Design and implementation of engine test device for the M601 engine
Date
2023Publisher
University of ŽilinaLanguage
enAuthor
Pukač, Andrej
Čerňan, Jozef
Metadata
Show full item recordAbstract
The 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.
Subject
aircraft engines , aircraft engine testing , engine monitoring , engine regulationCollections
Except where otherwise noted, this item's license is described as http://creativecommons.org/licenses/by/4.0/
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