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

Author:

Dinc Ali1ORCID,Mamedov Ali1ORCID,Duran Ertugrul Tolga1,Abbassi Fethi1ORCID,Elbadawy Ibrahim1ORCID,Nag Kaushik1,Moayyedian Mehdi1,Fayed Mohamed1ORCID,Otkur Murat1ORCID,Gharbia Yousef1

Affiliation:

1. College of Engineering and Technology, American University of the Middle East, Egaila 54200, Kuwait

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.

Publisher

MDPI AG

Subject

Aerospace Engineering

Reference48 articles.

1. (2022, October 12). GE News GE’s Gas Turbine Upgrades Increase Output and Efficiency at Kuwait’s Sabiya West CCGT 2000 MW Power Plant. Available online: https://www.ge.com/news/press-releases/ge’s-gas-turbine-upgrades-increase-output-and-efficiency-kuwait’s-sabiya-west-ccgt.

2. (2022, October 12). Kuwait Energy Outlook. Available online: https://www.undp.org/arab-states/publications/kuwait-energy-outlook-1.

3. Brooks, F.J. (2000). GE Gas Turbine Performance Characteristics, GE Power Systems. GER-3567H.

4. Gas Turbine Performance at Varying Ambient Temperature;Appl. Therm. Eng.,2011

5. The Energy Analysis of GE-F5 Gas Turbines Inlet Air–Cooling Systems by the off-Design Method;Arabi;Meas. Control,2019

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