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An Investigation of Real Gas Effects in Supercritical CO_2 Centrifugal Compressors

机译:超临界CO_2离心压缩机实际气体影响的研究

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摘要

This paper presents a comprehensive assessment of real gas effects on the performance and matching of centrifugal compressors operating in supercritical CO_2. The analytical framework combines first principles based modeling with targeted numerical simulations to characterize the internal flow behavior of supercritical fluids with implications for radial turbomachinery design and analysis. Trends in gas dynamic behavior, not observed for ideal fluids, are investigated using influence coefficients for compressible channel flow derived for real gas. The variation in the properties of CO_2 and the expansion through the vapor-pressure curve due to local flow acceleration are identified as possible mechanisms for performance and operability issues observed near the critical point. The performance of a centrifugal compressor stage is assessed at different thermo-dynamic conditions relative to the critical point using computational fluid dynamics (CFD) calculations. The results indicate a reduction of 9% in the choke margin of the stage compared to its performance at ideal gas conditions due to variations in real gas properties. Compressor stage matching is also impacted by real gas effects as the excursion in corrected mass flow per unit area from inlet to outlet increases by 5%. Investigation of the flow field near the impeller leading edge at high flow coefficients shows that local flow acceleration causes the thermodynamic conditions to reach the vapor-pressure curve. The significance of two-phase flow effects is determined through a nondimensional parameter that relates the time required for liquid droplet formation to the residence time of the flow under saturation conditions. Applying this criterion to the candidate compressor stage shows that condensation is not a concern at the investigated operating conditions. In the immediate vicinity of the critical point however, this effect is expected to become more prominent. While the focus of this analysis is on supercritical CO_2 compressors for carbon capture and sequestration (CCS), the methodology is directly applicable to other nonconventional fluids and applications.
机译:本文全面评估了实际气体对超临界CO_2下运行的离心压缩机性能和匹配的影响。该分析框架将基于第一原理的建模与目标数值模拟相结合,以表征超临界流体的内部流动行为,这对径向涡轮机械的设计和分析具有重要意义。使用针对真实气体得出的可压缩通道流量的影响系数,研究了理想流体未观察到的气体动力学行为趋势。可以确定在局部临界点附近观察到的性能和可操作性问题的可能机制,是由于局部流动加速引起的CO_2性质变化和通过蒸汽压力曲线的膨胀。使用计算流体动力学(CFD)计算,可以在相对于临界点的不同热力学条件下评估离心压缩机级的性能。结果表明,由于实际气体特性的变化,与在理想气体条件下的性能相比,该级的节流裕度降低了9%。压缩机级匹配也受到实际气体影响的影响,因为从入口到出口的每单位面积校正质量流的偏移增加了5%。对高流量系数下叶轮前缘附近的流场的研究表明,局部流加速度导致热力学条件达到蒸气压曲线。两相流效应的重要性是通过一个无量纲参数确定的,该参数将液滴形成所需的时间与流体在饱和条件下的停留时间相关联。将这一标准应用于候选压缩机阶段表明,在研究的运行条件下,冷凝水不是问题。但是,在临界点附近,这种效果有望变得更加突出。尽管此分析的重点是用于碳捕获和封存(CCS)的超临界CO_2压缩机,但该方法可直接应用于其他非常规流体及其应用。

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  • 来源
    《Journal of turbomachinery》 |2015年第9期|091003.1-091003.13|共13页
  • 作者单位

    MIT Gas Turbine Laboratory, Massachusetts Institute of Technology, Cambridge, MA 02139;

    MIT Gas Turbine Laboratory, Massachusetts Institute of Technology, Cambridge, MA 02139;

    MIT Gas Turbine Laboratory, Massachusetts Institute of Technology, Cambridge, MA 02139;

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