Design and implementation of engine test device for the M601 engine

dc.contributor.authorPukač, Andrej
dc.contributor.authorČerňan, Jozef
dc.date.accessioned2023-11-16T13:30:00Z
dc.date.available2023-11-16T13:30:00Z
dc.date.issued2023
dc.description.abstractThe aim of this article is to create a proposal and documents for the implementation phase of the engine test device for the Walter M601 engine, which after implementation will serve as a teaching and research aid for researching new alternative fuels, testing different variants of propellers and others. As part of our work, we are dedicated to the development of two entire future test segments of device, namely the test stand and the design of the monitoring and regulation part, where we use the original devices, manufactured in compliance with LUN, which was directly designed in the past for the M601 engine and its installation in the L-410 Turbolet aircraft. The design of the test stand will include a 3D design and documentation. The monitoring part will consist of the design of the monitoring panel, which will contain selected engine indicators and LUN sensors, which will be used from the defined solutions of specific requirements and the design of electrical wiring and power sources and modules for the operation of the monitoring and regulation part.en_US
dc.identifier.doihttps://doi.org/10.26552/pas.Z.2023.2.06
dc.identifier.urihttp://drepo.uniza.sk/handle/hdluniza/973
dc.language.isoenen_US
dc.publisherUniversity of Žilinaen_US
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/
dc.subjectaircraft enginesen_US
dc.subjectaircraft engine testingen_US
dc.subjectengine monitoringen_US
dc.subjectengine regulationen_US
dc.titleDesign and implementation of engine test device for the M601 engineen_US
dc.typeConference paperen_US

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