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dc.contributor.authorDvoran, Filip
dc.contributor.authorČerňan, Jozef
dc.date.accessioned2020-06-30T11:26:59Z
dc.date.available2020-06-30T11:26:59Z
dc.date.issued2020
dc.identifier.isbn978-80-554-1686-1
dc.identifier.urihttp://drepo.uniza.sk/handle/hdluniza/181
dc.description.abstractThis paper aims to familiarize the reader with modifications of the engine parts of a light-sport aircraft necessary for aerial acrobatics. Modifications relating to the performance, operational capability, and resistance to the negative effects of the gravitational acceleration of acrobatic maneuvers to which the aircraft is subjected. First of all, the necessity of modification for the aircraft and its principle of operation is explained in the individual chapters. The secondary objective of the work is to introduce the design possibilities offered by manufacturing companies operating on the market, with the intention of the best product selection in the construction of acrobatic aircraft, with special requirements. The intention is to point out the factors that have to be taken into account when selecting products with their subsequent comparison in terms of technology used by the company for the best performance of the aircraft. The last chapter deals with the issue of aviation electrification, its use in aerobatic sports, and the advantages that the electric motor brings.en_US
dc.language.isosken_US
dc.publisherŽilinská univerzita v Žilineen_US
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/
dc.subjectinvert systemen_US
dc.subjectgravitational accelerationsen_US
dc.subjectengine poweren_US
dc.subjectconstruction materialen_US
dc.subjectelectric motoren_US
dc.titlePOHONNÉ JEDNOTKY AKROBATICKÝCH LIETADIELen_US
dc.title.alternativePOWERTRAIN OF AEROBATIC AIRCRAFTen_US
dc.typeBook of proceedingsen_US
dc.identifier.doihttps://doi.org/10.26552/pas.Z.2020.1.7


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