Design of electric motor drives with high fault-tolerant capability for aerospace applications

This thesis investigates the performance of a novel Vernier machine, the Dual Permanent Magnet Hybrid-Slot Field Twisting Vernier Machine (DPM-HSFTVM), for aerospace applications. The study focuses on improving power efficiency and reducing vibration compared to traditional motors. Simulation result...

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Main Author: Wang, Isaac Xuanyuan
Other Authors: Christopher H. T. Lee
Format: Thesis-Master by Coursework
Language:English
Published: Nanyang Technological University 2024
Subjects:
Online Access:https://hdl.handle.net/10356/181858
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-1818582024-12-27T15:46:07Z Design of electric motor drives with high fault-tolerant capability for aerospace applications Wang, Isaac Xuanyuan Christopher H. T. Lee School of Electrical and Electronic Engineering chtlee@ntu.edu.sg Engineering Electric motor Vernier machine Aerospace Power factor Fault-tolarent Hybrid stator Permanent magnet Aircraft This thesis investigates the performance of a novel Vernier machine, the Dual Permanent Magnet Hybrid-Slot Field Twisting Vernier Machine (DPM-HSFTVM), for aerospace applications. The study focuses on improving power efficiency and reducing vibration compared to traditional motors. Simulation result highlights significant improvements in efficiency and stability with the new design being 15% more efficient in terms of torque output as well as a 0.3 increase in power factor when comparing to the conventional design. These findings suggest the DPM-HSFTVM is well-suited for addressing the challenges of aerospace motor design. Master's degree 2024-12-26T11:37:34Z 2024-12-26T11:37:34Z 2024 Thesis-Master by Coursework Wang, I. X. (2024). Design of electric motor drives with high fault-tolerant capability for aerospace applications. Master's thesis, Nanyang Technological University, Singapore. https://hdl.handle.net/10356/181858 https://hdl.handle.net/10356/181858 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
Electric motor
Vernier machine
Aerospace
Power factor
Fault-tolarent
Hybrid stator
Permanent magnet
Aircraft
spellingShingle Engineering
Electric motor
Vernier machine
Aerospace
Power factor
Fault-tolarent
Hybrid stator
Permanent magnet
Aircraft
Wang, Isaac Xuanyuan
Design of electric motor drives with high fault-tolerant capability for aerospace applications
description This thesis investigates the performance of a novel Vernier machine, the Dual Permanent Magnet Hybrid-Slot Field Twisting Vernier Machine (DPM-HSFTVM), for aerospace applications. The study focuses on improving power efficiency and reducing vibration compared to traditional motors. Simulation result highlights significant improvements in efficiency and stability with the new design being 15% more efficient in terms of torque output as well as a 0.3 increase in power factor when comparing to the conventional design. These findings suggest the DPM-HSFTVM is well-suited for addressing the challenges of aerospace motor design.
author2 Christopher H. T. Lee
author_facet Christopher H. T. Lee
Wang, Isaac Xuanyuan
format Thesis-Master by Coursework
author Wang, Isaac Xuanyuan
author_sort Wang, Isaac Xuanyuan
title Design of electric motor drives with high fault-tolerant capability for aerospace applications
title_short Design of electric motor drives with high fault-tolerant capability for aerospace applications
title_full Design of electric motor drives with high fault-tolerant capability for aerospace applications
title_fullStr Design of electric motor drives with high fault-tolerant capability for aerospace applications
title_full_unstemmed Design of electric motor drives with high fault-tolerant capability for aerospace applications
title_sort design of electric motor drives with high fault-tolerant capability for aerospace applications
publisher Nanyang Technological University
publishDate 2024
url https://hdl.handle.net/10356/181858
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