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Influences of various orifice layouts on the properties of aerostatic journal bearings based on finite element method

机译:各种孔口布局对基于有限元法的航空轴颈轴承性能影响

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It is essential to thoroughly investigate influences of orifice layouts on properties of aerostatic journal bearings employed in ultra-high speed spindles.In this paper,four orifice layouts of aerostatic journal bearings which have a large length-diameter ratio are designed and investigated,particularly in light of the nonlinear compressible Reynolds equation and the associated computational analysis and algorithms using the FEM-based Galerkin weighted residual method.A series of pressure distributions as well as the load capacity,attitude angle,volume flow rate and air film stiffness of the aerostatic journal bearings for the cases of four orifice layouts are analysed with respect to different rotational speeds and eccentricity ratios.It can be concluded that increasing orifice sets is not beneficial to enhance the performance of the aerostatic journal bearing.The aerostatic journal bearing divided into two identical independent aerostatic journal bearings has relative optimal performance at rotational speeds from 0 r/min to 160,000 r/min,such as the highest load capacity,the lowest attitude angle and modest air film stiffness,however,with consumption of the largest quantities of pressurized gas.The designers can use the analysis results to optimize the orifice layout for improving the performance of the aerostatic journal bearing.
机译:彻底调查关于在超高速采用气体静压轴颈轴承性能孔口布局的影响是很重要spindles.In本文的具有大的长度 - 直径比气体静压轴颈轴承4点孔的布局的设计和研究,特别是在非线性可压缩雷诺方程和相关联的计算分析和使用基于FEM-的Galerkin算法的光加权残差method.A系列压力分布的以及所述负载容量,姿态角,体积流量和空气薄膜的刚度的空气静力轴颈针对不同的转速和偏心比分析了四个孔口布局的轴承。可以得出结论,越来越多的孔板没有利用增强空气静力学轴颈轴承的性能。空气静力轴颈轴承分为两个相同的独立性空气静力学轴颈轴承具有相对最佳的表现以0 r / min的转速为160,000 r / min的ance,例如最高负载能力,最低的姿态角度和适度的空气薄膜刚度,但是由于最大量的加压气体消耗。设计人员可以使用该分析结果优化孔口布局以改善空气静力学轴颈轴承的性能。

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