Infrared and Laser Engineering, Volume. 51, Issue 11, 20220232(2022)

New lightweight design method and application of main support structure in airborne infrared imaging system

Yanwei Li1, Longhai Yin1、*, Yulong Li2, Xinwang Xie1, Jingguo Zhang3, and Hongbo Xie1
Author Affiliations
  • 1Ji Hua Laboratory, Foshan 528200, China
  • 2Changchun Changguang Aerospace Composite Materials Co., LTD, Changchun 130102, China
  • 3Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, Changchun 130033, China
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    Figures & Tables(20)
    Schematic diagram of main support system installation
    Schematic diagram of position relation of main optical system
    Lightweight main support structure of titanium alloy material
    Flow diagram of new lightweight design method
    Schematic diagram of the interface connection
    Main support structure of new lightweight design method
    Parametric model of main support structure
    Finite element model of main support system
    (a) First order mode shape; (b) Second order mode shape; (c) Third order mode shape
    (a) Curve of vibration analysis result; (b) Stress figure of sine vibration analysis
    Forming process flow chart of new lightweight main support structure
    Figure of hot melt prepreg line
    Figure of new lightweight main support structure
    Curve of vibration test result
    • Table 1. The material parameters

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      Table 1. The material parameters

      MaterialDensity/ 103 kg·m−3Elastic modulus/GPaPoisson's ratioLinear expansion coefficient/10−6 K−1
      SiC3.054000.182.5
      Glass-ceramics2.53910.240.05
      4J368.11410.250.05
      ZTC44.401120.298.9
      ZL1142.80700.3323.6
    • Table 2. Comparison of physical and mechanical properties of modified cyanate resin castings

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      Table 2. Comparison of physical and mechanical properties of modified cyanate resin castings

      PerformanceUnmodified cyanate estersModified cyanate esters
      Bending strength/MPa90127
      Bending modulus/GPa3.83.2
      Tensile strength/MPa5273
      Tensile modulus/GPa3.43.2
      Elongation at break1.2%3.4%
      Impact strength/kJ·m−27.316.4
    • Table 3. Performance parameters of M40 carbon fiber composites

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      Table 3. Performance parameters of M40 carbon fiber composites

      PerformanceValue
      Longitudinal modulus/GPa90
      Transverse modulus/GPa3.8
      Shear modulus/GPa52
      Poisson’s ratio3.4
      Density/103 kg·m−31.6
      Axial linear expansion coefficient/10−6 K−10.76 e-6
    • Table 4. Weight of mass points

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      Table 4. Weight of mass points

      NameWeight/kg
      Image preprocessor4.5
      Third and fourth mirrors3.0
      Reflective optical system14.5
      Detector assembly4.5
    • Table 5. Result of modal analysis

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      Table 5. Result of modal analysis

      ItemValue
      First order frequency/Hz415
      Second order frequency/Hz610
      Third order frequency/Hz793
    • Table 6. Conditions of sine vibration analysis

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      Table 6. Conditions of sine vibration analysis

      Frequency/HzMagnitude (Y direction)/g
      5−5000.2
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    Yanwei Li, Longhai Yin, Yulong Li, Xinwang Xie, Jingguo Zhang, Hongbo Xie. New lightweight design method and application of main support structure in airborne infrared imaging system[J]. Infrared and Laser Engineering, 2022, 51(11): 20220232

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    Paper Information

    Category: Optical design

    Received: Mar. 31, 2022

    Accepted: --

    Published Online: Feb. 9, 2023

    The Author Email: Yin Longhai (ylh761208@163.com)

    DOI:10.3788/IRLA20220232

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