Power and efficiency in a regenerative gas-turbine cycle with multiple reheating and intercooling stages
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Using an improved Brayton cycle as a model, a general analysis accounting for the efficiency and net power output of a gas-turbine power plant with multiple reheating and intercooling stages is presented. This analysis provides a general theoretical tool for the selection of the optimal operating conditions of the heat engine in terms of the compressor and turbine isentropic efficiencies and of the heat exchanger efficiency. Explicit results for the efficiency, net power output, optimized pressure ratios, maximum efficiency, maximum power, efficiency at maximum power, and power at maximum efficiency are given. Among others, the familiar results of the Brayton cycle (one compressor and one turbine) and of the corresponding Ericsson cycle (infinite compressors and infinite turbines) are obtained as particular cases.
[1] Bhairav D. Joshi. Thermodynamic work for N-step isothermal processes involving an ideal gas , 1986 .
[2] A. Bejan. Advanced Engineering Thermodynamics , 1988 .
[3] Alejandro Medina,et al. Power and efficiency in a regenerative gas turbine , 1995 .
[4] Bahri Sahin,et al. Efficiency of a Joule-Brayton engine at maximum power density , 1995 .
[5] J. Gordon,et al. General performance characteristics of real heat engines , 1992 .