ULTRA-LIGHT AIRCRAFTS WITH ELECTRICAL DRIVING SYSTEMS

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26220%2F10%3APU89172" target="_blank" >RIV/00216305:26220/10:PU89172 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Result language
angličtina
Original language name
ULTRA-LIGHT AIRCRAFTS WITH ELECTRICAL DRIVING SYSTEMS
Original language description
An article "Ultra-light aircrafts with electrical driving systems" deals in detail with technical parameters of developed ultra-light aircrafts prototypes with an applied electrical driving system that fully replaces the driving system of ultra-light gas-engine aircrafts. The special article primary concentrates on technical parameters and characteristics of electrical driving systems, especially on technical parameters of rotating machines that are implemented in these ultra-light aircrafts prototypes.Nowadays there are developed many ultra-light aircrafts prototypes with implemented electrical driving systems but only some of them have technical parameters that can be compared with technical parameters of ultra-light gas-engine aircrafts. If we wantto compare technical parameters of both driving systems it is necessary to analyze developed technical concepts of electrical driving systems and on basis of this analysis we can design new technical concepts. The aim of the article "Ult
Czech name
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Czech description
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Project
<a href="/en/project/GA102%2F09%2F1875" target="_blank" >GA102/09/1875: Analysis and Modelling of Low Voltage Electric Machines Parameters</a><br>
Continuities
S - Specificky vyzkum na vysokych skolach

Publication year
2010
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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