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Zasnova in analiza porazdeljenega, električnega,oplaščeno-propelerskega pogona jadralnega letala
ID Dobre, Bernard (Author), ID Kikelj, Radivoj (Mentor) More about this mentor... This link opens in a new window, ID Petrović, Igor (Comentor)

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Abstract
V zaključni nalogi obravnavamo zasnovo in analizo porazdeljenega električnega pogonskega sistema za jadralna letala. V uvodu predstavimo cilje, sledi pregled teoretičnih osnov pogona jadralnih letal. K teoretičnim osnovam vključimo tudi obrazložitev Penaudovega diagrama in izpeljavo enačbe inducirane hitrosti zaradi pogona. V nadaljevanju zasnujemo nosilno konstrukcijo sistema ter propelerje. Na kratko predstavimo tudi izdelavo propelerjev. V eksperimentalnem delu izdelamo preizkuševališče in izvedemo dva preizkusa. V prvem preizkusu na avtomobilu pri hitrosti letenja preizkusimo upor sistema, v drugem preizkusu pa namesto celotnega sistema preizkusimo samo potisk ene pogonske enote. Na podlagi izmerjenega potiska drugega preizkusa ugotovimo, da bi se letalo z zasnovanim sistemom lahko vzpenjalo.

Language:Slovenian
Keywords:pogonski sistem, jadralno letalo, elektromotorji, zračne zavore, analiza pogona
Work type:Bachelor thesis/paper
Typology:2.11 - Undergraduate Thesis
Organization:FS - Faculty of Mechanical Engineering
Place of publishing:Ljubljana
Publisher:[B. Dobre]
Year:2023
Number of pages:XX, 64 str.
PID:20.500.12556/RUL-148498 This link opens in a new window
UDC:629.73:629.035:621.313.13(043.2)
COBISS.SI-ID:167988995 This link opens in a new window
Publication date in RUL:25.08.2023
Views:929
Downloads:51
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Secondary language

Language:English
Title:Design and analysis of a distributed, electric,ducted propeller powerplant for a sailplane
Abstract:
In this thesis, we present the design and analysis of a distributed, electric, ducted propeller powerplant. In the introduction, we present our goals, which is followed by an overview of the theoretical foundations of sailplane propulsion, where we also include the description of Penaud diagram and derive the equation of induced velocity due to propulsion. Next, we design the support structure of the system and design and describe the production of propellers. In the empirical part, we make a test stand and then test the drag of the system on the car at the flight speed. In the second test, we only test the thrust of one propulsion unit and not of the entire system. Based on the measured thrust of the second test, we conclude that a sailplane with the designed system could climb.

Keywords:powerplant, sailplane, electric motors, air brakes, propulsion analysis

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