In the gas turbine cycle whose installation scheme is given in the figure below, 80% Isentropically efficient high pressure turbine with only 75% isentropic efficiency It works to give enough power for the compressor. At intermediate pressure, 85% The air entering the isentropically efficient low pressure turbine is expanding. Other information on the cycle where the pressure ratio is rp = 9 given in the figure. Regenerator efficiency is 0.6. Up to Qgiren to the combustion chamber heat is added from the source at Th = 1800 K. If from the heat exchanger The amount of heat released is thrown into the heat well at TL = 290 K. Admissions: 1. Adopt variable specific heat. 2. Compressor and turbines are adiabatic. 3. 4. The dead state temperature is To = TL = 290 K and the dead state pressure is Po = 100 kPa. a) Determine the heat and thermal efficiency given to the cycle at once. b) Each component (compressor, regenerator, combustion chamber, high pressure turbine, low pressure turbine, heat exchanger) entropy generation calculate.

Introduction to Chemical Engineering Thermodynamics
8th Edition
ISBN:9781259696527
Author:J.M. Smith Termodinamica en ingenieria quimica, Hendrick C Van Ness, Michael Abbott, Mark Swihart
Publisher:J.M. Smith Termodinamica en ingenieria quimica, Hendrick C Van Ness, Michael Abbott, Mark Swihart
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In the gas turbine cycle whose installation scheme is given in the figure below, 80% Isentropically efficient high pressure turbine with only 75% isentropic efficiency It works to give enough power for the compressor. At intermediate pressure, 85% The air entering the isentropically efficient low pressure turbine is expanding. Other information on the cycle where the pressure ratio is rp = 9 given in the figure. Regenerator efficiency is 0.6. Up to Qgiren to the combustion chamber heat is added from the source at Th = 1800 K. If from the heat exchanger The amount of heat released is thrown into the heat well at TL = 290 K.

Admissions: 1. Adopt variable specific heat. 2. Compressor and turbines are adiabatic. 3. 4. The dead state temperature is To = TL = 290 K and the dead state pressure is Po = 100 kPa.

a) Determine the heat and thermal efficiency given to the cycle at once. b) Each component (compressor, regenerator, combustion chamber, high pressure turbine, low pressure turbine, heat exchanger) entropy generation calculate. c) Total exergy loss of the cycle, exergy provided to the cycle and II. Calculate the law efficiency. The air thrown into the environment from the "y" point Also consider its exergy.

Regenerator
T3=1200 K
Combustion chamber
Wnet=90 kW
%75
%80
%85
compressor
High pressure turbine
P,=100 kPa
T;=290 K
Low pressure turbine
Transcribed Image Text:Regenerator T3=1200 K Combustion chamber Wnet=90 kW %75 %80 %85 compressor High pressure turbine P,=100 kPa T;=290 K Low pressure turbine
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