Development of hybrid-excited switched reluctance motor for aerospace application
More Electric Aircrafts has been gaining traction in the recent years. As such, there is a need to investigate applicable motor drives that meet aerospace demands. Some of which includes: high power density, high fault tolerance and high availability without compromising weight, operational costs...
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| Format: | Final Year Project |
| Language: | English |
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Nanyang Technological University
2023
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| Online Access: | https://hdl.handle.net/10356/167308 |
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| Institution: | Nanyang Technological University |
| Language: | English |
| Summary: | More Electric Aircrafts has been gaining traction in the recent years. As such, there is a need to
investigate applicable motor drives that meet aerospace demands. Some of which includes: high
power density, high fault tolerance and high availability without compromising weight,
operational costs and environmental impacts. This project will focus on the working principles of
a SRM, and thereafter, moving on to a proposed PM-SRM. The main reason being that the SRM
can meet most of the aerospace demands. The drawback, however, is what makes it less
attractive than its competitors. The high torque rippling effect and high noise levels. This project
encompasses 2 main motor models that will be implemented using the JMAG Designer. Analysis
on the motor itself will be conducted to compare and evaluate the motor models. After which,
recommendations on improvements shall be made towards the proposed models of the motor and
what other relevant research gaps that can be explored to enhance the compatibility of the
proposed motor and aerospace demands |
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