In a Gas-Turbine power plant unit, a high-pressure turbine drives the compressor, and a low-pressure turbine drives the generator through suitable gearing system. The overall pressure ratio is 4/1, and the maximum temperature is 6500C. The isentropic efficiencies of the compressor, H.P. turbine, and L.P. turbine, are respectively 0.8, 0.83, and 0.85, and the mechanical efficiency of both shafts is 98%. Calculate the intermediate pressure of the turbine when the air intake conditions are 1.01 bar and 250C. Calculate also the thermal efficiency and the shaft power when mass flow is 60 kg/s.

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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In a Gas-Turbine power plant unit, a high-pressure
turbine drives the compressor, and a low-pressure
turbine drives the generator through suitable gearing
system. The overall pressure ratio is 4/1, and the
maximum temperature is 6500C. The isentropic
efficiencies of the compressor, H.P. turbine, and L.P.
turbine, are respectively 0.8, 0.83, and 0.85, and the
mechanical efficiency of both shafts is 98%. Calculate
the intermediate pressure of the turbine when the air
intake conditions are 1.01 bar and 250C. Calculate
also the thermal efficiency and the shaft power when
mass flow is 60 kg/s.
Transcribed Image Text:In a Gas-Turbine power plant unit, a high-pressure turbine drives the compressor, and a low-pressure turbine drives the generator through suitable gearing system. The overall pressure ratio is 4/1, and the maximum temperature is 6500C. The isentropic efficiencies of the compressor, H.P. turbine, and L.P. turbine, are respectively 0.8, 0.83, and 0.85, and the mechanical efficiency of both shafts is 98%. Calculate the intermediate pressure of the turbine when the air intake conditions are 1.01 bar and 250C. Calculate also the thermal efficiency and the shaft power when mass flow is 60 kg/s.
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