Chinese Optics, Volume. 15, Issue 5, 1079(2022)

Flexural mounting technology of a 1.8 m space-borne rectangular mirror

Zong-xuan LI1,3、*, Chang-hao ZHANG1,2,3, De-fu ZHANG1,3, Bin MA1,2,3, and Yun-feng LI1,2,3
Author Affiliations
  • 1Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, Changchun 130033, China
  • 2University of Chinese Academy of Sciences, Beijing 100049, China
  • 3Key Laboratory of Space-Based Dynamic Fast Optical Imaging Technology, Chinese Academy of Sciences, Changchun 130033, China
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    Figures & Tables(30)
    Schematic diagram of mounting structure of a rectangular mirror with large aperture
    Typical constraints for a mirror. (a) 2-2-2 Constraint; (b) 3-2-1 Constraint
    A bi-axial flexural hinge based on kinematic equivalence principle
    Bi-axial flexural support
    Schematic diagram of equivalent flexural short straight beam
    Relationship between kx and height a, thickness t, width w of the short straight beam
    Relationship between kθy and a, t, w
    Relationship between the flexural support and CG plane
    Finite element model of the mirror assembly
    Optical axis of 1.8 m rectangular mirror
    Effect of ε1 (a) and ε2 (b) on the surface figure RMS
    Effect of ε1 (a) and ε2 (b) on the first-order natural frequency of PMA
    Mounting angle of the flexural supports
    Surface deformation at different θ1 values under 1 G gravity (removed rigid-body displacement)
    Effect of different θ2 values on the RMS and first-order natural frequency
    Effect of different sizes of flexural support on the RMS value
    Effect of different sizes of flexural supports on the first-order natural frequency
    Schematic diagram of the flexural supports′ structure
    Surface deformation under 1 G gravity in x and y directions (rigid-body displacement removed)
    The first three modes of PMA
    Dynamic test scene site map
    Swept frequency test results in x direction
    Sweep sine vibration result in y direction
    Random vibration test in z direction
    Schematic diagram of mirror aspheric interferometry optical testing layout
    The surface figure of the mirror tested in 0° direction
    The surface figure of the mirror tested in 180° direction
    • Table 1. Degree of freedom at each support point for mirror's typical constraints

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      Table 1. Degree of freedom at each support point for mirror's typical constraints

      (a)“2-2-2”约束方式
      支撑点约束自由度释放自由度
      ATxRxTyTzRyRz
      BTyRyTxTzRxRz
      CTzRzTxTyRxRy
      (b)“3-2-1”约束方式
      支撑点约束自由度释放自由度
      ATxTyTzRxRyRz
      BTyRzTxTyTzRx
      CRxTxTyTzRyRz
    • Table 2. Initial size values of the short straight beam

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      Table 2. Initial size values of the short straight beam

      尺寸变量初值/mm尺寸范围/mm
      a2015~25
      t85~10
      w127~15
    • Table 3. Surface figure error of flexural support No.1 at different mounting angles

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      Table 3. Surface figure error of flexural support No.1 at different mounting angles

      角度θx向RMS/nm y向RMS/nm 一阶固有频率/Hz
      010.128.5108.75
      903.975.34106.36
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    Zong-xuan LI, Chang-hao ZHANG, De-fu ZHANG, Bin MA, Yun-feng LI. Flexural mounting technology of a 1.8 m space-borne rectangular mirror[J]. Chinese Optics, 2022, 15(5): 1079

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    Paper Information

    Category: Original Article

    Received: Jun. 13, 2022

    Accepted: --

    Published Online: Sep. 29, 2022

    The Author Email:

    DOI:10.37188/CO.2022-0131

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