20.500.12556/RUL-138767 Dinamski model elise helikopterja na osnovi dinamike sistema togih teles Dynamics model of helicopter propeller blade based on rigid body system dynamics V zaključni nalogi je obravnavan dinamski model elise helikopterja in njen dinamski odziv na udarno motnjo med obratovanjem. Najprej je v nalogi predstavljen poenostavljen fizikalni model elise helikopterja, ki sestoji iz sistema togih teles, ki so povezana s torzijskimi dušilkami in vzmetmi. Sledi izpeljava gibalnih enačb, katerih sistem predstavlja numerični model obravnavanega sistema. Rezultati naloge zajemajo simulacijo vrtenja lopatice elise helikopterja in analizo odziva lopatice na udarno motnjo med obratovanjem. This work deals with dynamic model of helicopter propeller and its dynamic response to shock load during operation. First, a simplified physical model of the helicopter propeller is developed as a system of rigid bodies, connected with torsional dampers and springs. This is followed by the derivation of the equations of motion, system of which represents a numerical model of the system under consideration. Results of our work include the simulation of rotation of the helicopter propeller blade and the analysis of blade response to shock load during operation. elisa helikopterja dinamski model dinamika togih teles simulacija odziv na udarno motnjo helicopter propeller dynamic model rigid body dynamics simulation shock response true false false [G. Kokelj] Slovenski jezik Angleški jezik Zaključna naloga 2022-08-17 08:30:35 2022-08-17 08:30:42 2022-09-15 04:17:08 0000-00-00 00:00:00 2022 0 Ljubljana 0 0000-00-00 NiDoloceno NiDoloceno NiDoloceno 0000-00-00 0000-00-00 0000-00-00 519.876.5:629.735.45:539.43(043.2) 242340 118601219 15513.pdf 15513.pdf 1 9A3E7247817B9CC201C39EE8F5FDF027 180e8e0f197fcad548916709c1828ed696827f6009c73a9a0daf9cfead35cf9a 20b8c97c-1df6-11ed-92af-00155dcfd717 https://repozitorij.uni-lj.si/Dokument.php?lang=slv&id=159211 Fakulteta za strojništvo 0 0 0