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Zasnova ultralahkega vrtoplana
ID Peterman, Primož (Author), ID Kikelj, Radivoj (Mentor) More about this mentor... This link opens in a new window, ID Petrović, Igor (Co-mentor)

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Abstract
Z vpeljavo novih tehnologij v letalstvo se odpirajo možnosti novim vrstam letalnikov, ki so nekoč morda že obstajali in tudi leteli, a zaradi starejših tehnologij gradnje niso imeli ekonomskega učinka. Z vpeljavo tehnologij kompozitne gradnje, ki so že uveljavljene pri ultralahkih letalih, ter hibridnih pogonov je v nalogi predstavljena zasnova ultralahkega krilatega vrtoplana. Najprej smo podali teoretične osnove delovanja takih letalnikov in predstavili nekaj primerljivih obstoječih letalnikov. V nadaljevanju sledi zasnova in vanj vključeni postopki. Končni izdelek je prikazan s risbami CAD modelom ter tehničnimi podatki. Predstavljene so ugotovitve iz zasnove s priporočili za nadaljnje delo.

Language:Slovenian
Keywords:krilati vrtoplani, letalniki, helikopterji, žirokopterji, zasnova, hibridni pogoni
Work type:Bachelor thesis/paper
Typology:2.11 - Undergraduate Thesis
Organization:FS - Faculty of Mechanical Engineering
Place of publishing:Ljubljana
Publisher:[P. Peterman]
Year:2024
Number of pages:XXII, 68 str.
PID:20.500.12556/RUL-155507 This link opens in a new window
UDC:629.73:629.735.5:004.896(043.2)
COBISS.SI-ID:193651971 This link opens in a new window
Publication date in RUL:05.04.2024
Views:53
Downloads:14
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Secondary language

Language:English
Title:Design of an ultralight heli-gyro-plane aircraft
Abstract:
With the implementation of new technologies in the aerospace industry, options for new types of aircraft are arising. Some types of aircraft were already produced and flying but made obsolete because of older production technologies, which in turn didn’t make economic sense at the time. Based on the implementation of technologies such as composite structures (which are already well established in the ultralight aircraft category) and hybrid powertrains, an ultralight heli-gyro-plane aircraft is going to be designed. At the beginning, we presented theoretical starting points to better understand the functioning of such aircraft. We also presented some existing aircraft, on which the design is based. At the end, the final design is presented with technical data and a CAD model. Furthermore, the results of the design are presented with recommendations for further work.

Keywords:heli-gyro-plane aircraft, aircraft, rotorcraft, gyroplanes, design, hybrid propulsion

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