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首页> 外文期刊>Journal of the Balkan Tribological Association >SKIDDING ANALYSIS OF HIGH-SPEED AND LIGHT-LOAD ROLLER BEARING BASED ON MODIFIED FILM THICKNESS FORMULA AND CONSIDERING BEARING WHIRL WITH ELLIPTICAL ORBIT
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SKIDDING ANALYSIS OF HIGH-SPEED AND LIGHT-LOAD ROLLER BEARING BASED ON MODIFIED FILM THICKNESS FORMULA AND CONSIDERING BEARING WHIRL WITH ELLIPTICAL ORBIT

机译:基于修正膜厚公式并考虑椭圆轨道的旋转轴承的高速轻载滚子轴承的滑动分析

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In order to obtain the more accurate film thickness formula to assist in the skidding analysis of high-speed and light-load roller bearings (HSLLRBs), the oil film characteristics of HSLLRBs under slip conditions were analysed. Moreover, the ellipse is adopted to be the whirl orbits, which is more close to real whirling orbit than the circular orbit in practice. Based on the oil film thickness modified formula, an analytical model was built by taking bearing whirl with elliptical orbit into account, and the skidding mechanism was investigated in terms of various factors such as whirl orbit, radial load, lubricating oil viscosity and roller diameter. The results showed that whirl often exacerbates skidding failure to HSLLRBs, and the degree of skidding is directly correlated with the whirl radius, especially the X-radius. Effects of different oil film thickness formulas on skidding of rolling bearing are different, Dowson 1977 modified film thickness formula is more fit to provide assistance in the skidding analysis of HSLLRBs. As radial load increase or the roller diameter decrease, the influence of whirling on bearing skid and the degree of skidding decrease. Therefore, for minishing skid so as to improve HSLLRBs service life and reliability, the whirl radius (especially the X-radius) and roller diameter should be decreased, whereas the radial load should be increased moderately. The final purpose of this study is to support the failure mechanism and vibration analysis of HSLLRBs.
机译:为了获得更准确的膜厚公式,以辅助高速和轻载滚子轴承(HSLLRB)的打滑分析,分析了HSLLRB在滑移条件下的油膜特性。此外,采用椭圆作为旋涡轨道,实际上比圆形旋涡更接近真实的旋涡轨道。在油膜厚度修正公式的基础上,建立了一个带有椭圆轨道的轴承涡流分析模型,并根据涡流轨道,径向载荷,润滑油粘度和滚子直径等因素研究了打滑机理。结果表明,旋风通常会加剧HSLLRB的滑移破坏,滑移的程度与旋风半径(尤其是X半径)直接相关。不同的油膜厚度公式对滚动轴承打滑的影响是不同的,Dowson 1977年修改的膜厚度公式更适合为HSLLRB的打滑分析提供帮助。随着径向载荷的增加或滚子直径的减小,回旋对轴承打滑和打滑程度的影响减小。因此,为了减少打滑以提高HSLLRB的使用寿命和可靠性,应减小涡流半径(尤其是X半径)和滚子直径,而应适当增加径向载荷。这项研究的最终目的是支持HSLLRB的失效机理和振动分析。

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