AEROSPACE SHANGHAI, Volume. 41, Issue 3, 167(2024)

Design Optimization and Experimental Verification of Trundle Bearing Mechanisms for Spacecrafts

Decai YANG*... Jianhui LI, Chuankun QU, Daxing HUANG, Zhifei MA, Zhiyi WANG and Zhiyuan QIAN |Show fewer author(s)
Author Affiliations
  • Shanghai Key Laboratory of Spacecraft Mechanism,Shanghai201109,China
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    Figures & Tables(19)
    Solar-oriented driving mechanisms for small and medium-sized spacecrafts at home and abroad
    Trundle bearing mechanisms for space stations at home and abroad
    Working principle of the trundle bearing mechanism in single pattern
    Design scheme and mechanism principle of the trundle bearing assembly
    Roller-rail kinematic pairs between the trundle bearing assembly and rail
    Schematic diagram of the roller-rail kinematic pair at Roller A
    Geometrical relationship between Roller A and the rail
    Status of the trundle bearing assembly and rail before and after clamping
    Principle of the vacuum circular rail test and picture of the test equipment
    Test specimens of the circular rail and rollers
    Product pictures in No.1 operating condition test
    • Table 1. Parameters of the schematic diagram of Fig.6

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      Table 1. Parameters of the schematic diagram of Fig.6

      参数名称参数含义
      R11滚轮A靠近导轨小圈一侧的滚轮半径
      R12滚轮A靠近导轨大圈一侧的滚轮半径
      R21与滚轮A接触位置的导轨小圈半径
      R22与滚轮A接触位置的导轨大圈半径
      ω1滚轮A转动角速度
      ω2导轨转动角速度
      v11滚轮A靠近导轨小圈一侧的滚轮外圈转动线速度,v11=R11ω1
      v12滚轮A靠近导轨大圈一侧的滚轮外圈转动线速度,v12=R12ω1
      v21与滚轮A接触位置的导轨小圈转动线速度,v21=R21ω2
      v22与滚轮A接触位置的导轨大圈转动线速度,v22=R22ω2
    • Table 2. Parameters of the schematic diagram of Fig.7

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      Table 2. Parameters of the schematic diagram of Fig.7

      参数名称参数含义
      o1滚轮A组件回转轴心
      o2滚轮A宽度方向中心点
      L1滚轮A轴向宽度,25 mm
      L2滚轮A与导轨面接触线长度
      β滚轮A圆锥面倾斜角
      d1滚轮A组件回转轴心与滚轮A回转轴线的距离
      d2滚轮A组件回转轴心与导轨回转轴线的距离
      r滚轮A回转轴线与接触面的距离
      R11滚轮A靠近导轨小圈一侧的滚轮半径
      R12滚轮A靠近导轨大圈一侧的滚轮半径
      R21与滚轮A接触位置的导轨小圈半径
      R22与滚轮A接触位置的导轨大圈半径
    • Table 3. Contact point radius ratios and roll-slip ratios of the conical roller-rail kinematic pairs

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      Table 3. Contact point radius ratios and roll-slip ratios of the conical roller-rail kinematic pairs

      位置部件名称

      接触点半径比

      (大径/小径)

      滚滑比s
      滚轮A处导轨1.028 820
      滚轮A1.028 82
      滚轮B处导轨1.030 380
      滚轮B1.030 38
      滚轮C处导轨1.066 430
      滚轮C1.066 43
    • Table 4. Effects of the roller structure dimension error on the roll-slip ratio

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      Table 4. Effects of the roller structure dimension error on the roll-slip ratio

      位置项目名称理论值最大值最小值
      滚轮A处滚轮半径比1.028 821.028 991.028 73
      滚滑比0-1.7×10-48.7×10-5
      滚轮B处滚轮半径比1.030 381.030 531.030 27
      滚滑比0-1.5×10-41.1×10-4
      滚轮C处滚轮半径比1.066 431.066 551.066 28
      滚滑比0-1.1×10-41.4×10-4
    • Table 5. Effects of the rail position error on the roll-slip ratio

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      Table 5. Effects of the rail position error on the roll-slip ratio

      位置项目名称导轨位置偏差/mm
      -1.0-0.5+0.5+1.0
      滚轮A处导轨半径比1.028 871.028 851.028 801.028 78
      滚滑比4.9×10-52.9×10-5-1.9×10-5-3.9×10-5
      滚轮B处导轨半径比1.030 431.030 411.030 351.030 33
      滚滑比4.9×10-52.9×10-5-2.9×10-5-4.9×10-5
      滚轮C处导轨半径比1.066 541.066 491.066 371.066 32
      滚滑比1.0×10-45.6×10-5-5.6×10-5-1.0×10-4
    • Table 6. Status of the specimens of the life test

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      Table 6. Status of the specimens of the life test

      参试产品产品状态
      导轨圆盘试件除结构尺寸外,其余与真实导轨状态一致
      圆柱形滚轮组件外圈面镀固体润滑膜,为圆柱形,带圆弧
      圆锥形滚轮组件外圈面镀固体润滑膜,为圆锥形,带圆弧
    • Table 7. Operating conditions of the life test

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      Table 7. Operating conditions of the life test

      工况 名称导轨转速/ (r·min-1)运动副滚滑比目标导轨圈数/万圈参试试件
      工况150.12922.6导轨圆盘+ 圆柱形滚轮
      工况25理论值022.6导轨圆盘+ 圆锥形滚轮
    • Table 8. Processing product pictures in No.2 operating condition test

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      Table 8. Processing product pictures in No.2 operating condition test

      导轨转动 圈数/万圈导轨试件 照片滚轮试件 照片
      1.0
      5.5
      10.8
      17.6
      22.7
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    Decai YANG, Jianhui LI, Chuankun QU, Daxing HUANG, Zhifei MA, Zhiyi WANG, Zhiyuan QIAN. Design Optimization and Experimental Verification of Trundle Bearing Mechanisms for Spacecrafts[J]. AEROSPACE SHANGHAI, 2024, 41(3): 167

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    Paper Information

    Category: Innovation and Exploration

    Received: Jun. 7, 2024

    Accepted: --

    Published Online: Sep. 3, 2024

    The Author Email:

    DOI:10.19328/j.cnki.2096-8655.2024.03.018

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