In: Mechanical Engineering
A gas-turbine power plant operates on the simple Brayton cycle between the pressure limits of 100 and 1200 kPa. The working fluid is air, which enters the compressor at 300K at a rate of 150 m3/min and leaves the turbine at 773K. Using variable specific heats for air and assuming a compressor isentropic efficiency of 82 percent and a turbine isentropic efficiency of 88 percent, determine:
(a) the net power output
(b) the back work ratio
(c) the thermal efficiency
The Brayton cycle is the ideal cycle for gas-turbine engines in which the working fluid undergoes a closed loop. That is the combustion and exhaust processes are modeled by constant-pressure heat addition and rejection, respectively. The Brayton ideal cycle is made up of four internally reversible processes:
1-2 isentropic compression (in the compressor)
2-3 const. pressure heat-addition (in the combustion chamber)
3-4 isentropic expansion (in the turbine)
4-1 constant pressure heat rejection
the p-v and T-s diagrams are shown in the image below:
the processes of the cycle are given in the table below
air is the working fluid with a variable specific heat
T1=300K
from the tables, we can obtain the values of S1 and h1.
s1 = 5.7159KJ/Kg.k
h1 = 303.6KJ/Kg
p1 = 12oo kPa
s1= s2
P2= 1200kPa
the solutions are given in the images below
the net power output is 659.73 kW
the back work ratio is 0.625
the thermal efficiency of the cycle is 0.3193/31.93%