Complexity, 2021 In recent years, the green aviation technology draws more attention, and more hybrid power units have been applied to the aerial vehicles. To achieve the high performance and long lifetime of components during varied working conditions, the effective ...
Zhengchao Wei +3 more
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A Probabilistic Design Methodology for a Turboshaft Engine Overall Performance Analysis
Advances in Mechanical Engineering, 2014 In reality, the cumulative effect of the many uncertainties in engine component performance may stack up to affect the engine overall performance. This paper aims to quantify the impact of uncertainty in engine component performance on the overall ...
Min Chen, Kun Zhang, Hai-Long Tang
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Design of Distributed Engine Control Systems with Uncertain Delay. [PDF]
PLoS ONE, 2016 Future gas turbine engine control systems will be based on distributed architecture, in which, the sensors and actuators will be connected to the controllers via a communication network.
Xiaofeng Liu, Yanxi Li, Xu Sun
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Intelligent Method of Identifying the Nonlinear Dynamic Model for Helicopter Turboshaft Engines [PDF]
SensorsThis research focused on the helicopter turboshaft engine dynamic model, identifying task solving in unsteady and transient modes (engine starting and acceleration) based on sensor data. It is known that about 85% of helicopter turboshaft engines operate
Serhii Vladov +8 more
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An Innovative Applied Control System of Helicopter Turboshaft Engines Based on Neuro-Fuzzy Networks [PDF]
Applied System InnovationThis study focuses on helicopter turboshaft engine innovative fault-tolerant fuzzy automatic control system development to enhance safety and efficiency in various flight modes.
Serhii Vladov +5 more
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Gas Turbine Engine Starting Applicated on TV2-117 Turboshaft
Engineering, Technology & Applied Science Research, 2017 The paper presents the examination of two different types of engine starting configurations, applicated on TV2-117A turboshaft, running into the test bench. The first type of starting configuration is a normal starting, with the engine connected to the dynamometer which controls the free turbine speed by the dynamometer load.
R. M. Catana,, Cican, G., Dediu, G.
openaire +3 more sources
Maisotsenko Cycle for Heat Recovery in Gas Turbines: A Fundamental Thermodynamic Assessment. [PDF]
Glob Chall, 2023 This paper reports the selection of optimal parameters and assessments for Innovative waste heat recovery systems using gas turbines for improved energy and exergy efficiency. The innovative systems utilize Maisotsenko's cycle‐based waste heat recovery system with enhanced humidification to exploit the maximum waste heat recovery potential of the gas ...
Tariq R, Caliskan H, Sheikh NA.
europepmc +2 more sources
Analysis of unstable mode of a free gas turbine of turbo-compressors engines [PDF]
MATEC Web of Conferences, 2021 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 ...
Hocko Marián, Al-Rabeei Samer
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Impact of dust erosion on the reduction of axial compressor efficiency of a turboshaft engine and on the stability of its operation [PDF]
MATEC Web of Conferences, 2022 This paper aimed to solve the impact of operational abrasive wear on the rotor blades of the axial compressor of the turboshaft engine on the decrease in its total compression efficiency ηCt and its transition into unstable work mode (surge).
Hocko Marián, Al-Rabeei Samer
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Control Oriented Modelling of a Turboshaft Engine for Hybrid Electric Urban Air-Mobility [PDF]
E3S Web of Conferences, 2020 The electrification of aircraft is a well-established trend in recent years in order to achieve economic and environmental sustainability. In this framework, an application particularly interesting for hybrid electric power system is represented by urban
Donateo Teresa +3 more
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