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Effect of Refrigerated Inlet Cooling on Greenhouse Gas Emissions for a 250 MW Class Gas Turbine Engine.

Authors :
Dinc, Ali
Mamedov, Ali
Duran, Ertugrul Tolga
Abbassi, Fethi
Elbadawy, Ibrahim
Nag, Kaushik
Moayyedian, Mehdi
Fayed, Mohamed
Otkur, Murat
Gharbia, Yousef
Source :
Aerospace (MDPI Publishing); Oct2023, Vol. 10 Issue 10, p833, 19p
Publication Year :
2023

Abstract

In this study, the effect of inlet air cooling on greenhouse gas (GHG) emissions and engine performance for a land-based gas turbine engine was investigated under varying ambient temperatures (15–55 °C). The study aimed to reduce GHG emissions while improving output power and fuel efficiency during hot weather operating conditions. For illustrative purposes, a representative gas turbine engine model, approximating the 250 MW class General Electric (GE) engine, was analyzed in a simple cycle. A refrigeration process was integrated with a turboshaft gas turbine engine to chill the incoming air, and the power required for cooling was extracted from the gas turbine's output power. This mechanical chiller was assumed to provide a 15 °C inlet air temperature. Without inlet air cooling, at 55 °C ambient temperature, the engine's power output was calculated to decrease by 15.06%, while power-specific fuel consumption and GHG emissions increased by 6.09% and 5.84%, respectively. However, activating the refrigeration or cooling system in the inlet made it possible to mitigate most of the adverse effects of hot weather on the engine's performance and GHG emissions. Therefore, with inlet air cooling, the power output loss reduces to 3.28%, indicating an 11.78% recovery compared to the 15.06% loss without cooling. Similarly, the rise in power-specific fuel consumption caused by high ambient temperature decreases from 6.09% to 3.43%, reflecting a 2.66% improvement. An important finding of the study is that with inlet air cooling, the increase in GHG emissions reduces from 5.84% to 3.41%, signifying a 2.43% improvement on a hot day with a temperature of 55 °C. [ABSTRACT FROM AUTHOR]

Details

Language :
English
ISSN :
22264310
Volume :
10
Issue :
10
Database :
Complementary Index
Journal :
Aerospace (MDPI Publishing)
Publication Type :
Academic Journal
Accession number :
173263409
Full Text :
https://doi.org/10.3390/aerospace10100833