Javascript must be enabled to continue!
Analyzing the efficiency of moderate and deep cooling of air at the inlet of gas turbine in various climatic conditions
View through CrossRef
The efficiency of deep cooling air at the inlet of gas turbine unite to the temperature of 10 °С by waste heat recovery combined absorption-ejector chiller was analyzed in climatic conditions at Kharkov site, Ukraine, and Beijing site, China, and compared with the moderate cooling to the temperature of 15°C in traditional absorption lithium-bromide chiller. The refrigerant ejector chiller is chosen as the most simple and reliable in operation chiller. It was used as the low-temperature stage for subcooling the air precooled in absorption lithium-bromide chiller to the temperature about 15 °C. Both waste heat recovery absorption lithium-bromide chiller and ejector chiller use the heat of gas turbine unite exhaust gas to produce a cooling capacity. Air cooling at the inlet of gas turbine unite was investigated for varying climatic conditions during the year. The current values of temperature depression with cooling ambient air to different temperatures of 10 °C and 15 °C and corresponding cooling capacities required were calculated. The comparison of the effect due to gas turbine unite inlet air cooling was performed by annual fuel saving and power production growth. With this the current values of turbine power output increase and specific fuel consumption decrease due to cooling inlet air from current varying ambient temperatures to the temperatures of 10 °C and 15 °C were calculated. It was shown that annual fuel saving and power production growth have increased by 1,8 times for Kharkov (Ukraine) site climatic conditions and by 1,6 times for Beijing (China) site due to deep cooling air to the temperature of 10 °C by absorption-ejector chiller as compared with cooling inlet air to the temperature of 15 °C by absorption lithium-bromide chiller.
Odesa National University of Technology
Title: Analyzing the efficiency of moderate and deep cooling of air at the inlet of gas turbine in various climatic conditions
Description:
The efficiency of deep cooling air at the inlet of gas turbine unite to the temperature of 10 °С by waste heat recovery combined absorption-ejector chiller was analyzed in climatic conditions at Kharkov site, Ukraine, and Beijing site, China, and compared with the moderate cooling to the temperature of 15°C in traditional absorption lithium-bromide chiller.
The refrigerant ejector chiller is chosen as the most simple and reliable in operation chiller.
It was used as the low-temperature stage for subcooling the air precooled in absorption lithium-bromide chiller to the temperature about 15 °C.
Both waste heat recovery absorption lithium-bromide chiller and ejector chiller use the heat of gas turbine unite exhaust gas to produce a cooling capacity.
Air cooling at the inlet of gas turbine unite was investigated for varying climatic conditions during the year.
The current values of temperature depression with cooling ambient air to different temperatures of 10 °C and 15 °C and corresponding cooling capacities required were calculated.
The comparison of the effect due to gas turbine unite inlet air cooling was performed by annual fuel saving and power production growth.
With this the current values of turbine power output increase and specific fuel consumption decrease due to cooling inlet air from current varying ambient temperatures to the temperatures of 10 °C and 15 °C were calculated.
It was shown that annual fuel saving and power production growth have increased by 1,8 times for Kharkov (Ukraine) site climatic conditions and by 1,6 times for Beijing (China) site due to deep cooling air to the temperature of 10 °C by absorption-ejector chiller as compared with cooling inlet air to the temperature of 15 °C by absorption lithium-bromide chiller.
Related Results
A Solution for Improving Gas Turbine Performance Degradation and Emissions: The “GT Auto Tuner” Product
A Solution for Improving Gas Turbine Performance Degradation and Emissions: The “GT Auto Tuner” Product
Abstract
The main causes of gas turbine performance degradation in natural gas combined cycle power plants are corrosion, fouling, and high turbine inlet temperature...
Analysis of Integrated Cooling Systems for Gas Turbine Power Plants
Analysis of Integrated Cooling Systems for Gas Turbine Power Plants
With the current increase in electricity consumption and energy demand, most of the research focus is shifted towards the means of increasing the power plants efficiency in order t...
Predicting streetscape green infrastructure performance amidst uncertain inflow
Predicting streetscape green infrastructure performance amidst uncertain inflow
Sustainable cities feature infrastructure that is adaptive to a wide range of spatially and temporally variable conditions. Water infrastructure needs to be responsive to both the ...
Thermodynamic Analysis of an Evaporative Inlet Air Cooled Combined Cycle for Marine Application
Thermodynamic Analysis of an Evaporative Inlet Air Cooled Combined Cycle for Marine Application
<div class="section abstract"><div class="htmlview paragraph">The integration of inlet air cooling to gas turbine based power utilities is a well accepted practice as t...
Effects of Inlet Swirl on Endwall Film Cooling in Neighboring Vane Passages
Effects of Inlet Swirl on Endwall Film Cooling in Neighboring Vane Passages
The distribution of film cooling effectiveness of endwall film-cooling holes is considered to be periodic between neighboring high pressure turbine passages in most cascade experim...
PENGARUH AIR FUEL RATIO (AFR) TERHADAP EFISIENSI TURBIN GAS
PENGARUH AIR FUEL RATIO (AFR) TERHADAP EFISIENSI TURBIN GAS
Gas turbine efficiency is an indicator to determine the performance of a generator. The greater the efficiency value of the gas turbine in a generator, the better the performance o...
Data-Driven Thermo-Structural Optimization of Gas Turbine Blades Using Finite Element Modeling, Cooling Configurations, and Thermal Barrier Coatings
Data-Driven Thermo-Structural Optimization of Gas Turbine Blades Using Finite Element Modeling, Cooling Configurations, and Thermal Barrier Coatings
Gas turbine blades operate under extremely severe thermo-mechanical environments characterized by elevated turbine inlet temperatures, high centrifugal forces, thermal gradients, o...
Innovative Turbine Intake Air Cooling Systems and Their Rational Designing
Innovative Turbine Intake Air Cooling Systems and Their Rational Designing
The efficiency of cooling ambient air at the inlet of gas turbines in temperate climatic conditions was analyzed and reserves for its enhancing through deep cooling were revealed. ...

