Design of fault-tolerant machine for hybrid aircraft

This project presents a study on the design of a suitable fault-tolerant electric machine for aerospace application using the JMAG program. This project mainly focuses on the electromagnetic properties of the electric machine. There are two kinds of machines presented in this paper, the flux-switchi...

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Main Author: Tan, Swee Chong
Other Authors: Christopher H. T. Lee
Format: Final Year Project
Language:English
Published: Nanyang Technological University 2021
Subjects:
Online Access:https://hdl.handle.net/10356/149715
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-1497152023-07-07T17:20:08Z Design of fault-tolerant machine for hybrid aircraft Tan, Swee Chong Christopher H. T. Lee School of Electrical and Electronic Engineering chtlee@ntu.edu.sg Engineering Engineering::Electrical and electronic engineering Engineering::Electrical and electronic engineering::Power electronics This project presents a study on the design of a suitable fault-tolerant electric machine for aerospace application using the JMAG program. This project mainly focuses on the electromagnetic properties of the electric machine. There are two kinds of machines presented in this paper, the flux-switching permanent magnet machine (FSPM) and the permanent magnet synchronous machine (PMSM). These two machines were chosen because of their ability to produce high torque density. The modular winding design is implemented on the FSPM machine while the multiple 3-phase design is implemented in the PMSM. Simulations are conducted when the machines are under healthy and faulty conditions. Through the simulation results, the FSPM machine is rejected due to the high amount of power losses during high-speed operations. The high-power loss is due to the high fundamental frequency of the FSPM machine. The PMSM on the other hand shows promising results due to its ability to provide high power with high amount of efficiency. There are two different fault-tolerant PMSM designs, one with dual 3-phase while the other with quadruple 3-phase. The quadruple 3-phase design is chosen to be the most suitable for fault tolerant aerospace application due to its added freedom of control during fault conditions as compared to the dual 3-phase design. When one or two 3-phase circuits faces a fault, they will be disconnected, and the fault will not affect the other healthy phases. The control circuit will then increase the current output of the other healthy 3-phase circuits so that the electric machine is able to continue supplying its rated power. Bachelor of Engineering (Electrical and Electronic Engineering) 2021-06-07T02:35:11Z 2021-06-07T02:35:11Z 2021 Final Year Project (FYP) Tan, S. C. (2021). Design of fault-tolerant machine for hybrid aircraft. Final Year Project (FYP), Nanyang Technological University, Singapore. https://hdl.handle.net/10356/149715 https://hdl.handle.net/10356/149715 en 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
Engineering::Electrical and electronic engineering
Engineering::Electrical and electronic engineering::Power electronics
spellingShingle Engineering
Engineering::Electrical and electronic engineering
Engineering::Electrical and electronic engineering::Power electronics
Tan, Swee Chong
Design of fault-tolerant machine for hybrid aircraft
description This project presents a study on the design of a suitable fault-tolerant electric machine for aerospace application using the JMAG program. This project mainly focuses on the electromagnetic properties of the electric machine. There are two kinds of machines presented in this paper, the flux-switching permanent magnet machine (FSPM) and the permanent magnet synchronous machine (PMSM). These two machines were chosen because of their ability to produce high torque density. The modular winding design is implemented on the FSPM machine while the multiple 3-phase design is implemented in the PMSM. Simulations are conducted when the machines are under healthy and faulty conditions. Through the simulation results, the FSPM machine is rejected due to the high amount of power losses during high-speed operations. The high-power loss is due to the high fundamental frequency of the FSPM machine. The PMSM on the other hand shows promising results due to its ability to provide high power with high amount of efficiency. There are two different fault-tolerant PMSM designs, one with dual 3-phase while the other with quadruple 3-phase. The quadruple 3-phase design is chosen to be the most suitable for fault tolerant aerospace application due to its added freedom of control during fault conditions as compared to the dual 3-phase design. When one or two 3-phase circuits faces a fault, they will be disconnected, and the fault will not affect the other healthy phases. The control circuit will then increase the current output of the other healthy 3-phase circuits so that the electric machine is able to continue supplying its rated power.
author2 Christopher H. T. Lee
author_facet Christopher H. T. Lee
Tan, Swee Chong
format Final Year Project
author Tan, Swee Chong
author_sort Tan, Swee Chong
title Design of fault-tolerant machine for hybrid aircraft
title_short Design of fault-tolerant machine for hybrid aircraft
title_full Design of fault-tolerant machine for hybrid aircraft
title_fullStr Design of fault-tolerant machine for hybrid aircraft
title_full_unstemmed Design of fault-tolerant machine for hybrid aircraft
title_sort design of fault-tolerant machine for hybrid aircraft
publisher Nanyang Technological University
publishDate 2021
url https://hdl.handle.net/10356/149715
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