DETERMINATION OF FAN DESIGN PARAMETERS FOR LIGHT-SPORT AIRCRAFT

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F22%3A00363304" target="_blank" >RIV/68407700:21220/22:00363304 - isvavai.cz</a>
Result on the web
<a href="https://doi.org/10.14311/AP.2022.62.0549" target="_blank" >https://doi.org/10.14311/AP.2022.62.0549</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.14311/AP.2022.62.0549" target="_blank" >10.14311/AP.2022.62.0549</a>

Result language
angličtina
Original language name
DETERMINATION OF FAN DESIGN PARAMETERS FOR LIGHT-SPORT AIRCRAFT
Original language description
This paper is focused on the preliminary design of an electric fan for light-sport aircraft. Usage of electric motors brings some advantages compared to piston engines, especially small size and the independence of power on shaft RPM. A 1D compressible fluid flow model is used for the determination of the performace. The influence of various system parameters is analysed. Results for the case of the UL-39 ultralight aircraft are presented. Finally, input parameters for the fan design are determined according to this analysis. This can be then used as input data for the standard fan (axial compressor) design procedure.
Czech name
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Czech description
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Type
J<sub>SC</sub> - Article in a specialist periodical, which is included in the SCOPUS database
CEP classification
—
OECD FORD branch
20304 - Aerospace engineering

Project
<a href="/en/project/FV40263" target="_blank" >FV40263: Development of high power propulsion unit of electric ducted fans with application in aircraft industry</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2022
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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