Infrared and Laser Engineering, Volume. 49, Issue 4, 0414003(2020)

Parametric design and test of flexible support for mirror of single trans optical terminal

Xiaoming Li1,2、*, Guibing Wang1, Lizhong Zhang1,2, Tianyu Wang1, and Tianshuo Zhang1
Author Affiliations
  • 1National and Local Joint Engineering Research Center of Space and Optoelectronics Technology, Changchun University of Science and Technology, Changchun 130022, China
  • 2Institute of Mechanical Engineering, Changchun University of Science and Technology, Changchun 130022, China
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    Figures & Tables(20)
    Schematic diagram of laser communication terminal device
    Scheme of mirror subassembly
    Diagrams of two kinds of flexible support structure
    Main parameters of flexible support structure
    Relationship between the center angle of grooved circle θ, RMS of surface shape and dynamic stiffness of assembly
    Schematic diagram of flexible support structure
    Finite element model of mirror subassembly
    Modal analysis nephogram
    Mirror subassembly object and assembly drawing of the whole machine
    System for mirror subassembly surface shape testing
    Results of mirror subassembly surface shape testing at different temperatures
    Sweep sine response test site of mirror subassembly
    Sweep sine response curve under Z vibration
    • Table 1. Material properties of reflector components

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      Table 1. Material properties of reflector components

      PartMaterialρ/g·cm−3E/GPa μα/℃
      MirrorZerodur2.5390.60.230.05×10−6
      Support4J328.021450.260.3×10−6
      PlateTC44.441090.298.9×10−6
    • Table 2. Level table of parameter factors for flexible support structures

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      Table 2. Level table of parameter factors for flexible support structures

      LevelFactors
      R/mm θ/(°) B/mm R2/mm r/mm
      12.5151270.25
      23301.527.50.5
      33.5452280.75
      44602.528.51
    • Table 3. Orthogonal test scheme

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      Table 3. Orthogonal test scheme

      No.RθBR2rP
      12.5151270.2515.38
      22.5301.527.50.516.13
      32.5452280.7.520.04
      42.5602.528.5127.26
      53151.528114.71
      6330128.50.759.54
      73452.5270.518.88
      8360227.50.2520.17
      93.515228.50.59.34
      103.5302.5280.2512.79
      113.545127.518.08
      123.5601.5270.7512.66
      134152.527.50.7522.35
      14430227110.73
      154451.528.50.2513.28
      164601280.519.54
    • Table 4. Range analysis of factors

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      Table 4. Range analysis of factors

      NumberABCDE
      FactorsRθBR2r
      N119.715.4513.1414.4115.4
      N215.8312.2914.1916.6815.97
      N210.7215.0715.0716.7716.15
      N416.4819.4119.8214.8615.19
      R8.987.126.682.360.96
    • Table 5. Results of modal analysis of mirror subassembly

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      Table 5. Results of modal analysis of mirror subassembly

      OrderFz/Hz Mode of vibration
      1352.61Around X axis direction
      2486.29Around Y axis direction
      3488.98Around Y axis direction
    • Table 6. Analysis results of mirror surface error under 10 ℃ uniform temperature rise(reduction) and 1 g gravity(Unit: nm)

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      Table 6. Analysis results of mirror surface error under 10 ℃ uniform temperature rise(reduction) and 1 g gravity(Unit: nm)

      Load case directionTemperature riseTemperature reduction
      PVRMSPVRMS
      Xλ/10.84 λ/58.27 λ/10.69 λ/57.84
      Yλ/10.76 λ/58.11 λ/10.84 λ/57.79
      Zλ/10.14 λ/54.97 λ/11.4 λ/60.61
    • Table 7. Results of mirror subassembly surface shape testing(Unit: nm)

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      Table 7. Results of mirror subassembly surface shape testing(Unit: nm)

      Temperature/℃PVRMS
      10λ/6.62 λ/43
      20λ/6.94 λ/52
      30λ/6.9 λ/50
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    Xiaoming Li, Guibing Wang, Lizhong Zhang, Tianyu Wang, Tianshuo Zhang. Parametric design and test of flexible support for mirror of single trans optical terminal[J]. Infrared and Laser Engineering, 2020, 49(4): 0414003

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    Paper Information

    Received: Dec. 15, 2019

    Accepted: --

    Published Online: May. 27, 2020

    The Author Email: Li Xiaoming (lxmkidd@163.com)

    DOI:10.3788/IRLA202049.0414003

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