Tuananh Bui, Young Duk Lee, Young Sang Kim, Do Won Kang, K. Ahn, Sangmin Lee, Sung Ho Chang, Min Kuk Kim
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引用次数: 0
摘要
通过系统模拟、参数分析和放能分析,确定了直燃式超临界二氧化碳(sCO2)动力循环中再压缩的优缺点。在参数调查中,改变了再压缩比、涡轮机入口温度(TIT)和压力比,并比较了所获得的动力循环效率值。TIT 在 600 °C 和 1600 °C 之间变化,结果表明,再压缩对较低的 TIT 值非常有效,但对较高的 TIT 值影响较小。当温度系数高于 1400 ℃ 时,再压缩循环的效率几乎没有提高。高压侧和低压侧之间的压力比不同,获得的最佳再压缩比也不同。热能分析表明,热能破坏主要发生在全氧燃烧器中,原因是化学反应和高再循环流体的混合。较高的 TIT 会减少全氧燃烧器的放能破坏,但会增加低温换热器的放能破坏,而且并不总是有利于提高效率。
Performance analysis of high-efficiency supercritical CO2 power cycles using recompression
System simulation, parametric analysis, and exergy analysis were performed to identify the advantages and drawbacks of recompression in the direct-fired supercritical carbon dioxide (sCO2) power cycle. In a parametric investigation, the recompression ratio, turbine inlet temperature (TIT), and pressure ratio were changed, and the obtained values for the efficiency of the power cycle were compared. The TIT was varied between 600 °C and 1600 °C, revealing that recompression is highly effective for lower TIT values but is less effected at higher TIT values. For TITs above 1400 °C, the recompression cycle obtains almost no increase in efficiency. Different optimal recompression ratios were obtained for the different pressure ratios between the high- and low-pressure sides. Exergy analysis reveals that exergy destruction occurs primarily in the oxy-fuel combustor due to a chemical reaction and mixing of the high recirculation fluid. Higher TIT decreases the exergy destruction of the oxy-fuel combustor, but increases the exergy destruction in the lower temperature recuperator, and is not always favorable for obtaining efficiency improvements.