相对速比对超临界CO2离心叶轮运行的影响

Haiqing Liu, Zhongran Chi, S. Zang
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引用次数: 0

摘要

超临界CO2燃气轮机被认为是通过减少压缩机在临界点附近的工作来实现高循环效率。但国际上进行的试验循环表明,该压缩机的性能与设计点的目标还相差甚远。研究了相对速比对实际气体CO2和理想气体CO2工况下离心叶轮性能的影响。同时,比较了近临界、超临界和亚临界进口工况下叶轮与实际气体CO2的特性曲线。在同一叶轮中,实际气体CO2和理想气体CO2的相对流速比变化趋势相同,但具体数值不同。当相对速度比在1.05 ~ 1.5范围内时,真实气体CO2叶轮可以获得较高的等熵效率。结果表明,相对速度比对压气机性能有重要影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Influence of Relative Velocity Ratio on Centrifugal Impellers Operating With Supercritical CO2
The supercritical CO2 gas turbine is considered to achieve a high cycle efficiency by reducing compressor work near the critical point. But test loops made by international community show that the performance of the compressor is still quite far from the target at the design point. The paper focuses on the influence of relative velocity ratio on the performances of centrifugal impellers operating with real gas CO2 and ideal gas CO2. At the same time, comparisons between characteristic curves of impellers operating at near critical, supercritical, and subcritical inlet condition with real gas CO2 are also demonstrated. Relative velocity ratio demonstrates the same trend with real and ideal gas CO2 in the same impeller, but the specific value is different. Impellers with real gas CO2 could achieve a high isentropic efficiency when relative velocity ratio is in the range of 1.05∼1.5. The results show that relative velocity ratio plays an important role in compressor performance.
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