Influence of Real Gas Properties on Loss in a Super Critical CO2 (sCO2) Centrifugal Compressor

Ruikai Cai, Mingyang Yang, K. Deng, W. Zhuge, Bijie Yang, R. Martinez-Botas, Tao Chen
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Abstract

The performance of the SCO2 centrifugal compressor is the key component influencing the efficiency and stability of the whole Close-Bryton cycle system. It is important to understand the loss mechanism inside the compressor to guide the design and performance optimization of the compressor. However, the physical properties of SCO2 are strongly nonlinear near the critical point, and the internal flow of the compressor is highly coupled with its properties, which inevitably profoundly influences the loss generation in the device. In this paper, the loss mechanism of SCO2 compressor is investigated comprehensively based on numerical method compared with experimental data. CO2 real gas model embodied in RANS model are used for the study. Firstly, grid independence and influence of the resolution of real gas properties tables are discussed. The numerical simulation results are in good agreement with the experimental data of Sandia SCO2 compressor. Secondly, the distribution of the loss of the compressor are evaluated by means of local entropy generation at different mass flow rates. In particular, a direction comparison between the cases with real gas properties and the constant properties is carried out for manifesting of the influence by real gas properties. The results manifest that the loss of the case with constant properties is profoundly higher than that of the real gas properties, especially at small flow rate. Detailed flow field is compared to understand the influence of the properties. It is shown that the tip leakage flow is evidently decreased with the real gas properties and results in a much more uniform flow distribution throughout the impeller. The decrease in static temperature and pressure due to the acceleration of SCO2 at the tip of the main blade causes an increase in fluid density, reducing the tip leakage and secondary flow. Moreover, the influence on the flow in the impeller results in smaller incidence angle near hub side for the case with real gas properties, thus the separation on the suction surface which happens in the case with constant properties is alleviated. Therefore, the loss in both the impeller and diffuser is significantly reduced by the real gas properties.
超临界CO2 (sCO2)离心式压缩机实际气体特性对损耗的影响
SCO2离心式压缩机的性能是影响整个Close-Bryton循环系统效率和稳定性的关键部件。了解压缩机内部的损耗机理对指导压缩机的设计和性能优化具有重要意义。然而,在临界点附近,SCO2的物理性质是强烈非线性的,压缩机内部流动与其性质高度耦合,这不可避免地深刻影响了装置内的损耗产生。本文采用数值方法与实验数据进行对比,对SCO2压缩机的损失机理进行了全面研究。采用RANS模型中包含的CO2实气模型进行研究。首先,讨论了网格独立性及其对真实气体属性表分辨率的影响。数值模拟结果与桑迪亚SCO2压缩机的实验数据吻合较好。其次,利用局部熵产生法对不同质量流量下压气机的损失分布进行了评估;为了体现实际气体性质的影响,特别对实际气体性质与恒定气体性质的情况进行了方向比较。结果表明,恒定性质情况下的损失远高于实际气体性质,特别是在小流量情况下。通过详细的流场对比来了解性能的影响。结果表明,叶尖泄漏流量随实际气体性质的变化明显减小,叶轮内流动分布更加均匀。由于主叶片尖端SCO2的加速,静温和静压的降低导致流体密度的增加,减少了叶尖泄漏和二次流。此外,对叶轮内流动的影响使得真实气体特性的情况下,靠近轮毂侧的入射角较小,从而减轻了恒定气体特性情况下发生的吸力面分离。因此,叶轮和扩散器中的损失都因实际气体性质而显著降低。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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