Research and Realization of High-Power Medium-Voltage Active Rectifier Concepts for Future Hybrid-Electric Aircraft Generation

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dc.contributor.authorTrentin, Andrew
dc.contributor.authorSala, Giacomo
dc.contributor.authorTarisciotti, Luca
dc.contributor.authorGalassini, Alessandro
dc.contributor.authorDegano, Michele
dc.contributor.authorConnor, Peter H.
dc.contributor.authorGolovanov, Dmitry
dc.contributor.authorGerada, David
dc.contributor.authorXu, Zeyuan
dc.contributor.authorLa Rocca, Antonino
dc.contributor.authorEastwick, Carol N.
dc.contributor.authorPickering, Stephen J.
dc.contributor.authorWheeler, Patrick
dc.contributor.authorClare, Jon C.
dc.contributor.authorGerada, Chris
dc.date.accessioned2025-03-10T15:22:36Z
dc.date.available2025-03-10T15:22:36Z
dc.date.issued2021-12
dc.descriptionIndexación: Scopus.
dc.description.abstractIn this article, we describe the research and development of a 3 kV active rectifier for a 4 MW aerospace generator drive system demonstrator. The converter is fed by a multiphase high-speed/high-frequency permanent magnet generator. The main aim of the work is to demonstrate for the first time the feasibility of an MW-class generator system meeting future hybrid-electric propulsion requirements. A concept with multiple and isolated three-phase systems feeding different power buses is proposed to meet the availability requirements. Multiple converters (one for each three-phase system) are connected in series and/or in parallel to achieve the rated power and dc-link voltage. This article describes the key design concepts and the development and testing of the converter to meet the challenging application requirements. Reduced power tests are carried out on a full-scale 4 MW converter prototype, validating the proposed design. The work represents a step forward in terms of voltage, power, and output frequency with respect to the state-of-the-art. © 1982-2012 IEEE.
dc.description.urihttps://ieeexplore-ieee-org.recursosbiblioteca.unab.cl/document/9280429
dc.identifier.citationIEEE Transactions on Industrial Electronics, Volume 68, Issue 12, Pages 11684 - 11695, December 2021, Article number 9280429
dc.identifier.doi10.1109/TIE.2020.3040692
dc.identifier.issn0278-0046
dc.identifier.urihttps://repositorio.unab.cl/handle/ria/63705
dc.language.isoen
dc.publisherInstitute of Electrical and Electronics Engineers Inc.
dc.rights.licenseAtribución/Reconocimiento 4.0 Internacional CC BY 4.0 Deed
dc.rights.urihttps://creativecommons.org/licenses/by/4.0/deed.es
dc.subjectAerospace generation drives
dc.subjectHigh-power generation systems
dc.subjectHigh-power high-voltage converter design
dc.subjectHybrid-electric aircraft
dc.subjectMultiphase drives
dc.subjectVariable speed drives
dc.titleResearch and Realization of High-Power Medium-Voltage Active Rectifier Concepts for Future Hybrid-Electric Aircraft Generation
dc.typeArtículo
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