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不同轴承壁面沟槽诱导油液穿透机理

刘红彬 刘公平 郝金华 杨梦科

刘红彬, 刘公平, 郝金华, 杨梦科. 不同轴承壁面沟槽诱导油液穿透机理[J]. 航空动力学报, 2019, 34(5): 1127-1136. doi: 10.13224/j.cnki.jasp.2019.05.019
引用本文: 刘红彬, 刘公平, 郝金华, 杨梦科. 不同轴承壁面沟槽诱导油液穿透机理[J]. 航空动力学报, 2019, 34(5): 1127-1136. doi: 10.13224/j.cnki.jasp.2019.05.019
Oil penetration mechanism induced by different bearing wall grooves[J]. Journal of Aerospace Power, 2019, 34(5): 1127-1136. doi: 10.13224/j.cnki.jasp.2019.05.019
Citation: Oil penetration mechanism induced by different bearing wall grooves[J]. Journal of Aerospace Power, 2019, 34(5): 1127-1136. doi: 10.13224/j.cnki.jasp.2019.05.019

不同轴承壁面沟槽诱导油液穿透机理

doi: 10.13224/j.cnki.jasp.2019.05.019
基金项目: 国家自然科学基金(U1404517); 工信部智能制造综合标准化项目(2017ZHZX04)

Oil penetration mechanism induced by different bearing wall grooves

  • 摘要: 以高速角接触球轴承为研究对象,在轴承外圈内壁开设沟槽,采用流体动力学对高速轴承壁面沟槽模型进行气液两相流数值模拟。利用VOF(volume of fluid)模型对轴承环间气液两相流界面进行动态捕捉,分析油液在沟槽诱导作用下的运动过程和分布特点,探究阻碍油液进入腔内的影响机理。分别研究了沟槽形状、深度、方向以及喷油参数等因素对高速轴承腔内和滚道润滑油体积分数的影响规律。研究结果表明:在高速轴承喷油润滑阶段,通过对沟槽形状、深度、方向的分析,得到圆弧形沟槽适用于高速轴承,沟槽深度为0.8 mm,沟槽方向为60°有利于油液进入轴承环间,腔内有效润滑油和外滚道油液体积分数最高。通过试验测得壁面有沟槽和无沟槽轴承腔内油液体积分数并与仿真结果对比,发现在轴承高速阶段开设壁面沟槽有利于润滑油进入轴承腔,为高速轴承的润滑设计提供了新的方法。

     

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出版历程
  • 收稿日期:  2018-11-23
  • 刊出日期:  2019-05-28

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