Experimental state of thrust testing of aircraft reciprocating internal combustion engine
Dátum
2020Vydavateľ
University of ZilinaJazyk
enAutor
Mrva, Matúš
Pecho, Pavol
Hrúz, Michal
Škvareková, Iveta
Bugaj, Martin
Metadáta
Zobraziť celý záznamAbstrakt
The project “Experimental State of Thrust Testing of Aircraft Reciprocating Internal Combustion Engine” is aimed at creating a complex measuring device in order to obtain selected characteristics and parameters of the engine using different types of propellers. In addition to the basic measured parameters such as. thrust, temperature, speed and fuel flow will be a state of the art to test the latest prototype propellers designed for aircraft models. After its construction, the experimental state will be used as a study aid for testing various types of conventional as well as currently developed propellers, engine characteristics and teaching of the whole equipment in the process of teaching, training of aircraft mechanics and for presentation purposes of the University of Žilina.