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AN EXPERIMENTAL INVESTIGATION OF THE OPTIMUM GEOMETRY OF TWO NOZZLE COUNTER FLOW VORTEX TUBE

机译:两个喷嘴计数器涡管最佳几何形状的实验研究

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An experimental study of two nozzle Ranque-Hilsch vortex tube are carried out with air as the working medium. Performance of the vortex tube is measured by varying the operating and geometric parameters such as L/D ratio, cold mass fraction, operating pressure and cold end orifice diameter and number of nozzles. Three Cold end orifices diameters 3 mm, 4 mm and 5 mm are tested with three L/D ratios vortex tubes 12.5, 13.5 and 17.5. Inlet pressure is varied from 2 bar to 8 bar with the increment of 1 bar. It was found that for 4 mm cold end orifices diameter brings maximum cold end temperature drop of 25~0 C. It is observed that cold end temperature drop in case of double nozzle is better than that of with single nozzle. Maximum temperature drop is obtained with cold mass fraction in the range of 0.45 to 0.55 for the cases, single nozzle and double nozzles. Vortex tube with L/D ratio 17.5 performs better than other two chosen L/D ratios.
机译:对两个喷嘴Ranque-Hilsch涡流管的实验研究用空气作为工作介质进行。通过改变操作和几何参数,例如L / D比,冷质量分数,操作压力和冷端孔直径和喷嘴数来测量涡流管的性能。三个冷端径直径3mm,4mm和5mm,用三个L / D比涡管12.5,13.5和17.5进行测试。入口压力从2巴到8巴不同,增量为1巴。发现,对于4毫米冷端孔口直径带来了25〜0℃的最大冷端温度下降。观察到双喷嘴的冷端温度下降比单个喷嘴更好。对于壳体,单个喷嘴和双喷嘴,在0.45至0.55的冷质量分数中获得最大温度降。具有L / D比的涡旋管17.5比其他两种所选择的L / D比率更好。

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