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Turbulence measurements of high shear flow fields in a turbomachine seal configuration

机译:涡轮机密封结构中高剪切流场的湍流测量

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摘要

The mean velocity and Reynolds stress tensor throughout a whirling annular seal are presented. The data was collected with a three dimensional laser Doppler velocimeter using phase averaging. Two axial flow conditions (Re = 12,000 and 24,000) were studied at one shaft speed (Ta = 6,600). The eccentricity and whirl ratios were 50 and 100 percent, respectively. There is a region of high axial momentum in this region is higher in the low Reynolds number case due to an axial recirculation zone that occurs on the suction side of the rotor at the inlet. The recirculation zone does not occur in the high Reynolds number case. At both Reynolds numbers, there is a recirculation zone on the rotor surface in the pressure side of the inlet. This recirculation zone extends from 20 to 200 degrees rotor zenith in the tangential direction, and is one third of a clearance wide radially. The high Reynolds number recirculation zone is 1.5 mean clearances long, while the low Reynolds number zone extends 2 mean clearances downstream. When compared to previous studies, it is apparent that the tangential momentum is no greater for a seal with whirl than for one without if other parameters are constant. Areas of high tangential momentum occur in the clearance where the axial momentum is low. Average exit plane tangential velocities in the high Reynolds number case are 1.5 times greater than those in the other flow case. These results are in general agreement with predictions made by other investigators.
机译:给出了整个旋转环形密封件的平均速度和雷诺应力张量。使用三维激光多普勒测速仪,使用相位平均来收集数据。在一个轴转速(Ta = 6,600)下研究了两种轴向流动条件(Re = 12,000和24,000)。偏心率和涡流率分别为50%和100%。在低雷诺数的情况下,在该区域中存在较高的轴向动量,这是由于在进口的转子吸入侧出现了轴向回流区域。在高雷诺数情况下不会出现回流区。在两个雷诺数下,入口压力侧的转子表面上都有一个回流区。该再循环区域在切线方向上从20到200度的转子天顶延伸,并且是径向间隙的三分之一。高雷诺数再循环区的平均间隙长为1.5,而低雷诺数再循环区的下游平均间隙长2。与以前的研究相比,很明显,带有涡旋的密封件的切向动量不大于没有其他参数恒定的情况下的切向动量。切向动量高的区域出现在轴向动量低的游隙中。在高雷诺数情况下,平均出口平面切向速度是在其他流动情况下的1.5倍。这些结果与其他研究者的预测基本一致。

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