Experimental state of thrust testing of aircraft reciprocating internal combustion engine | Zendy

Matúš Mrva | Zendy; Pavol Pecho | Zendy; Michal Hrúz | Zendy; Iveta Škvareková | Zendy; Martin Bugaj | Zendy

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Experimental state of thrust testing of aircraft reciprocating internal combustion engine

Author(s) -

Matúš Mrva,

Pavol Pecho,

Michal Hrúz,

Iveta Škvareková,

Martin Bugaj

Publication year - 2020

Publication title -

aero journal/aero-journal

Language(s) - English

Resource type - Journals

eISSN - 1338-8215

pISSN - 1336-5738

DOI - 10.26552/aer.c.2020.2.3

Subject(s) - thrust , reciprocating motion , internal combustion engine , engineering , automotive engineering , aerospace engineering , jet engine , combustion , process (computing) , mechanical engineering , turbofan , engine coolant temperature sensor , combustion chamber , computer science , gas compressor , operating system , chemistry , organic chemistry

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 propel lers. 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, traini ng of aircraft mechanics and for presentation purposes of the University of Žilina.

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