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Numerical and experimental analysis of aerostatic thrust bearings with porous restrictors

机译:多孔限流器空气静力推力轴承的数值与实验分析

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摘要

The finite element method is used to predict the performance of aerostatic thrust bearings with a complete porous surface. Results obtained by a ID and 3D source flow model derived from D'Arcy's law are compared for rectangular porous bearings having an infinite width. It turns out that the ID source flow model is adequate for practical design parameters, For a circular aerostatic porous thrust bearing results calculated with several mathematical models for the source flow and slip flow are compared with experimental results. A relatively simple model incorporating unflatness and deformation of the bearing surface correlates well with the experimentally determined bearing performance.
机译:有限元方法用于预测具有完整多孔表面的空气静力推力轴承的性能。对于具有无限宽度的矩形多孔轴承,比较了从D'Arcy定律得出的ID和3D源流模型获得的结果。事实证明,ID源流模型足以满足实际设计参数的要求,对于圆形空气静力多孔推力轴承,利用几种数学模型对源流和滑移流计算的结果与实验结果进行了比较。结合了轴承表面的不平坦度和变形的相对简单的模型与实验确定的轴承性能有很好的关联。

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