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IMPLICATIONS OF PHASE CHANGE ON THE AERODYNAMICS OF CENTRIFUGAL COMPRESSORS FOR SUPERCRITICAL CARBON DIOXIDE APPLICATIONS

机译:相变对超临界二氧化碳应用中离心压缩机空气动力学的影响

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Closed Joule-Bryton cycles operating with carbon dioxide in supercritical conditions (sCO_2) are nowadays collecting a significant scientific interest, due to their high potential efficiency, the compactness of their components, and the flexibility that makes them suitable to exploit diverse energy sources. However, the technical implementation of sCO_2 power systems introduces new challenges related to the design and operation of the components. The compressor, in particular, operates in a thermodynamic condition close to the critical point, whereby the fluid exhibits significant non-ideal gas effects and is prone to phase change in the intake region of the machine. These new challenges require novel design concepts and strategies, as well as proper tools to achieve reliable predictions. In the present study, we consider an exemplary sCO_2 power cycle with main compressor operating in proximity to the critical point, with an intake entropy level of the fluid lower than the critical value. In this condition, the phase change occurs as evaporationflashing, thus resembling cavitation phenomena observed in liquid pumps, even though with specific issues associated to compressibility effects occurring in both the phases. The flow configuration is therefore highly non-conventional and demands the development of proper tools for fluid and flow modeling, which are instrumental for the compressor design. The paper discusses the modeling issues from the thermodynamic perspective and then highlighting the implications on the compressor aerodynamics. We propose tailored models to account for the effect of the phase change in 0D mean-line design tools as well as in fully 3D computational fluid-dynamic (CFD) simulations. In this way, a design strategy is build-up as a combination of mean-line tools, industrial design experience, and CFD for detailed flow analysis. The application of the design strategy reveals that the potential onset of the phase change might alter significantly the performance and operation of the compressor, both in design and in off-design conditions.
机译:封闭焦耳Bryton个循环,在超临界条件(sCO_2)二氧化碳操作现今收集显著科学兴趣,由于其高电势效率,它们的组件的紧凑性,这使得它们适合于利用多样能源的灵活性。然而,技术实施sCO_2动力系统的引入相关部件的设计和运行新的挑战。的压缩机,特别是工作在热力学条件接近临界点,由此流体展品显著非理想气体的影响,而且容易在机器的吸入区相位变化。这些新的挑战需要新的设计理念和策略,以及适当的工具来实现可靠的预测。在本研究中,我们考虑与主压缩机在接近地操作到临界点,具有比临界值中的流体下的进气熵水平的示例性sCO_2电源循环。在该状态下,相变发生时作为evaporationflashing,从而类似于在液体泵观察穴现象,即使与相关联的在两个阶段中发生压缩性效应的具体问题。因此,该流动构造是高度非传统的和要求的流体和流建模适当的工具,这是仪器的压缩机设计的发展。本文从热力学角度讨论了建模问题,然后突出压缩机空气动力学的影响。我们提出符合模型帐户,以及在全3D的计算流体动力学(CFD)模拟在0D中间线设计工具相变化的影响。通过这种方式,设计策略是积聚为中间线工具,工业设计经验相结合,与CFD的详细流程的分析。设计策略的应用表明,相变化的潜在发病可能改变压缩机的显著的性能和操作,无论是在设计和非设计条件。

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