Operational characteristics of micro gas turbine engines using kerosenes produced by different technologies; Fuel; Vol. 406, Pt. C

Operational characteristics of micro gas turbine engines using kerosenes produced by different technologies; Fuel; Vol. 406, Pt. C

Bibliographic Details
Parent link:Fuel.— .— Amsterdam: Elsevier Science Publishing Company Inc.
Vol. 406, Pt. C.— 2026.— Article number 137102, 15 p.
Main Author: Antonov D. V. Dmitry Vladimirovich
Other Authors: Cherkasov R. E. Roman Evgenjevich, Mikulich M. E. Mikhail Evgenjevich
Summary:Title screen
This study evaluates the combustion of different liquid fuel samples, including straight-run kerosene, hydrotreated kerosene, their blend, and TS-1 kerosene, in micro gas turbine engines (MGTEs). A series of tests revealed key operational parameters of the engines: thrust, inlet static pressure, compressor static pressure, compressor total pressure, combustor total pressure, turbine total pressure, turbine speed, as well as air temperature at the inlet, inside the compressor, at the turbine outlet, and at the nozzle exit. The thermodynamic cycle analysis of MGTE was performed at the required thrust levels for each fuel. The concentrations of anthropogenic gas emissions CO, CO2, NO, NO2, N2O, SO2, CH4, and C3H8 were quantified, alongside noise and vibration levels. According to the multi-criteria analysis of MGTE performance, accounting for the hydrocarbon-type composition of each fuel, hydrotreated kerosene exhibits the best results
Текстовый файл
AM_Agreement
Language:English
Published: 2026
Subjects:
Liquid aviation fuels
Straight-run kerosene
Hydrotreated kerosene
Micro gas turbine engines
Thermodynamic cycle analysis
Multi-criteria analysis
электронный ресурс
труды учёных ТПУ
Online Access:https://doi.org/10.1016/j.fuel.2025.137102
Format: Electronic Book Chapter
KOHA link:https://koha.lib.tpu.ru/cgi-bin/koha/opac-detail.pl?biblionumber=682681

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