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 2478C. 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 (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.

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 2478C. 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 (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.

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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Question

2. 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 2478C. 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 (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.

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