Results 1 to 10 of about 7,895 (248)

Intelligent Situational Control of Small Turbojet Engines

open access: goldInternational Journal of Aerospace Engineering, 2018
Improvements in reliability, safety, and operational efficiency of aeroengines can be brought in a cost-effective way using advanced control concepts, thus requiring only software updates of their digital control systems.
Rudolf Andoga   +6 more
doaj   +3 more sources

Design and Experimental Study of a Turbojet VTOL Aircraft with One-Dimensional Thrust Vectoring Nozzles

open access: yesAerospace, 2022
Turbojet engines have a slow response and require mechanical assistance to perform vertical take-offs and landings. In this paper, we propose a vertical take-off and landing (VTOL) aircraft that contains one-dimensional thrust vectoring nozzle modules to
Benshan Liu   +6 more
doaj   +2 more sources

Mach 4 Simulating Experiment of Pre-Cooled Turbojet Engine Using Liquid Hydrogen

open access: yesAerospace, 2022
This study investigated a pre-cooled turbojet engine for a Mach 5 class hypersonic transport aircraft. The engine was demonstrated under takeoff and Mach 2 flight conditions, and a Mach 5 propulsion wind tunnel test is planned.
Hideyuki Taguchi   +5 more
doaj   +2 more sources

Single Neural Adaptive PID Control for Small UAV Micro-Turbojet Engine. [PDF]

open access: yesSensors (Basel), 2020
The micro-turbojet engine (MTE) is especially suitable for unmanned aerial vehicles (UAVs). Because the rotor speed is proportional to the thrust force, the accurate speed tracking control is indispensable for MTE.
Tang W, Wang L, Gu J, Gu Y.
europepmc   +2 more sources

Advanced Control of an Electric Fuel-Oil Pump for Small Turbojet Engines

open access: yesAerospace, 2022
One way to efficiently control the fuel flow of small turbojet engines is to use direct control of the speed of a suitable electric fuel pump, as opposed to using relief valves.
Ladislav Főző, Rudolf Andoga
doaj   +2 more sources

Impact of Using Chevrons Nozzle on the Acoustics and Performances of a Micro Turbojet Engine

open access: yesApplied Sciences, 2021
This paper presents a study regarding the noise reduction of the turbojet engine, in particular the jet noise of a micro turbojet engine. The results of the measurement campaign are presented followed by a performances analysis which is based on the ...
Grigore Cican   +2 more
doaj   +2 more sources

Robust Control of Small Turbojet Engines [PDF]

open access: yesMachines, 2019
Modern turbojet engines mainly use computerized digital engine control systems. This opens the way for application of advanced algorithms aimed at increasing their operational efficiency and safety.
Rudolf Andoga   +5 more
doaj   +4 more sources

Control-Oriented System Identification of Turbojet Dynamics

open access: yesAerospace
The autonomous operation of turbojets requires reliable, accurate, and manageable dynamical models for several key processes. This article describes a practical robust method for obtaining turbojet thrust and shaft speed models from experimental data ...
Francisco Villarreal-Valderrama   +5 more
doaj   +2 more sources

Linear dynamic mathematical model and identification of micro turbojet engine for Turbofan Power Ratio control

open access: diamondAviation, 2019
Micro turbojets can be used for propulsion of civilian and military aircraft, consequently their investigation and control is essential. Although these power plants exhibit nonlinear behaviour, their control can be based on linearized mathematical models
Khaoula Derbel, Károly Beneda
doaj   +3 more sources

Making High Thermoelectric and Superior Mechanical Performance Nb0.88Hf0.12FeSb Half-Heusler via Additive Manufacturing. [PDF]

open access: yesAdv Sci (Weinh)
Nb0.88Hf0.12FeSb, a half‐Heusler thermoelectric material for energy harvesting, exhibits a very promising thermoelectric figure of merit ZT ≈ 100 °C. With the application of laser‐based 3D printing technique onto high‐quality spherical precursor powder, highly flexible shape‐customization, and efficient prolificacy can be further achieved with ...
Yao Z   +16 more
europepmc   +2 more sources

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