Pregled bibliografske jedinice broj: 989373
Numerical analysis of real open cycle gas turbine
Numerical analysis of real open cycle gas turbine // INTERNATIONAL SCIENTIFIC CONFERENCE HIGH TECHNOLOGIES. BUSINESS. SOCIETY 2019 - Volume 1 - PROCEEDINGS / Popov, Georgi ; Stavrev, Dimitar (ur.).
Sofija: Scientific technical union of mechanical engineering Industry - 4.0, 2019. str. 51-54 (poster, međunarodna recenzija, cjeloviti rad (in extenso), znanstveni)
CROSBI ID: 989373 Za ispravke kontaktirajte CROSBI podršku putem web obrasca
Naslov
Numerical analysis of real open cycle gas turbine
Autori
Mrzljak, Vedran ; Poljak, Igor ; Orović, Josip ; Prpić-Oršić, Jasna
Vrsta, podvrsta i kategorija rada
Radovi u zbornicima skupova, cjeloviti rad (in extenso), znanstveni
Izvornik
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, 2019, 51-54
Skup
IV International Scientific Conference: High Technologies. Business. Society
Mjesto i datum
Borovec, Bugarska, 11.03.2019. - 14.03.2019
Vrsta sudjelovanja
Poster
Vrsta recenzije
Međunarodna recenzija
Ključne riječi
Gas turbine ; Real open cycle ; Numerical analysis ; Losses ; Efficiency
Sažetak
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%.
Izvorni jezik
Engleski
Znanstvena područja
Strojarstvo, Tehnologija prometa i transport
POVEZANOST RADA
Projekti:
HRZZ-IP-2018-01-3739 - Sustav potpore odlučivanju za zeleniju i sigurniju plovidbu brodova (DESSERT) (Prpić-Oršić, Jasna, HRZZ - 2018-01) ( CroRIS)
Ustanove:
Tehnički fakultet, Rijeka,
Sveučilište u Zadru