System optimization demonstrator for aircraft propulsion technology using fuel cells
dc.contributor.author | Uhlár, Erik | |
dc.contributor.author | Čerňan, Jozef | |
dc.date.accessioned | 2021-06-18T10:45:17Z | |
dc.date.available | 2021-06-18T10:45:17Z | |
dc.date.issued | 2021 | |
dc.description.abstract | In order to help accelerate transition to sustainable and eco-friendly personal transportation in a single engine piston aircraft category we’ve developed a simulation software platform of hydrogen powered aircraft for further research and development. Measurements were carried out on a real reference airplane Cessna 172 R and were crosschecked with an airplane flight manual as well as a computer flight simulation. We also focused on a software-based safety and economy optimization by components usage ratio improvement and inflight energy production and transfer limitations. | en_US |
dc.identifier.doi | https://doi.org/10.26552/pas.Z.2021.1.29 | |
dc.identifier.uri | http://drepo.uniza.sk/handle/hdluniza/420 | |
dc.language.iso | sk | en_US |
dc.publisher | University of Zilina | en_US |
dc.rights.uri | http://creativecommons.org/licenses/by/4.0/ | |
dc.subject | Hydrogen fuel cell | en_US |
dc.subject | Compressed gaseous hydrogen | en_US |
dc.subject | Electric airplane propulsion | en_US |
dc.title | System optimization demonstrator for aircraft propulsion technology using fuel cells | en_US |
dc.type | Conference paper | en_US |
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