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局部多孔质气浮止推轴承特性研究 被引量:2

Study of the Characteristics of Partial Porous Air Thrust Bearing
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摘要 在考虑轴承气膜交界面处切向速度滑移的条件下,建立了局部多孔质气浮止推轴承的理论模型,然后使用有限元算法进行了数值仿真,仿真的结果与试验结果取得了一定程度的一致性,说明此新的修改了的雷诺方程可以用来作为局部多孔质气浮止推轴承研究的理论模型。利用该模型,能够成功计算出不同渗透系数、不同厚度及不同直径的局部多孔质气浮轴承的流量、承载及刚度。还从理论上与小孔类型及全多孔质类型的气浮轴承特性进行了对比,结果表明,局部多孔质气浮轴承有着优良的特性及很好的应用前景。 A nonlinear model based on the finite element method is provided to compute the static characteristics of partial porous gas thrust bearing, considering the tangential velocity slip at the bearing-film interface. Good agreement is achieved between theoretical and experimental results on static load capacity, mass flow and static stiffness. The new modified Reynolds equation is proved to be a proper model to investigate the characteristics of cxternally pressurized partial porous gas thrust bearing. With a change to the feeding parameters of permeability coefficient, height or diameter of partial porous restrictors, the effect of the steady state characteristics, such as mass rate of flow, load capacity and static stiffness are studied, Also the performance comparison among the thrust beatings with orifice restrictors, partial porous restrictors and whole porous restrictors shows that this kind of beating has promising potential in application.
出处 《国防科技大学学报》 EI CAS CSCD 北大核心 2007年第6期106-111,共6页 Journal of National University of Defense Technology
基金 国家自然科学基金重点资助项目(50535020)
关键词 多孔质轴承 气浮轴承 有限元法 速度滑移 多孔质 porous beating aerostafie bearing finite element method slip velocity porous
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参考文献5

  • 1Kwan Y B P, Corbett J. A Simplified Method for the Correction of Velocity Slip and Inertia Effects in Porous Aerostatic Thrust Bearing[J]. Tribology Instrumental, 1998,31 (12).
  • 2Tian Y. Static Study of the Porous Bearings by the Simplified Finite Element Analysis[J]. Wear, 1998,218:203 -209.
  • 3Fourka M, Bonics M. Comparison between Externally Pressurized Gas Thrust Bearings with Different Orifice and Porous Feeding Systems[J]. Wear, 1997,210: 311 - 317.
  • 4王建敏,戴一帆,李圣怡.局部多孔质气浮轴承的有限元方程收敛算法研究[J].中国机械工程,2006,17(5):474-477. 被引量:3
  • 5Yoshimoto S. An Aerostatic Thrust Bearing with a Stiffness of 1 N* nm^- 1 [ j]. Nanotechnology, 1996,7 : 52 - 57.

二级参考文献3

  • 1程雪梅,陈海斌,张显全.空气静压轴承工作特性的有限元分析[J].渝州大学学报,1996,13(3):18-24. 被引量:1
  • 2Luong T S,Potze W,Post J B,et al.Numerical and Experimental Analysis of Aerostatic Thrust Bearings with Porous Restrictors.Tribology International,2004,37:825~832
  • 3Tian Y.Static Study of the Porous Bearings by the Simplified Finite Element Analysis.Wear,1998,218:203~209

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