Návrh hybridnej pohonnej jednotky pre experimentálny letún Straton D7

dc.contributor.authorLongauer, Oliver
dc.contributor.authorČerňan, Jozef
dc.date.accessioned2024-11-14T12:14:13Z
dc.date.issued2024
dc.description.abstractThe aim of this article is designing hybrid power unit for the needs of experimental aircraft Straton D7. Article describes different options of hybridization of power units on basis of their architecture and the function of electric component in relation to the whole power unit. Compares different designs of automotive and aircraft solutions of hybridization of power units. After that, article offers solution for hybrid engine of Straton D7 on basis of gained theoretical knowledge, comparison of shown conceptions and basic calculations, with the needs and predispostion of the original aircraft in its best interest.
dc.identifier.doihttps://doi.org/10.26552/pas.Z.2024.1.16
dc.identifier.urihttps://drepo.uniza.sk/handle/hdluniza/1130
dc.language.isoother
dc.publisherUniversity of Žilina
dc.subjectHybrid power unit
dc.subjectdesign
dc.subject2-stroke engine
dc.subjectmild hybrid
dc.titleNávrh hybridnej pohonnej jednotky pre experimentálny letún Straton D7
dc.typeWorking Paper

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