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NUMERICAL ANALYSIS OF DRY GAS FACE SEALS WITH SPIRAL GROOVE AND INNER ANNULAR GROOVE

机译:用螺旋槽和内环形槽的干气面密封件数值分析

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A two-dimensional Reynolds equation was established for isothermal compressible gas between the two faces of a dry gas face seal with both spiral grooves and an inner annular groove onto the hard face. The opening force, the leakage rate, the axial film stiffness and the film stiffness to leakage ratio were calculated by finite element method. The comparisons with the sealing performances of a typical gas face seal only with spiral grooves onto its hard face were made. The effects of the face geometric parameters on the static behavior of such a seal were analyzed. The optimization principle for geometric parameters of a dry gas face seals with spiral grooves and an inner annular groove was presented. The recommended geometric parameters of spiral grooves and circular groove presented by optimization can ensure larger axial stiffness while lower leakage rates.
机译:在干燥气体面密封的两个面之间为等温可压缩气体建立了二维雷诺式方程,用螺旋槽和内部环形槽到硬面上。通过有限元方法计算开启力,泄漏速率,轴向膜刚度和膜刚度与泄漏比率。制造了仅利用螺旋槽的典型气体面密封的密封性能的比较。分析了面部几何参数对这种密封的静态行为的影响。提出了一种用螺旋槽和内环形槽的干气面密封件的几何参数的优化原理。通过优化提供的螺旋槽和圆形槽的推荐几何参数可以确保较大的轴向刚度,而较低的泄漏速率。

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