Analysis of Helicopter Turboshaft Engines
Copyright (c) 2018 Varga Béla

This work is licensed under a Creative Commons Attribution 4.0 International License.
Abstract
Significant improvement of helicopter engines, which has embodied mainly in power weight ratio, thermal cycle efficiency, specific fuel consumption, together with reliability and maintainability, of course, has influenced the technical-tactical parameters of helicopters. This fact makes it well worth examining this field. In this paper I introduce the evolution of helicopter turboshaft engines, review the specialities of their operation, the most important producers and types. Through statistical analyses I display, what kind of performance parameters the helicopter turboshaft engines had in the past and have present days.
Keywords:
helicopter gas turbine engines
turboshaft
shaft power
specific fuel consumption
thermal efficiency
specific output network
How to Cite
[1]
B. Varga, “Analysis of Helicopter Turboshaft Engines”, RepTudKoz, vol. 30, no. 1, pp. 7–28, Apr. 2018.
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