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特大型双排四点接触球轴承承载能力的研究 总被引:1,自引:0,他引:1
给出特大型双排四点接触球轴承承载曲线的精确计算方法。绘制其静承载曲面,并对精确静承载曲线及简化静承载曲线进行比较。分析轴承游隙、沟曲率半径系数及原始接触角对静承载曲线的影响。结果表明:随着轴承负游隙绝对值的增大,轴承所能承受的最大倾覆力矩增大,最大轴向力减小。游隙在–0.2~0 mm范围内取值,对轴承承载能力的影响较小。沟曲率半径系数对轴承承载能力影响较大,随着轴承沟曲率半径系数的增大,轴承静承载能力减小。随径向力增加,轴承承载能力随接触角增大先增大后减小。 相似文献
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The friction coefficients between the surfaces of a ball and a disc lubricated by a space lubricating oil No.4129 were measured at various operating conditions on a ball-disc friction test rig. Friction characteristic curves were obtained under sliding and rolling movements at point contact. A new model for calculation of the friction coefficient was presented. The results show that the bigger the load is, the larger the friction coefficient becomes. The rolling speed ranging from 1 m/s to10 m/s has an important effect on the friction coefficient. The friction coefficient increases with the increase in sliding speed and the decrease in rolling speed. The linear variation region of the friction coefficient versus the sliding speed at high rolling speed is wider than that at low rolling speed. The model for calculation of the friction coefficient is accurate for engineering use. 相似文献
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在自行研制的模拟航天轴承的摩擦力试验机上,对4129航天润滑油进行了摩擦特性分析。对该润滑油在实际高低温工况下的黏度进行了测量。分析了温度、滚动速度和滑动速度与该油摩擦系数的关系,建立了该航天润滑油的黏温模型、摩擦系数计算模型。研究结果表明:当温度小于0 ℃时,4129航天润滑油黏度随温度的变化非常大;温度大于30 ℃时,其黏度随温度的变化较小。当滑动速度小于0.3 m/s时,该油摩擦系数随滑动速度近似线性增加;当滑动速度大于0.3 m/s时, 摩擦系数随着滑动速度的增加呈非线性增加;当滑动速度大于1 m/s之后,摩擦系数随滑动速度增加基本保持不变。摩擦系数随油温的增加而减小。当滚动速度从1 m/s增加到3 m/s时,油的摩擦系数迅速下降,随着滚动速度继续增加,摩擦系数下降缓慢直到达到最小值,然后基本保持不变。 相似文献