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Study on the Gas Film Flow Field and its Influencing Factors at the Outlet of the Orifice of the Aerostatic Bearing

机译:气膜流场及其在孔静压轴承孔口出口的影响因素研究

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In order to further explore and study the influencing factors and regulars of the gas film flow field at the outlet of the orifice of the aerostatic bearing, the large eddy simulation method was used to calculate the N-S equation in the calculation area of the gas film flow field at the outlet of the orifice of the aerostatic bearing, and the overrelaxation iteration method was used to solve the Reynolds equation in the other calculation areas, which was proposed in this paper. Based on the physical model of the outlet of the orifice of the aerostatic bearing, the solution area of the gas film flow field of the aerostatic bearing was solved, and the calculation results were analyzed and discussed. The results showed that there was a sharp drop of the gas film pressure at the outlet of the orifice of the aerostatic bearing and the separation of the gas film pressure p became inconsistent in the thickness direction of gas film clearance h. It was assumed that there was a critical ratio θ between the gas film clearance h and the orifice diameter d of the aerostatic bearing, and when the ratio of gas film clearance h to the orifice diameter d was greater than the critical ratio θ, various fluctuations of the gas film flow field began to appear, which may be the initial signal state of the gas film flow field of the aerostatic bearing starting to transition to turbulence. It provided a theoretical basis and guidance for further study of the transition lubrication mechanism between the laminar and the turbulent flow at the outlet of the orifice of the aerostatic bearing in this paper.
机译:为了进一步探索和研究空气静止轴承的孔口的出口处的气膜流场的影响因素和常规,使用大的涡模拟方法来计算气体膜流量的计算面积中的NS方程在空气静止轴承的孔口的出口处,使用过度迭代方法来解决本文提出的其他计算区域中的雷诺等式。基于空气静止轴承的孔口的出口的物理模型,解决了空气膜轴承的气体膜流场的溶液面积,分析并讨论了计算结果。结果表明,空气膜轴承的孔口的出口处存在急剧下降,并且气体膜压力P的分离在气体膜间隙H的厚度方向上变得不一致。假设气体膜间隙H和空气膜轴承的孔口直径D之间存在临界比θ,并且当气膜间隙H与孔口直径d的比率大于临界比θ时,各种波动气体膜流场开始出现,其可以是航空轴承的气体膜流场的初始信号状态,该轴承轴承开始过渡到湍流。它提供了一种理论基础和指导,进一步研究了本文的空气静止轴承出口处的层状和湍流之间的过渡润滑机构。

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