Results 1 to 10 of about 13,981 (165)

Gear-Shaped High‑g Combustion Chamber for Micro Turbojet Engine Applications [PDF]

open access: goldACS Omega
Enhancing combustion efficiency and optimizing the thrust-to-weight ratio are critical technical challenges encountered in the development, application, and growth of micro turbojet engines.
Haozhong Huang   +4 more
doaj   +7 more sources

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

open access: goldSensors, 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.
Wei Tang   +3 more
doaj   +8 more sources

Investigation of thrust vector angle control law based on micro-turbojet engine [PDF]

open access: goldAIP Advances, 2022
The fluid thrust vectoring nozzle has a fixed profile, few moving parts, and lightweight structure, providing effective flight control for high maneuvering aircraft. The nonlinear control law of the jet deflection angle is one of the critical problems of
Shaoqing Chi   +3 more
doaj   +4 more sources

Experimental Investigation of Particulate Number Measurement Methodology for Micro-Turbojet Engine Emissions [PDF]

open access: goldAerospace
Increasing aviation activities have heightened concerns about particulate emissions from aircraft engines. Current ICAO standards mainly focus on large civil turbofan engines, leaving a gap in the research on PN emissions from small aircraft engines ...
Zheng Xu   +8 more
doaj   +4 more sources

Micro turbojet engine nozzle ejector impact on the performance and transient regimes analysis

open access: goldCase Studies in Thermal Engineering
This study investigates the influence of an ejector nozzle on the performance and transient behavior of a micro turbojet engine. The problem addressed is the improvement of thrust and fuel efficiency in micro propulsion systems and offering new insights ...
Valentin Silivestru   +4 more
doaj   +4 more sources

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

open access: goldApplied 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   +3 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   +6 more sources

Micro Turbojet Engine Nozzle Ejector Impact on the Acoustic Emission, Thrust Force and Fuel Consumption Analysis [PDF]

open access: goldAerospace, 2023
This paper explores the implementation of an ejector to a micro turbojet engine and analysis of the advantages in terms of acoustic and thrust/fuel consumption.
Grigore Cican   +3 more
doaj   +3 more sources

Exergoenvironmental, environmental impact and damage cost analyses of a micro turbojet engine (m-TJE)

open access: goldEnergy Reports, 2022
This study presents a comprehensive investigation of the emission impact, environmental damage cost, exergoenvironmental and life cycle assessment (LCA) analyses of a micro turbojet engine (m-TJE) utilized on Unmanned Air Vehicle (UAV) for four different
Ozgur Balli   +3 more
doaj   +3 more sources

Analisis Performa Micro Turbojet Engine Aero-16 Berbasis Turbocharge Holset

open access: diamondJurnal Mahasiswa Dirgantara, 2023
Pesawat terbang adalah kendaraan yang mampu terbang di udara. Pesawat  dapat terbang karena memiliki 4 gaya yaitu thrust, drag, weight dan lift. 4 gaya tersebut dapat berkerja di pesawat karena ada bantuan dari engine dan wing.
Mohammad Reza Pahlevi   +2 more
semanticscholar   +5 more sources

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