Heat Transfer: Volume 1 2008
DOI: 10.1115/ht2008-56129
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Optimization of Combined Cycle Power Plant Using Sequential Quadratic Programming

Abstract: The thermal-economic optimization of a combined cycle power plant (CCPP) which can provide 140 MW of electrical power is discussed in this paper. The CCPP is composed of a gas turbine cycle (including, air compressor, combustion chamber, gas turbine), heat recovery steam generator (HRSG), steam turbine, condenser system, and a pump. The design parameters of such a plant are compressor pressure ratio (rAC), compressor isentropic efficiency (ηAC) gas turbine isentropic efficiency (ηGT), and turbine inlet tempera… Show more

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Cited by 13 publications
(5 citation statements)
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“…The lower heating value (LHV), referred to as the net calorific value, of a fuel is determined by combusting a specified quantity of the fuel (initially at 25℃) and restoring the temperature of the combustion products to 150℃. In the case of gaseous fuels with a composition of C x H y , a specific experimental equation is employed to calculate the parameter ξ, representing the fuel exergy [21],…”
Section: Exergy Analysismentioning
confidence: 99%
“…The lower heating value (LHV), referred to as the net calorific value, of a fuel is determined by combusting a specified quantity of the fuel (initially at 25℃) and restoring the temperature of the combustion products to 150℃. In the case of gaseous fuels with a composition of C x H y , a specific experimental equation is employed to calculate the parameter ξ, representing the fuel exergy [21],…”
Section: Exergy Analysismentioning
confidence: 99%
“…Along with system simulation and economic analysis, mathematical optimization was applied to gas turbine power cycles [14][15][16][17][18]. For the optimization, several algorithms were selected depending on the type of optimization, e.g., the mixed integer linear programming (MINLP), genetic algorithm (GA), simplex method, and sequential quadratic programming (SQP).…”
Section: Simple Cyclementioning
confidence: 99%
“…The inequality constraints were selected considering the technological status of the gas turbine components [18,38,39,44]. As discussed in Section 4.2 and shown in Table A1, design variables, such as the air compressor pressure ratio, compressor and turbine isentropic efficiencies, were included in the cost equations.…”
Section: Optimization Proceduresmentioning
confidence: 99%
“…The cost function for each composition of the multigeneration system in terms of design parameters[8,9]. exp (C 32 comb − 24 )) 21 = 46.08, 22 = 0.995 23 = 0.018, 24 = 26.4…”
mentioning
confidence: 99%