to the field of MEA design, and to help accelerate the commercialization of MEA technology. Bachelor of Engineering (Electrical and Electronic Engineering) 2023-12-19T23:39:40Z 2023-12-19T23:39:40Z 2023 Final Year Project (FYP) Tan, M. Y. F. (2023). Development of power converter for aerospace applications. Final Year Project (FYP), Nanyang Technological University, Singapore. https://hdl.handle.net/10356/172757 https://hdl.handle.net/10356/172757 en B1190-222 application/pdf Nanyang Technological University
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic Engineering::Electrical and electronic engineering::Electronic systems
spellingShingle Engineering::Electrical and electronic engineering::Electronic systems
Tan, Melvin Yu Fei
Development of power converter for aerospace applications
description More Electrical Aircraft (MEA) are becoming increasingly popular, as they offer a number of advantages over traditional aircraft, such as reduced weight, improved fuel efficiency, and lower emissions. Hybrid electric aircraft (HEA) are a type of MEA that use both electric and conventional engines to generate power. This allows for a more flexible and efficient use of energy, and can lead to significant reductions in fuel consumption and emissions. One of the key challenges in designing HEA is the optimization of the power chain. The power chain includes all of the components that are involved in converting engine power into electrical power, and then converting that electrical power back into mechanical propulsion power. The optimization of the power chain is critical in terms of reducing weight and improving reliability. This project aims to focus on the power chain of MEA, including the shaft-rectifier-generator-inverter-motor system. The project will explore both component level and system level solutions to optimize the power chain for weight and reliability. Development of new materials and designs for generators, inverters, and motors that are lighter and more efficient. Development of new control algorithms for power electronics components that improve efficiency and reliability. Development of new system architectures for power chains that are more efficient and reliable. Integration of the power chain with other aircraft systems, such as the flight control system and the energy management system. Development of new tools and methodologies for the design and optimization of power chains. The project is expected to make significant contributions to the field of MEA design, and to help accelerate the commercialization of MEA technology.
author2 Josep Pou
author_facet Josep Pou
Tan, Melvin Yu Fei
format Final Year Project
author Tan, Melvin Yu Fei
author_sort Tan, Melvin Yu Fei
title Development of power converter for aerospace applications
title_short Development of power converter for aerospace applications
title_full Development of power converter for aerospace applications
title_fullStr Development of power converter for aerospace applications
title_full_unstemmed Development of power converter for aerospace applications
title_sort development of power converter for aerospace applications
publisher Nanyang Technological University
publishDate 2023
url https://hdl.handle.net/10356/172757
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