Results 1 to 10 of about 44,071 (209)

Neural Network Signal Integration from Thermogas-Dynamic Parameter Sensors for Helicopters Turboshaft Engines at Flight Operation Conditions [PDF]

open access: yesSensors
The article’s main provisions are the development and application of a neural network method for helicopter turboshaft engine thermogas-dynamic parameter integrating signals.
Serhii Vladov   +6 more
doaj   +2 more sources

CFD-enabled sustainable design and manufacturing of cooling fan for unmanned helicopter [PDF]

open access: yesScientific Reports
Due to the demand of unmanned helicopters for drag reduction and rain-proof, the helicopter nacelle must be sealed. It will lead to a decrease in the heat transfer efficiency of the radiator, and the output power of the engine will drop dramatically. The
Liang Si   +10 more
doaj   +2 more sources

Comparative Study of Helicopter Engine Particle Separators [PDF]

open access: yesJournal of Aircraft, 2014
Particle separators are fitted to helicopter engine intakes to remove potentially harmful dust from the influent air. Their use is necessary in desert environments to eliminate the risk of rapid engine wear and subsequent power deterioration. However, their employment is concomitant with an inherent loss in inlet pressure and, in some cases, auxiliary ...
Nicholas Bojdo, Antonio Filippone
exaly   +2 more sources

Development of the helicopter turboshafted engine regulator

open access: yesАвіаційно-космічна техніка та технологія, 2023
The subject of research was the development of the RDC-450M-117V – the TV3-117VMA-SBM1V digital engine regulator – based on the RDC-450M previously created at the enterprise for the AI-450M engine, considering differences in engine characteristics and ...
Gennadii Ranchenko   +4 more
doaj   +2 more sources

Intelligent Method of Identifying the Nonlinear Dynamic Model for Helicopter Turboshaft Engines [PDF]

open access: yesSensors
This 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
doaj   +2 more sources

Neural Network Approximation of Helicopter Turboshaft Engine Parameters for Improved Efficiency

open access: yesEnergies
The work is devoted to the development of a method for neural network approximation of helicopter turboshaft engine parameters, which is the basis for researching engine energy characteristics to improve efficiency, reliability, and flight safety.
Serhii Vladov   +3 more
doaj   +3 more sources

Analysis of unstable mode of a free gas turbine of turbo-compressors engines [PDF]

open access: yesMATEC 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
doaj   +1 more source

Preliminary investigation on the self-propulsion performance of wedge-shaped functional surfaces [PDF]

open access: yesJournal of Intelligent Manufacturing and Special Equipment, 2022
Purpose – The purpose of this paper is to artificially construct a functional surface with self-propulsion flow characteristics for the directional transportation of propellant in surface tension tanks.
Qianqian Li   +5 more
doaj   +1 more source

Influence of Engine Dynamic Characteristics on Helicopter Handling Quality in Hover and Low-Speed Forward Flight

open access: yesAerospace, 2023
This study assesses the influence of engine dynamic characteristics on helicopter handling quality during hover and low-speed forward flight. First, we construct the helicopter–engine coupling model (HECM) based on the power-matching relationship between
Yuan Wei   +3 more
doaj   +1 more source

Forming of turboshaft engine mathematical model

open access: yesАвіаційно-космічна техніка та технологія, 2023
The subject of the study is the process of forming a mathematical model (MM) of a turboshaft gas turbine engine and a twin-engine helicopter power plant, which provides the determination of parameters of the working process in steady and transient ...
Sergiy Yepifanov, Oleksii Bondarenko
doaj   +1 more source

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