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圆柱滚子轴承V形兜孔形面的磨损性能

桑得雨 刘延斌 孙秀照 邓增辉

桑得雨, 刘延斌, 孙秀照, 等. 圆柱滚子轴承V形兜孔形面的磨损性能[J]. 航空动力学报, 2023, 38(2):473-481 doi: 10.13224/j.cnki.jasp.20210414
引用本文: 桑得雨, 刘延斌, 孙秀照, 等. 圆柱滚子轴承V形兜孔形面的磨损性能[J]. 航空动力学报, 2023, 38(2):473-481 doi: 10.13224/j.cnki.jasp.20210414
SANG Deyu, LIU Yanbin, SUN Xiuzhao, et al. Wear performance of geometric parameters of V-shape pocket of cylindrical roller bearing[J]. Journal of Aerospace Power, 2023, 38(2):473-481 doi: 10.13224/j.cnki.jasp.20210414
Citation: SANG Deyu, LIU Yanbin, SUN Xiuzhao, et al. Wear performance of geometric parameters of V-shape pocket of cylindrical roller bearing[J]. Journal of Aerospace Power, 2023, 38(2):473-481 doi: 10.13224/j.cnki.jasp.20210414

圆柱滚子轴承V形兜孔形面的磨损性能

doi: 10.13224/j.cnki.jasp.20210414
基金项目: 河南省自然科学基金(182300410273)
详细信息
    作者简介:

    桑得雨(1995-),男,硕士生,主要从事滚动轴承保持架设计及理论研究

    通讯作者:

    刘延斌(1971-),男,教授、硕士生导师,博士,主要从事滚动轴承动力学研究。E-mail: liuyb2018@163.com

  • 中图分类号: V233.4+5;TH113

Wear performance of geometric parameters of V-shape pocket of cylindrical roller bearing

  • 摘要:

    为研究高速轻载工况下兜孔形面几何参数对V形兜孔圆柱滚子轴承保持架磨损性能的影响,建立了考虑兜孔处润滑影响的轴承动力学模型。以基于Masjedi磨损模型的时间平均磨损率作为磨损性能的评价标准,研究了兜孔形面几何参数对V形兜孔保持架磨损性能的影响规律,分析了在不同转速下兜孔壁倾角均为15°的V形兜孔保持架的磨损性能及打滑特性。结果表明:兜孔形面几何参数对保持架的磨损性能影响显著,通过对其优化可有效提升保持架的磨损性能;保持架的时间平均磨损率随内圈转速的增加而上升;在内圈转速的范围为5000~20000 r/min时,兜孔壁倾角均为15°的V形兜孔保持架的时间平均磨损率和打滑率均低于普通直兜孔轴承。

     

  • 图 1  V形兜孔的结构及参数示意图

    Figure 1.  Structure and parameters diagram of V-shape pocket

    图 2  滚子与兜孔的接触模型

    Figure 2.  Contact model of roller and pocket

    图 3  滚子与兜孔的接触刚度、阻尼及其接触区

    Figure 3.  Contact stiffness,damping and area of roller and pocket

    图 4  滚子与兜孔的等效接触刚度和阻尼

    Figure 4.  Equivalent contact stiffness and damping of the roller and pocket

    图 5  保持架打滑率在不同内圈转速下的变化曲线(径向载荷为2100 N)

    Figure 5.  Variation curves of cage slip rate under different inner ring rotational speeds (radial load is 2100 N )

    图 6  保持架打滑率在不同径向载荷下的变化曲线(内圈转速为7000 r/min)

    Figure 6.  Variation curves of cage slip rate under different radial loads (inner ring rotational speed is 7000 r/min)

    图 7  各个壁倾角取不同值时的时间平均磨损率

    Figure 7.  Time-averaged wear rate with variousinclination angles

    图 8  周向上两个壁倾角取不同值时的时间平均磨损率

    Figure 8.  Time-averaged wear rate of the two various inclination angles in circumferential direction

    图 9  不同转速下的时间平均磨损率

    Figure 9.  Time-averaged wear rate under various rotational speeds

    图 10  保持架打滑率在不同内圈转速下的变化曲线

    Figure 10.  Variation curves of cage slip rate under various inner ring rotational speeds

    表  1  轴承结构参数

    Table  1.   Geometric parameters of bearing

    参数数值
    轴承内径/mm100
    轴承外径/mm140
    轴承宽度/mm20
    滚子数量26
    滚子直径/mm10
    滚子宽度/mm7
    保持架内径/mm114.46
    保持架外径/mm124.46
    下载: 导出CSV

    表  2  轴承材料特性参数

    Table  2.   Material performance parameters of bearing

    元件密度/
    10−6 (kg/mm3
    弹性模量/
    105 (N/mm2
    泊松比
    内圈7.8012.070.290
    外圈7.8012.070.290
    滚子7.8012.070.290
    保持架8.5451.060.324
    下载: 导出CSV

    表  3  4050航空润滑油参数

    Table  3.   Parameters of 4050 aviation lubricating oil

    参数数值
    常温密度/10−6 (kg/mm30.970
    动力黏度/(Pa·s)0.055
    导热系数/(N/(m·K))0.0966
    黏压系数/10−8 Pa−12.02
    下载: 导出CSV
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  • 收稿日期:  2021-08-03
  • 网络出版日期:  2022-10-21

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