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NUMERICAL APPROACH FOR REAL GAS SIMULATIONS - PART II: FLOW SIMULATION FOR SUPERCRITICAL CO_2 CENTRIFUGAL COMPRESSOR

机译:实气模拟的数值方法 - 第二部分:超临界CO_2离心式压缩机的流模拟

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This paper is presented in two parts. Part I (Tabular fluid properties for real gas analysis) describes an approach to creating a tabular representation of the equation of state that is applicable to any fluid. This approach is applied to generating an accurate and robust tabular representation of the RefProp CO_2 properties. Part II (this paper) presents numerical simulations of a low flow coefficient supercritical CO_2 centrifugal compressor developed for a closed loop power cycle. The real gas tables presented in part I are used in these simulations. Three operating conditions are simulated near the CO_2 critical point: normal day (85 bar, 35C), hot day (105 bar, 50 C) and cold day (70 bar, 20C) conditions. The compressor is a single stage overhung design with shrouded impeller, 155 mm impeller tip diameter and a vaneless diffuser. An axial variable inlet guide vane (IGV) is used to control the incoming swirl into the impeller. An in-house three-dimensional computational fluid dynamics (CFD) solver named TACOMA is used with real gas tables for the steady flow simulations. The equilibrium thermodynamic modeling is used in this study. The real gas effects are important in the desired impeller operating range. It is observed that both the operating range (minimum and maximum volumetric flow rate) and the pressure ratio across the impeller are dependent on the inlet conditions. The compressor has nearly 25% higher operating range on a hot day as compared to the normal day conditions. A condensation region is observed near the impeller leading edge which grows as the compressor operating point moves towards choke. The impeller chokes near the mid-chord due to lower speed of sound in the liquid-vapor region resulting in a sharp drop near the choke side of the speedline. This behavior is explained by analyzing the 3D flow field within the impeller and thermodynamic quantities along the streamline. The 3D flow analysis for the flow near the critical point provides useful insight for the designers to modify the current compressor design for higher efficiency.
机译:本文以两部分介绍。第一部分(用于真实气体分析的表格流体性质)描述了一种形成适用于任何流体的状态等式的表格表示的方法。该方法应用于生成REFPROP CO_2属性的准确且坚固的表格表示。第二部分(本文)呈现了为闭环功率循环开发的低流量系数超临界CO_2离心压缩机的数值模拟。在第I部分呈现的真实气体表在这些模拟中使用。在CO_2关键点附近模拟了三种操作条件:正常日(85巴,35℃),炎热的一天(105巴,50℃)和寒冷的一天(70巴,20℃)条件。压缩机是一个单级横向设计,带有遮蔽的叶轮,155mm叶轮尖端直径和无差漫射器。轴向可变入口导向叶片(IGV)用于将进入的涡旋器控制到叶轮中。内部三维计算流体动力学(CFD)求解器命名为Tacoma,与真实的气体表一起使用,用于稳定流动模拟。本研究使用平衡热力学造型。实际气体效果在所需的叶轮操作范围内是重要的。观察到,操作范围(最小和最大体积流量)和叶轮上的压力比都取决于入口条件。与正常的日常条件相比,压缩机在炎热的一天中的操作范围近25%。在叶轮前缘附近观察到冷凝区域,随着压缩机的操作点朝向扼流圈移动而生长。由于液体蒸汽区域中的速度较低,导致中间沿中弦靠近中间叶片导致靠近速度线的窒息侧的急剧下降。通过沿着流线线分析叶轮内的3D流场和热力学量来解释该行为。临界点附近流量的3D流分析为设计人员提供了有用的洞察力,以便为更高效率修改电流压缩机设计。

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