ANALYSIS OF THE OPERATING LOAD OF THE TURBINE ENGINE DURING DECELERATION TO DASH MANEUVER
Zbigniew Czyż
z.czyz@pollub.plDepartment of Thermodynamics, Fluid Mechanics and Aviation Propulsion Systems, Lublin University of Technology, 36 Nadbystrzycka St., 20-618 Lublin, Poland (Poland)
https://orcid.org/0000-0003-2281-1149
Abstract
The article presents the analysis of the loads on the gas generator of turbine engine power of unmanned helicopter. The analysis was performed for deceleration to dash maneuver. Particular attention was paid to loads of bearing assembly in gas generator of turbine engine. The analysis was based on the timelines of changes in velocity of manned helicopter PZL W3-Falcon. The dependence of velocity changes during the flight was made as approximation by the least squares method and then determined for its change in acceleration. On this basis, the forces acting on the bearing gas generator assembly in static and dynamic conditions were determined. These values were compared with values obtained during maneuvers such as "jump up and jump down" and "acceleration and deceleration maneuver".
Keywords:
helicopter, turbine engine, gas bearings, foil-air-bearingsReferences
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Authors
Zbigniew Czyżz.czyz@pollub.pl
Department of Thermodynamics, Fluid Mechanics and Aviation Propulsion Systems, Lublin University of Technology, 36 Nadbystrzycka St., 20-618 Lublin, Poland Poland
https://orcid.org/0000-0003-2281-1149
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