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Propulsion unit of competition model airplane
Vančo, Miroslav ; Matějů, Jiří (oponent) ; Hájek, Tomáš (vedoucí práce)
This bachelor´s thesis deals with the design and validation of the operation of the model propulsion system, according to the Aero Design East rules. The introduction is focused on rules and regulations of the competition and then, the point analysis is carried out. The research section is devoted to an overview of the propulsion system components and their basic parameters. The most appropriate configurations of the propulsion system are selected, based on calculations from the manufacturer´s datasheet. These configurations are then validated by measurements of static thrust and measurements in aerodynamic tunnel. In these measurements, the responses of the limiter for boundary power are also examined. In the last part, the choice of the propulsion system is completed.
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Design for building an electric drive into a Orlican VSO-10 Gradient glider
Vančo, Miroslav ; Juračka, Jaroslav (oponent) ; Sklenář, Filip (vedoucí práce)
This diploma thesis deals with the design of building electric propulsion (FES) into an Orličan VSO-10 Gradient glider. The introduction is focused on problem statement with main challenges of building electric propulsion into gliders. The research section is devoted to current situation on the market of gliders with overview of the propulsion systems and their basic parameters. The most appropriate configuration of the propulsion system is selected, based on performance calculations, regulations, and requirements. For final configuration, installation into the glider construction is designed, with respect to actual regulations. In the last part, cost of propulsion and installation is calculated.
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Propulsion unit of competition model airplane
Vančo, Miroslav ; Matějů, Jiří (oponent) ; Hájek, Tomáš (vedoucí práce)
This bachelor´s thesis deals with the design and validation of the operation of the model propulsion system, according to the Aero Design East rules. The introduction is focused on rules and regulations of the competition and then, the point analysis is carried out. The research section is devoted to an overview of the propulsion system components and their basic parameters. The most appropriate configurations of the propulsion system are selected, based on calculations from the manufacturer´s datasheet. These configurations are then validated by measurements of static thrust and measurements in aerodynamic tunnel. In these measurements, the responses of the limiter for boundary power are also examined. In the last part, the choice of the propulsion system is completed.
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