A fault-tolerant electric motor for more electric aircraft
The growing momentum in the aircraft industry toward the idea of a hybrid electric-powered or more electric aircraft (MEA), and eventually an all-electric aircraft, exemplifies the industry's efforts to improve aircraft performance, lower operating and maintenance costs, boost dispatch reliabil...
Saved in:
Main Author: | |
---|---|
Other Authors: | |
Format: | Final Year Project |
Language: | English |
Published: |
Nanyang Technological University
2023
|
Subjects: | |
Online Access: | https://hdl.handle.net/10356/167131 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Nanyang Technological University |
Language: | English |
id |
sg-ntu-dr.10356-167131 |
---|---|
record_format |
dspace |
spelling |
sg-ntu-dr.10356-1671312023-07-07T17:49:48Z A fault-tolerant electric motor for more electric aircraft Lim, Sebastin Choon Huat Christopher H. T. Lee School of Electrical and Electronic Engineering chtlee@ntu.edu.sg Engineering::Electrical and electronic engineering The growing momentum in the aircraft industry toward the idea of a hybrid electric-powered or more electric aircraft (MEA), and eventually an all-electric aircraft, exemplifies the industry's efforts to improve aircraft performance, lower operating and maintenance costs, boost dispatch reliability, and lower gas emissions. The MEA idea, in particular, calls for the use of electricity for all non-propulsive devices. Traditionally, various auxiliary power sources, including hydraulic, pneumatic, mechanical, and electrical, are used to drive these non-propulsive devices. These motors must have a wide range of operating speeds in addition to high efficiency, compactness, and torque density properties. Without the employment of rare-earth permanent magnets, these requirements have not yet been met. This paper demonstrated that it is possible to create a switched reluctance motor that is competitive with rare-earth permanent-magnet motors. Experiments revealed that the designed motor outperforms ordinary rare-earth permanent-magnet motors in terms of efficiency, torque density, and range of working speeds. Bachelor of Engineering (Electrical and Electronic Engineering) 2023-05-23T02:53:39Z 2023-05-23T02:53:39Z 2023 Final Year Project (FYP) Lim, S. C. H. (2023). A fault-tolerant electric motor for more electric aircraft. Final Year Project (FYP), Nanyang Technological University, Singapore. https://hdl.handle.net/10356/167131 https://hdl.handle.net/10356/167131 en P1036-212 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 |
spellingShingle |
Engineering::Electrical and electronic engineering Lim, Sebastin Choon Huat A fault-tolerant electric motor for more electric aircraft |
description |
The growing momentum in the aircraft industry toward the idea of a hybrid electric-powered or more electric aircraft (MEA), and eventually an all-electric aircraft, exemplifies the industry's efforts to improve aircraft performance, lower operating and maintenance costs, boost dispatch reliability, and lower gas emissions. The MEA idea, in particular, calls for the use of electricity for all non-propulsive devices. Traditionally, various auxiliary power sources, including hydraulic, pneumatic, mechanical, and electrical, are used to drive these non-propulsive devices. These motors must have a wide range of operating speeds in addition to high efficiency, compactness, and torque density properties. Without the employment of rare-earth permanent magnets, these requirements have not yet been met. This paper demonstrated that it is possible to create a switched reluctance motor that is competitive with rare-earth permanent-magnet motors. Experiments revealed that the designed motor outperforms ordinary rare-earth permanent-magnet motors in terms of efficiency, torque density, and range of working speeds. |
author2 |
Christopher H. T. Lee |
author_facet |
Christopher H. T. Lee Lim, Sebastin Choon Huat |
format |
Final Year Project |
author |
Lim, Sebastin Choon Huat |
author_sort |
Lim, Sebastin Choon Huat |
title |
A fault-tolerant electric motor for more electric aircraft |
title_short |
A fault-tolerant electric motor for more electric aircraft |
title_full |
A fault-tolerant electric motor for more electric aircraft |
title_fullStr |
A fault-tolerant electric motor for more electric aircraft |
title_full_unstemmed |
A fault-tolerant electric motor for more electric aircraft |
title_sort |
fault-tolerant electric motor for more electric aircraft |
publisher |
Nanyang Technological University |
publishDate |
2023 |
url |
https://hdl.handle.net/10356/167131 |
_version_ |
1772827586057994240 |