Variable Pitch Propulsion Drive Model

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F61989100%3A27230%2F17%3A10236317" target="_blank" >RIV/61989100:27230/17:10236317 - isvavai.cz</a>
Result on the web
<a href="http://dx.doi.org/10.22223/tr.2017-1/2024" target="_blank" >http://dx.doi.org/10.22223/tr.2017-1/2024</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.22223/tr.2017-1/2024" target="_blank" >10.22223/tr.2017-1/2024</a>

Result language
angličtina
Original language name
Variable Pitch Propulsion Drive Model
Original language description
The contribution deals with the mathematical model of the propeller drive unit with variable pitch. The introductory part of the article aims at a general mathematical description of the internal structure of the aircraft propulsion. The DC motor and propeller model are presented in next chapter. The last part presents the comparison between MatLab Simulink model and experimental laboratory stand of variable pitch drive unit. Variable pitch propeller drive is useful to minimize power consumption. The use of these units for the drones is only experimental in terms of optimization of energy consumption.
Czech name
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Czech description
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Publication year
2017
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Name of the periodical
Sborník vědeckých prací Vysoké školy báňské - Technické univerzity Ostrava. Řada strojní
ISSN
1210-0471
e-ISSN
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Volume of the periodical
63
Issue of the periodical within the volume
1
Country of publishing house
CZ - CZECH REPUBLIC
Number of pages
6
Pages from-to
25-30
UT code for WoS article
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EID of the result in the Scopus database
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