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A NUMERICAL AND EXPERIMENTAL STUDY OF WINDBACK SEALS

机译:风挡密封的数值和实验研究

摘要

Windback seals work similarly to labyrinth seals except for the effect of helicalgroove. These seals are essentially a tooth on stator or tooth on rotor labyrinth sealwhere the grooves are a continuous helical cut like a thread. Windback seals are used incentrifugal gas compressor to keep oil out of the gas face seal area. These face sealscannot be contaminated by oil. A purge gas is applied to the seal to help force the oilback into the bearing area.The windback seal should be designed to prevent any oil contamination into thesupply plenum and to reduce purge gas leakage. The CFD simulations have beenperformed with the effect of clearance, tooth width, cavity shape, shaft rotation,eccentricity, and tooth location on the seal leakage performance and the flow field insidethe seal. The leakage flow rate increases with increasing the pressure differential, rotorspeed, radial clearance, cavity size, and shaft diameter and with decreasing the toothwidth. The eccentricity has a minimal effect for the windback seal. From oil simulations,the windback seal with 25% rotor eccentricity has some of the journal bearing action anddrives back flow into the gas plenum. However the windback seal can be used to force the oil back into the bearing side before starting the compressor by applying a purge gasflow since the positive axial velocity inside the cavity is larger than the negative axialvelocity. m A Rw cav & / ? is constant for varying shaft rotation since the leakage flow ratefor the windback seal increases linearly as the the rotor speed increases. The leakageflow rate for the windback seal increases as the groove size increases due to the pumpingaction of the windback seal. A windback seal design based upon the numericalsimulations that minimize gas leakage and help prevent gas face seal oil contaminationwas optimized.The windback seal has two leakage flow paths. Since the leakage flow rate underteeth of windback seals is the same as for a similar geometry labyrinth seal, the flowunder the teeth can be predicted by two-dimensional labyrinth seal analysis. Anempirical model for the leakage rate through the cavity has been developed which fitsthe data with a standard deviation of 0.12.
机译:除螺旋槽的作用外,回风密封件的工作方式与迷宫式密封件类似。这些密封件实质上是定子上的齿或转子迷宫式密封上的齿,其中凹槽是像螺纹一样的连续螺旋形切口。回旋密封件用于离心式气体压缩机,以防止油进入气面密封件区域。这些端面密封垫不会被油污染。向密封件施加吹扫气以帮助将回油压入轴承区域。反吹密封件的设计应防止任何油污进入供气室并减少吹扫气的泄漏。在间隙,齿宽,腔体形状,轴旋转,偏心率和齿位置对密封件泄漏性能和密封件内部流场的影响下执行了CFD仿真。泄漏流量随着压差,转子速度,径向间隙,腔尺寸和轴直径的增加以及齿宽的减小而增加。偏心对反吹密封的影响最小。根据油的模拟,转子偏心率为25%的反吹密封件具有一些轴颈轴承作用,并带动回流进入气室。但是,由于空腔内部的正轴向速度大于负轴向速度,因此回风密封件可通过施加吹扫气流用于在启动压缩机之前将油压回到轴承侧。 m A Rw cav&/?随轴转速的变化,常数是恒定的,因为回旋密封件的泄漏流量会随着转子速度的增加而线性增加。由于凹槽的尺寸由于反吹密封件的泵送作用而增加,反吹密封件的泄漏流量增加。基于数值模拟的反吹密封设计可以最大程度地减少气体泄漏并有助于防止气密面油被污染。反吹密封具有两个泄漏流路。由于回风密封件的齿的泄漏流量与类似几何迷宫式密封件的泄漏流量相同,因此可以通过二维迷宫式密封分析来预测齿下的流量。已经开发了通过型腔泄漏率的经验模型,该模型拟合数据的标准偏差为0.12。

著录项

  • 作者

    Lim Chae H.;

  • 作者单位
  • 年度 2010
  • 总页数
  • 原文格式 PDF
  • 正文语种 en_US
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