Optimum design of bivariate operation strategy for a supercritical/ transcritical CO2 hybrid waste heat recovery system driven by gas turbine exhaust

被引:6
作者
Cao, Yue [1 ,2 ]
Zhan, Jun [1 ]
Jia, Boqing [1 ]
Chen, Ranjing [1 ]
Si, Fengqi [1 ]
机构
[1] Southeast Univ, Sch Energy & Environm, Key Lab Energy Thermal Convers & Control, Minist Educ, Nanjing 210096, Peoples R China
[2] Southeast Univ, Key Lab Energy Thermal Convers & Control, Minist Educ, 2 Sipailou, Nanjing 210096, Peoples R China
关键词
Supercritical carbon dioxide; Waste heat recovery system; Gas turbine exhaust; Bivariate operation strategy; Optimum design; THERMOECONOMIC ANALYSIS; COLD ENERGY; CYCLE; OPTIMIZATION;
D O I
10.1016/j.energy.2023.129325
中图分类号
O414.1 [热力学];
学科分类号
摘要
Gas turbines are always operated under part-load conditions to participate in the frequency regulation of power grids; therefore, the exhaust gas has fluctuating temperature and mass flow rate parameters. For better utilization of the waste heat in gas turbine exhaust under part-load conditions, a supercritical/transcritical carbon dioxide (CO2) hybrid waste heat recovery system with different operation strategies was studied. The turbine inlet pressure and mass flow rate were considered as the dominant factors affecting the system part-load performance, which formed a bivariate operation strategy. A solution procedure was proposed to optimize the bivariate operation strategy for a hybrid waste heat recovery system. The results indicate that the mass flow rate of the transcritical CO2 cycle has a greater effect on its net power than the turbine inlet pressure whereas these two regulation variables should be controlled cooperatively. The net power of the hybrid waste heat recovery system increased with an increase in the inlet valve opening of the supercritical CO2 turbine under a specific gas turbine load. Generally, the optimal bivariate operation strategy has the advantage of enhancing the part-load performance of a hybrid waste heat recovery system driven by gas turbine exhaust.
引用
收藏
页数:16
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