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 Find Work In put work efficiency To - 1600 k

Elements Of Electromagnetics
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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
T₂ = 700k.
p=7 Compressor
T₁ = 300k Fresh air
Combustion Chamber
Turbine
Find
Work
T3 = 1600 K
P3=600 кра
Exhaust gas
In put work
efficiency
we
net
=1050 K
P4=100 kPa
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 T₂ = 700k. p=7 Compressor T₁ = 300k Fresh air Combustion Chamber Turbine Find Work T3 = 1600 K P3=600 кра Exhaust gas In put work efficiency we net =1050 K P4=100 kPa
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