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Numerical analysis of the effect of helical nozzles gap on the cooling capacity of Ranque-Hilsch vortex tube

机译:螺旋喷嘴间隙对Ranque-Hilsch涡流管冷却能力影响的数值分析

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摘要

In this article, the effect of helical nozzles on both energy separation and refrigeration phenomena in the Ranque-Hilsch Vortex Tube (RHVT) was investigated by CFD techniques. The radial gap of inlet of helical nozzle from the vortex chamber (GPL) stands as a significant designing parameter. The standard k-ε turbulence model was introduced to the governing equations for analyzing highly rotating complex flow field. The studied helical nozzles have the same profile shape but their radial distance from the chamber distinct them from each other. Presented numerical results show that operating the vortex tube with GPL = 0.034 leads to the maximum cooling effect and swirl velocity. Furthermore, by keeping GPL value constant, the effect of number of nozzles is studied in more detail. Present results in this article, show increasing of temperature separation due to increase of nozzle numbers, however the coefficient of performance (COP) does not change very significantly.
机译:在本文中,通过CFD技术研究了螺旋喷嘴对Ranque-Hilsch涡流管(RHVT)中能量分离和制冷现象的影响。螺旋喷嘴从涡流室(GPL)进入的径向间隙是重要的设计参数。将标准k-ε湍流模型引入到控制方程中,以分析高旋转复杂流场。所研究的螺旋形喷嘴具有相同的轮廓形状,但它们与腔室的径向距离使它们彼此不同。给出的数值结果表明,在GPL = 0.034的条件下操作涡流管会导致最大的冷却效果和涡旋速度。此外,通过保持GPL值恒定,可以更详细地研究喷嘴数量的影响。本文中的当前结果表明,由于喷嘴数量的增加,温度分离的程度有所提高,但是性能系数(COP)不会发生很大变化。

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