Results 111 to 120 of about 1,125 (144)
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Fuzzy Logic Application in Helicopter Turboshaft Engines Automatic Control Systems

2024 IEEE 17th International Conference on Advanced Trends in Radioelectronics, Telecommunications and Computer Engineering (TCSET)
Serhii Vladov   +2 more
exaly   +2 more sources

A turboshaft engine NMPC scheme for helicopter autorotation recovery maneuver

Aerospace Science and Technology, 2018
Abstract Fast response for turboshaft engine plays an important role in shaping sound helicopter maneuver ability during some typical violent maneuvers like autorotation power recovery. An engine NMPC (nonlinear model predictive control), integrated with flight predictive information, is proposed to obtains better engine response speed and reduces ...
Qiangang Zheng   +3 more
openaire   +1 more source

Some Aspects of Turboshaft Engine Installations in Multi-engined Helicopters

The Journal of the Royal Aeronautical Society, 1964
In projecting future turboshaft engines for helicopter appUcations the engine designer is faced with the problem of selecting the size of engine to meet the likely size, configuration, performance and economic requirements of future helicopters. It is also desirable to meet as many different helicopter applications as possible with the same basic ...
openaire   +1 more source

Multi-objective optimization and system evaluation of recuperated helicopter turboshaft engines

Energy, 2020
Abstract Targeting higher efficiency and lower emissions, the employment of recuperators in helicopters is well recognized as an attractive technical strategy to enhance the operational capabilities. Primary surface recuperator (PSR) is proposed for such applications, as its favorable characteristics of good heat transfer performance and compact ...
Chengyu Zhang, Volker Gümmer
openaire   +1 more source

Performance of a Turboshaft Engine for Helicopter Applications Operating at Variable Shaft Speed

ASME 2012 Gas Turbine India Conference, 2012
An off-design steady state model of a generic turboshaft engine has been implemented to assess the influence of variable free power turbine (FPT) rotational speed on overall engine performance, with particular emphasis on helicopter applications. To this purpose, three off-design flight conditions were simulated and engine performance obtained with ...
MISTE', GIANLUIGI ALBERTO   +1 more
openaire   +2 more sources

Simulation of the Transient Response of a Helicopter Turboshaft Engine to Hot-Gas Ingestion

Volume 2: Controls, Diagnostics and Instrumentation; Cycle Innovations; Electric Power, 2008
Hot-Gas Ingestion (HGI) to the engines can potentially occur when a rotorcraft or a VTOL/STOVL fixed-wing aircraft is operating in close proximity to the ground. Especially for helicopters, due to the rotor downwash hot exhaust gases get recirculated into the engine inlet. Similar conditions may also occur due to the ingestion of hot exhaust gases from
Gu¨lru Koc¸er   +2 more
openaire   +1 more source

Contingency Power Concepts for Helicopter Turboshaft Engines

Journal of the American Helicopter Society, 1985
Robert Hirschkron   +4 more
openaire   +1 more source

Improving the efficiency of aviation turboshaft engine with the recuperator in the helicopter system

AIP Conference Proceedings, 2023
H. H. Omar   +3 more
openaire   +1 more source

Analytical Neural Network System for the Helicopter Turboshaft Engines Operating Modes Classification

International Journal of Computing
A novel neural network-based analytical system has been developed for classifying helicopter turboshaft engine operating modes during flight operations. This system utilizes a neural network architecture comprising an input layer with three neurons, two fully connected hidden layers, and an output layer with two neurons.
Serhii Vladov   +3 more
openaire   +1 more source

Neural Network Method for Detecting and Diagnostics Helicopters Turboshaft Engines Surge at Flight Modes [PDF]

open access: possibleComputer Modeling and Intelligent Systems, 2023
Serhii Vladov   +3 more
openaire   +1 more source

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