Please use this identifier to cite or link to this item: http://hdl.handle.net/10397/115435
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dc.contributorDepartment of Electrical and Electronic Engineeringen_US
dc.contributorResearch Centre for Electric Vehiclesen_US
dc.creatorChow, CCTen_US
dc.creatorLubin, Ten_US
dc.creatorAinslie, MDen_US
dc.creatorLee, CHTen_US
dc.creatorChau, KTen_US
dc.date.accessioned2025-09-25T07:06:57Z-
dc.date.available2025-09-25T07:06:57Z-
dc.identifier.urihttp://hdl.handle.net/10397/115435-
dc.language.isoenen_US
dc.publisherInstitute of Electrical and Electronics Engineersen_US
dc.rights© 2025 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works.en_US
dc.rightsThe following publication C. C. T. Chow, T. Lubin, M. D. Ainslie, C. H. T. Lee and K. T. Chau, "Analysis and Optimization of Permanent Magnet and DC-Excited Ironless Superconducting Synchronous Machines for Electric Aircraft," in IEEE Transactions on Transportation Electrification, vol. 11, no. 5, pp. 12596-12607, Oct. 2025 is available at https://doi.org/10.1109/TTE.2025.3592478.en_US
dc.subjectAc lossen_US
dc.subjectElectric aircraften_US
dc.subjectMgB₂en_US
dc.subjectSubdomain modellingen_US
dc.subjectSuperconducting electrical machinesen_US
dc.titleAnalysis and optimization of permanent magnet and dc-excited ironless superconducting synchronous machines for electric aircraften_US
dc.typeJournal/Magazine Articleen_US
dc.identifier.spage12596en_US
dc.identifier.epage12607en_US
dc.identifier.volume11en_US
dc.identifier.issue5en_US
dc.identifier.doi10.1109/TTE.2025.3592478en_US
dcterms.abstractSuperconducting motors have high power densities and thus have a high potential to be used for the propulsion of large electric aircraft. However, superconductors also dissipate ac loss when they are subject to a time-varying magnetic field or when they are carrying ac current. Refining an analytical machine evaluation model in the literature, this paper provides a fast analytical model that incorporates new ac loss formulae to model machines with a superconducting MgB2 armature, and rotor excitation via either permanent magnets (PMs) or superconducting coils. Machines with and without an iron yoke are modeled. In addition, the machine models are used in multiobjective optimization to explore the trade-off between minimizing the active mass and minimizing the armature ac loss, using the optimization package 'pymoo' in Python. The machines are rated at 3 MW, 4,500 rpm, based on NASA's N3-X concept aircraft. Results suggest that the lighter, yokeless machines do not have much higher armature ac loss than the machines with yoke (difference less than 0.1% of machine power), which may be contrary to expectation.en_US
dcterms.accessRightsopen accessen_US
dcterms.bibliographicCitationIEEE transactions on transportation electrification, Oct. 2025, v. 11, no. 5, p. 12596-12607en_US
dcterms.isPartOfIEEE transactions on transportation electrificationen_US
dcterms.issued2025-10-
dc.identifier.scopus2-s2.0-105011710042-
dc.identifier.eissn2332-7782en_US
dc.description.validate202509 bcelen_US
dc.description.oaAccepted Manuscripten_US
dc.identifier.SubFormIDG000157/2025-08-
dc.description.fundingSourceRGCen_US
dc.description.fundingSourceOthersen_US
dc.description.fundingTextThis work was supported in part by Hong Kong Research Grants Council under Project 17204021; and in part by Hong Kong Polytechnic University, Hong Kong Special Administrative Region, China, under Project P0048560 and Project P0046563.en_US
dc.description.pubStatusPublisheden_US
dc.description.oaCategoryGreen (AAM)en_US
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