Numerical analysis of real open cycle gas turbine (CROSBI ID 673761)
Prilog sa skupa u zborniku | izvorni znanstveni rad | međunarodna recenzija
Podaci o odgovornosti
Mrzljak, Vedran ; Poljak, Igor ; Orović, Josip ; Prpić-Oršić, Jasna
engleski
Numerical analysis of real open cycle gas turbine
The paper presents a thermodynamic analysis of gas turbine with real open cycle. Gas turbine operates in combined heat and power (CHP) system. Analysis is provided by using measured operating parameters of operating mediums (air and combustion gases) in all required operating points. Cumulative real turbine developed power amounts 78611.63 kW. In the whole gas turbine process, the highest losses occur in combustion chambers during the heat supply process and amounts 13689.24 kW. Turbine power losses are equal to 7976.22 kW, while the turbo-compressor power losses amounts 4774.24 kW. While taking into account all analyzed gas turbine components, the highest efficiency of 90.79% has turbine, followed by combustion chambers which efficiency is equal to 89.01%. Turbo-compressor efficiency amounts 88.59% and the whole gas turbine cycle has efficiency equal to 33.15%.
Gas turbine ; Real open cycle ; Numerical analysis ; Losses ; Efficiency
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Podaci o prilogu
51-54.
2019.
objavljeno
Podaci o matičnoj publikaciji
INTERNATIONAL SCIENTIFIC CONFERENCE HIGH TECHNOLOGIES. BUSINESS. SOCIETY 2019 - Volume 1 - PROCEEDINGS
Popov, Georgi ; Stavrev, Dimitar
Sofija: Scientific technical union of mechanical engineering Industry - 4.0
2535-0005
2535-0013
Podaci o skupu
IV International Scientific Conference: High Technologies. Business. Society
poster
11.03.2019-14.03.2019
Borovec, Bugarska