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弹性均压槽空气静压轴承静特性的影响因素分析
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国家自然科学基金项目(51705390);西安工业大学科研创新团队建设计划项目.


Analysis on the Influence Factors of Aerostatic Thrust Bearing with Elastic Equalizing Pressure Groove
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    摘要:

    为了研究影响弹性均压槽空气静压轴承静态特性的因素,基于气固耦合原理,建立弹性均压槽空气静压轴承的耦合控制方程,采用有限差分对控制方程进行离散求解,分别研究供气压力、均压槽宽度和节流孔直径对弹性均压槽空气静压轴承静态特性的影响。结果表明:供气压力、均压槽宽度和节流孔直径对弹性均压槽空气静压轴承承载力和刚度的影响较大,供气压力越大,轴承的承载力和刚度也越大,但刚度最大时的工作气膜间隙越小;均压槽宽度越大,轴承刚度最大时的工作气膜间隙越大;节流孔直径越小,轴承刚度越大。实验结果和理论计算结果基本一致,验证了数学模型和理论方法的正确性。

    Abstract:

    In order to study the factors affecting the static characteristics of aerostatic bearings with elastic equalizing pressure groove,based on the principle of gassolid coupling,the coupling control equation of aerostatic bearings with elastic equalizing pressure groove was established.The governing equation was solved by finite difference method.The effects of supply pressure,the width of equalizing pressure groove and the diameter of throttle hole on the static characteristics of aerostatic bearings with elastic equalizing pressure groove were studied respectively.The results show that the pressure of supply gas,the width of equalizing pressure groove and the diameter of throttle hole have great influence on the bearing capacity and stiffness of aerostatic bearing with elastic equalizing groove.The bigger the pressure of supply gas,the bigger the bearing capacity and stiffness,but the smaller the working gas film gap is when the stiffness is maximum.The bigger the width of equalizing pressure groove,the bigger the working gas film gap is when the bearing stiffness is maximum.The smaller the bearing stiffness is,the bigger the bearing stiffness is.The theoretical simulation results were verified by experiments,the theoretical simulation results are basically consistent with the experimental results,which verifying the correctness of mathematical model and theoretical method.

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赵晓龙,张君安,董皓,刘波.弹性均压槽空气静压轴承静特性的影响因素分析[J].润滑与密封,2019,44(2):34-38.
. Analysis on the Influence Factors of Aerostatic Thrust Bearing with Elastic Equalizing Pressure Groove[J]. Lubrication Engineering,2019,44(2):34-38.

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  • 在线发布日期: 2019-07-04
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