7. The gas-turbine cycle of a combined gas-steam power plant has a pressure ratio of 12. Air enters the compressor at 310 K and the turbine at 1400 K. The combustion gases leaving the gas turbine are used to heat the steam at 12.5 MPa to 500 °C in a heat exchanger. The combustion gases leave the heat exchanger at 247 °C. Steam expands in a high-pressure turbine to a pressure of 2.5 MPa and is reheated in the combustion chamber to 550 °C before it expands in a low-pressure turbine to 10 kPa. The mass flow rate of steam is 12 kg/s. Assuming all the compression and expansion processes to be isentropic, determine 154 kJ/s 1.44 105 kJ/s [50.1% (a) the mass flow rate of air in the gas-turbine cycle, (b) the rate of total heat input, and (c) the thermal efficiency of the combined cycle 8. Repeat previous problem assuming isentropic efficiencies of 100 % for the pump, 85 % for the compressor, and 90 % for the gas and steam turbines

Elements Of Electromagnetics
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7. The gas-turbine cycle of a combined gas-steam power plant has a pressure ratio of 12. Air enters
the compressor at 310 K and the turbine at 1400 K. The combustion gases leaving the gas turbine
are used to heat the steam at 12.5 MPa to 500 °C in a heat exchanger. The combustion gases leave
the heat exchanger at 247 °C. Steam expands in a high-pressure turbine to a pressure of 2.5 MPa
and is reheated in the combustion chamber to 550 °C before it expands in a low-pressure turbine
to 10 kPa. The mass flow rate of steam is 12 kg/s. Assuming all the compression and expansion
processes to be isentropic, determine
154 kJ/s
1.44 105 kJ/s
[50.1%
(a) the mass flow rate of air in the gas-turbine cycle,
(b) the rate of total heat input, and
(c) the thermal efficiency of the combined cycle
8. Repeat previous problem assuming isentropic efficiencies of 100 % for the pump, 85 % for the
compressor, and 90 % for the gas and steam turbines
Transcribed Image Text:7. The gas-turbine cycle of a combined gas-steam power plant has a pressure ratio of 12. Air enters the compressor at 310 K and the turbine at 1400 K. The combustion gases leaving the gas turbine are used to heat the steam at 12.5 MPa to 500 °C in a heat exchanger. The combustion gases leave the heat exchanger at 247 °C. Steam expands in a high-pressure turbine to a pressure of 2.5 MPa and is reheated in the combustion chamber to 550 °C before it expands in a low-pressure turbine to 10 kPa. The mass flow rate of steam is 12 kg/s. Assuming all the compression and expansion processes to be isentropic, determine 154 kJ/s 1.44 105 kJ/s [50.1% (a) the mass flow rate of air in the gas-turbine cycle, (b) the rate of total heat input, and (c) the thermal efficiency of the combined cycle 8. Repeat previous problem assuming isentropic efficiencies of 100 % for the pump, 85 % for the compressor, and 90 % for the gas and steam turbines
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