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Please use this identifier to cite or link to this item: http://hdl.handle.net/11375/28683
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dc.contributor.advisorEmadi, Ali-
dc.contributor.authorForsyth, Alexander-
dc.date.accessioned2023-06-26T14:22:44Z-
dc.date.available2023-06-26T14:22:44Z-
dc.date.issued2023-
dc.identifier.urihttp://hdl.handle.net/11375/28683-
dc.descriptionIn reference to IEEE copyrighted material which is used with permission in this thesis, the IEEE does not endorse any of McMaster University's products or services. Internal or personal use of this material is permitted. If interested in reprinting/republishing IEEE copyrighted material for advertising or promotional purposes or for creating new collective works for resale or redistribution, please go to http://www.ieee.org/publications_standards/publications/rights/rights_link.html to learn how to obtain a License from RightsLink.en_US
dc.description.abstractThe need for reductions in global greenhouse gas emissions, coupled with rising fuel prices, has motivated intense research in the area of hybrid and fully electric crafts for commercial applications in the aviation sector. This thesis explores implementation of Halbach arrays in high-speed radial flux machines (RFMs) and low-speed axial flux machines (AFMs) for aerospace applications. Highly accurate analytical equations are developed for quickly predicting the magnetic field in the latter (both for coreless and steel core stators) due to the complex three dimensional axial flux paths which make traditional finite element analysis time-consuming. Electromagnetic design and optimization of two aerospace machines that use Halbachs are detailed. The first is a ~14 kW AFM intended to replace an existing high lift motor RFM concept in NASA’s Maxwell X57 all-electric plane. Two design variants are selected which achieve a 10 % increase in torque/power and a 10 % decrease in mass/volume, respectively. The second machine is a 20,000 RPM surface permanent magnet RFM capable of 150 kW peak power output that is intended as a proof-of-concept for the later development of a megawatt machine for a hybrid and/or all-electric aircraft.en_US
dc.language.isoenen_US
dc.subjectAxial Flux Machinesen_US
dc.subjectRadial Flux machinesen_US
dc.subjectMotorsen_US
dc.subjectGeneratorsen_US
dc.subjectHalbach Arraysen_US
dc.subjectElectric Aircraften_US
dc.subjectElectric Machine Designen_US
dc.titleUse of Halbach Arrays in Axial and Radial Flux Permanent Magnet Machines for Aerospace Applicationsen_US
dc.title.alternativeHalbach Arrays in Aerospace Axial and Radial Flux Machinesen_US
dc.typeThesisen_US
dc.contributor.departmentElectrical Engineeringen_US
dc.description.degreetypeThesisen_US
dc.description.degreeMaster of Applied Science (MASc)en_US
Appears in Collections:Open Access Dissertations and Theses

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