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A STUDY ON TEMPERATURE SEPARATION IN THE VORTEX TUBE

机译:涡旋管温度分离研究

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This paper reports that increasing the number of inlet nozzles in both insulated and non-insulated vortex tubes affects the temperature distribution and causes temperature reduction in the counter flow vortex tube. From experiments with vortex tubes of 16 mm diameter and cold orifice diameter of 0.5D, we found the maximum temperature reductions at the core for 1,2 and 4 inlet nozzles respectively to be -16°C, -29°C and -30°C. In addition, the cold air temperature drop from employing the snail is higher than those from employing the tangential inlet with 1, 2, and 4 nozzles at the same inlet pressure. For applying the snail to the vortex tube, the maximum cold air temperature reduction and the isentropic efficiency are found to be 33°C and 36%, respectively. Applying dimensional analysis and similarity geometry yielded an empirical correlation for use in designing vortex tubes for optimal performance.
机译:本文报道,增加绝缘和非绝缘涡管中的入口喷嘴数量影响温度分布并导致逆流涡管中的温度降低。从涡流管的实验,直径为16毫米和冷孔直径0.5d,我们发现分别为-16°C,-29°C和-30°的1,2和4入口喷嘴处的芯处的最大温度降低C。另外,采用蜗牛的冷空气温度降高于采用相同入口压力的切向入口的切向入口的冷空气温度降低。为了将蜗牛施加到涡旋管,发现最大的冷空气降低和常规效率分别为33°C和36%。施加尺寸分析和相似性几何形状产生了用于设计涡管以获得最佳性能的经验相关性。

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