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A gas turbine power plant operating on Brayton cycle shown in figure. The air enters the compressor at 300 K and exits at 700 K. The pressure ratio for compressor is 7. The gas enters the turbine at 1600 K, 600 kPa and exits at 1050 K, 100 kPa. Fuel Toe Zook ( 6=7 commur T₁= 300k + fresh air Combustion Chamber Tj = 1600 K Py = 600kPa Tarbing Tut T-1050 K Exhaust ges P = 100 kP Below 30% O Between 30% and 40% O Between 40% and 50% Between 50% and 60% O Above 60% O 12** The adiabatic efficiency of turbine is Below 50% O Between 50% and 55% O Between 55% and 60% O Between 60% and 65% O Above 65% O Input work to compressor in (kJ/kg) ; is Below 400 O Between 400 and 410 Between 410 and 420 O Between 420 and 430 Above 430 O *: The turbine work in (kJ/kg) is Below 200 O Between 200 and 400 O Between 400 and 600 Between 600 and 800 Above 800

A gas turbine power plant operating on Brayton cycle shown in figure. The air enters the compressor at 300 K and exits at 700 K. The pressure ratio for compressor is 7. The gas enters the turbine at 1600 K, 600 kPa and exits at 1050 K, 100 kPa. Fuel Toe Zook ( 6=7 commur T₁= 300k + fresh air Combustion Chamber Tj = 1600 K Py = 600kPa Tarbing Tut T-1050 K Exhaust ges P = 100 kP Below 30% O Between 30% and 40% O Between 40% and 50% Between 50% and 60% O Above 60% O 12** The adiabatic efficiency of turbine is Below 50% O Between 50% and 55% O Between 55% and 60% O Between 60% and 65% O Above 65% O Input work to compressor in (kJ/kg) ; is Below 400 O Between 400 and 410 Between 410 and 420 O Between 420 and 430 Above 430 O *: The turbine work in (kJ/kg) is Below 200 O Between 200 and 400 O Between 400 and 600 Between 600 and 800 Above 800

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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A gas turbine power plant operating on Brayton cycle shown in figure. The air enters the compressor at 300 K and exits at 700 K The pressure ratio for compressor is 7. The gas enters the turbine at 1600 K, 600 kPa and exits at 1050 K, 100 kPa. Fuel T₁ Fook- = ( 6₂=7 commuor 45 T₁= 300k Fresh air TJ Combustion Chamber Ts = 1600 k P₂=600kPa 1 and Tarbing Ext ges -1050 K P=100 k Below 30% Between 30% and 40% Between 40% and 50% Between 50% and 60% Above 60% 12* The adiabatic efficiency of turbine is : Below 50% Between 50% and 55% Between 55% and 60% Between 60% and 65% Above 65% * Input work to compressor in (kJ/kg) ; is Below 400 Between 400 and 410 Between 410 and 420 Between 420 and 430 O Above 430 *: The turbine work in (kJ/kg) is Below 200 O Between 200 and 400 Between 400 and 600 Between 600 and 800 Above 800 O
Transcribed Image Text:A gas turbine power plant operating on Brayton cycle shown in figure. The air enters the compressor at 300 K and exits at 700 K The pressure ratio for compressor is 7. The gas enters the turbine at 1600 K, 600 kPa and exits at 1050 K, 100 kPa. Fuel T₁ Fook- = ( 6₂=7 commuor 45 T₁= 300k Fresh air TJ Combustion Chamber Ts = 1600 k P₂=600kPa 1 and Tarbing Ext ges -1050 K P=100 k Below 30% Between 30% and 40% Between 40% and 50% Between 50% and 60% Above 60% 12* The adiabatic efficiency of turbine is : Below 50% Between 50% and 55% Between 55% and 60% Between 60% and 65% Above 65% * Input work to compressor in (kJ/kg) ; is Below 400 Between 400 and 410 Between 410 and 420 Between 420 and 430 O Above 430 *: The turbine work in (kJ/kg) is Below 200 O Between 200 and 400 Between 400 and 600 Between 600 and 800 Above 800 O
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