首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers, Part C. Journal of mechanical engineering science >Investigation on influences of herringbone grooves for the aerostatic journal bearings applied to ultra-high-speed spindles
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Investigation on influences of herringbone grooves for the aerostatic journal bearings applied to ultra-high-speed spindles

机译:人字形沟槽对超高速轴承空气静力轴颈轴承影响的研究

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摘要

Aerostatic bearings are the core parts of ultra-high-speed spindles with maximum running speed greater than 100,000 r/min. In this paper, the influences of herringbone grooves on the performance of aerostatic journal bearings are studied to design spindles with the features of higher precision and higher speed. Parametric studies and sensitivity analyses are executed in terms of the improved finite element method, which is specially developed to solve the compressible Reynolds equation for herringbone grooved air bearings. The calculated results indicate that herringbone grooves significantly improve the performance of aerostatic journal bearings under the conditions of ultra-high speeds and low supply pressures. Groove parameters are nonlinear dependent, and groove depth and length are the dominant influential factors for the load capacity at speed of 200,000 r/min. Experiments are designed and conducted to verify the improved finite element method, which show that the improved finite element method can be used to analyze the influences of herringbone grooves on aerostatic journal bearings and also manifest that suitable herringbone groove geometrical parameters can obviously decrease spindle radial runouts at ultra-high speeds.
机译:空气轴承是超高速轴的核心部分,最大运行速度大于100,000 r / min。在本文中,研究了人字形沟槽对航空轴颈轴承性能的影响,设计了具有更高精度和更高速度的特征的主轴。参数研究和敏感性分析是在改进的有限元方法方面执行的,这是专门开发的,以解决人字形沟槽空气轴承的可压缩雷诺方程。计算结果表明,人字形槽在超高速度和低供电压力条件下显着提高了航空轴颈轴承的性能。凹槽参数是非线性相关的,凹槽深度和长度是负载能力以200,000 r / min的速度的主导影响因素。设计并进行了实验以验证改进的有限元方法,表明改进的有限元方法可用于分析人字形槽对空气静力轴颈轴承的影响,并且还表明合适的人字形槽几何参数可以明显减少主轴径向跳动以超高速度。

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