临界流喷嘴式分液器两相流喷射的数值模拟

Numerical Simulation of Two-phase Flow Injection in Critical Flow Nozzle Separator

  • 摘要: 气液两相流制冷剂经过喷嘴后达到临界音速,形成气液两相对称分布的环状流流型,可以改善下游换热器各支路因压力不同造成的换热不均情况。采用Fluent软件对新型整流喷嘴分液器的临界流喷射过程进行了模拟研究。使用R507制冷剂,在喷嘴喉径不变、不同的入口压力条件下分别模拟了喷嘴收缩段、扩张段、喉部长度和出口直径变化对流动特性的影响。模拟结果表明:在入口压力3.2~4.0 MPa范围内,气液两相流制冷剂的喷射速度随入口压力增大而增大,最高速度增大了12.6%。当入口压力为3.6 MPa时,两相流制冷剂的喷射速度达到临界音速。气液两相流制冷剂经四组不同结构尺寸的喷嘴喷射后,速度均达到临界音速,并形成液相包裹气相且沿轴对称分布的环状流流型。研究可为临界流喷嘴的设计提供参考。

     

    Abstract: The gas-liquid two-phase flow refrigerant reaches the critical speed of sound after passing through the nozzle, forming an annular flow pattern with symmetrical distribution of the gas-liquid two phases, which can improve the uneven heat exchange caused by different pressures in each branch of the downstream heat exchanger.The critical flow injection process of the new rectifier nozzle liquid separator was simulated and studied by Fluent software.Using R507 re-frigerant, under the condition of constant nozzle throat diameter and different inlet pressures, the effects of nozzle constric-tion section, expansion section, throat length and outlet diameter changes on flow characteristics were simulated.The simu-lation results show that the injection velocity of the gas-liquid two-phase flow refrigerant increases with the increase of the inlet pressure within the inlet pressure range of 3.2 to 4.0 MPa, and the maximum velocity increases by 12.6%.When the inlet pressure is 3.6 MPa, the injection velocity of the two-phase flow refrigerant reaches the critical speed of sound.After the gas-liquid two-phase flow refrigerant is sprayed through four groups of nozzles with different structural sizes, the speed of the injection all reaches the critical sound velocity, and an annular flow pattern is formed in which the liquid phase surrounds the gas phase and is symmetrically distributed along the axis.The research can provide reference for the design of critical flow nozzle.

     

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