ISSN   1004-0595

CN  62-1224/O4

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氦气-空气混合环境中微型螺旋槽止推气浮轴承的承载特性分析

Analysis on the Bearing Characteristics of Gas-Lubricated Spiral-Groove Thrust Micro-Bearings in Helium-Air Gas Mixtures

  • 摘要: 针对氦气-空气混合气体环境,分析了不同氦气体积含量下混合气体的黏度和分子平均自由程,利用有限单元法求解雷诺方程二阶滑移修正模型,计算了微型螺旋槽气浮轴承的气压和气膜厚度,研究了氦气体积含量、螺旋槽深度和转速对气浮轴承承载能力的影响. 分析结果表明:当螺旋槽深度由1 μm增至10 μm时,气浮轴承的气膜厚度先增加后减小,槽深为5 μm时,气膜厚度最大,气浮轴承的承载能力最佳. 此外,当槽深小于5 μm时,混合气体的分子平均自由程对气膜厚度的影响较大;当槽深大于5 μm时,混合气体黏度的影响起主导作用.

     

    Abstract: The mean free path and the viscosity of helium-air gas mixtures were calculated as a function of the helium fraction. The second-order-slip modified Reynolds equation was solved using the finite element method. The hydrodynamic pressure and film thickness of the micro-bearing were obtained. The effects of helium fraction, groove depth and angular velocity on the bearing characteristics of the micro-bearing were investigated. The results show that when the groove depth increased from 1 μm to 10 μm, the film thickness of the micro-bearing firstly increased and then decreased, reaching a maximum at the groove depth of 5 μm, which represented an optimum bearing capacity. In addition, at a groove depth less than 5 μm, the mean free path of the gas mixtures had a dominant effect on the film thickness of the micro-bearing. However, when the groove depth was larger than 5 μm, the effect of the gas viscosity dominated.

     

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