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Please use this identifier to cite or link to this item: http://hdl.handle.net/11375/30904
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DC FieldValueLanguage
dc.contributor.advisorVeldhuis, Dr. Stephen-
dc.contributor.advisorBilgin, Dr. Berker-
dc.contributor.authorRavichandran, Sanjeev-
dc.date.accessioned2025-01-21T19:42:08Z-
dc.date.available2025-01-21T19:42:08Z-
dc.date.issued2025-
dc.identifier.urihttp://hdl.handle.net/11375/30904-
dc.description.abstractThe increasing global emphasis on reducing greenhouse gas emissions has amplified interest in the electrification of light sport aircraft, particularly for training and recreational purposes. A Switched Reluctance Motor (SRM) is a groundbreaking technology in this field, offering a cost-effective, robust, and efficient alternative to permanent magnet motors. Its straightforward design and ability to perform reliably in elevated temperatures and high-speed make it suitable for aviation applications. While there are challenges surrounding the manufacturing and assembly of SRMs, their strengths position them as a strong contender in the market. The prototype development presented in this thesis focuses primarily on the mechanical design, manufacturing, and assembly of an SRM with a stator outer diameter of 280 mm and a relatively small airgap length of 0.4 mm airgap length between rotor and stator. The proposed SRM is designed to be a direct replacement for a 70 kW Permanent Magnet Synchronous Motor (PMSM) to meet the stringent volume restrictions and operational requirements specific to an aerospace application. This research investigates manufacturing techniques of motor components, precision assembly of rotor and stator cores. Challenges including dimensional accuracy, thermal management, and proper motor component assembly are also discussed. Maintaining mechanical alignment and a small air gap is critical and essential to the motor's efficiency and functionality. This work presents the SRM as an alternative for the electrification of light sport aircraft, contributing to more sustainable aviation solutions.en_US
dc.language.isoenen_US
dc.subjectSwitched Reluctance Motoren_US
dc.subjectPrototype Developmenten_US
dc.subjectLight Sport Aircraften_US
dc.titlePrototype Development of a Light Sport Aircraft Switched Reluctance Electric Motoren_US
dc.title.alternativePROTOTYPE DEVELOPMENT OF A LIGHT SPORT AIRCRAFT SWITCHED RELUCTANCE MOTORen_US
dc.typeThesisen_US
dc.contributor.departmentMechanical Engineeringen_US
dc.description.degreetypeThesisen_US
dc.description.degreeMaster of Applied Science (MASc)en_US
dc.description.layabstractThe growing focus on reducing greenhouse gas emissions has increased interest in electrifying light sport aircraft for training and recreational purposes. This thesis explores the development of a Switched Reluctance Motor (SRM) as a cost-effective, robust, and efficient alternative to Permanent Magnet Motors for aviation applications. The SRM's simple design and reliable performance at high temperatures and speeds make it suitable for these uses. The study focuses on the mechanical design, manufacturing, and assembly of an SRM prototype with a stator outer diameter of 280 mm and a small air gap length of 0.4 mm between the rotor and stator. The SRM is designed as a direct replacement for a 70 kW Permanent Magnet Synchronous Motor, adhering to the stringent volume restrictions and operational requirements of aerospace applications. This research addresses challenges such as dimensional accuracy, thermal management, and motor component assembly, emphasizing the critical importance of maintaining mechanical alignment and a precise air gap for optimal motor performance. The work highlights the SRM's potential as a sustainable alternative for light sport aircraft electrification.en_US
Appears in Collections:Open Access Dissertations and Theses

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