This paper analyses unstable mode of a free gas turbine of turboshaft helicopter engine TV3-117. The analysis is focused on the conditions of this phenomenon and the possibilities of its solution in a turboshaft helicopter engine and an industrial turbocharger engine with a free gas turbine. Knowing the causes of the unstable mode of operation of a free gas turbine will allow helicopter pilots to prevent accidents and increase the level of flight safety.
Analysis of unstable mode of a free gas turbine of turbo-compressors engines
2021
Aufsatz (Zeitschrift)
Elektronische Ressource
Unbekannt
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