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Design of Optical and Mechanical Structure for Lunar Simulator Based on Variable Shape and Adjustable Radiance

LIU Shi ZHANG Guoyu SUN Gaofei WANG Lingyun GAO Yujuni

LIU Shi, ZHANG Guoyu, SUN Gaofei, WANG Lingyun, GAO Yujuni. Design of Optical and Mechanical Structure for Lunar Simulator Based on Variable Shape and Adjustable Radiance[J]. 空间科学学报, 2015, 35(5): 647-652. doi: 10.11728/cjss2015.05.647
引用本文: LIU Shi, ZHANG Guoyu, SUN Gaofei, WANG Lingyun, GAO Yujuni. Design of Optical and Mechanical Structure for Lunar Simulator Based on Variable Shape and Adjustable Radiance[J]. 空间科学学报, 2015, 35(5): 647-652. doi: 10.11728/cjss2015.05.647
LIU Shi, ZHANG Guoyu, SUN Gaofei, WANG Lingyun, GAO Yujuni. Design Of Optical And Mechanical Structure For Lunar Simulator Based On Variable Shape And Adjustable Radiance[J]. Chinese Journal of Space Science, 2015, 35(5): 647-652. doi: 10.11728/cjss2015.05.647
Citation: LIU Shi, ZHANG Guoyu, SUN Gaofei, WANG Lingyun, GAO Yujuni. Design Of Optical And Mechanical Structure For Lunar Simulator Based On Variable Shape And Adjustable Radiance[J]. Chinese Journal of Space Science, 2015, 35(5): 647-652. doi: 10.11728/cjss2015.05.647

Design of Optical and Mechanical Structure for Lunar Simulator Based on Variable Shape and Adjustable Radiance

doi: 10.11728/cjss2015.05.647 cstr: 32142.14.cjss2015.05.647
基金项目: Supported by National Public Welfare Industry (GYHY200706003, GYHY201006043).
详细信息
    通讯作者:
    • LIU Shi,E-mail:2811792642@qq.com
  • 中图分类号: V524.7

Design Of Optical And Mechanical Structure For Lunar Simulator Based On Variable Shape And Adjustable Radiance

Funds: Supported by National Public Welfare Industry (GYHY200706003, GYHY201006043).
More Information
    Corresponding author: LIU Shi,E-mail:2811792642@qq.com
  • 摘要: To simulate the different lunar phases and ensure continuous adjustability of the radiant brightness, a new broad spectrum light and frosted glass were applied and designed in the optical system for lunar simulator with the shapes and radiance being able to be adjusted. According to the engineering demand and index requirements of the optical system, three major design aspects are addressed, including the high reliability and maintainability for broad-spectrum light, heat dissipation in lunar simulator for long working hours, and bearing of the main frame under different working conditions. By designing a reasonable machine structure, and through the structure itself with the matrix arrangement of 48 axial flow fans, an effectively cooling air duct is established. Deformation and temperature were calculated by the finite element software ANSYS. The results showed that the displacement deformation reached 0.33mm and stress deformation reached 0.02MPa at the temperature of 20℃; when the main frame was in the temperature field between 20℃ and 65℃, the maximum displacement deformation reached 13.30mm and maximum stress deformation is 97.90MPa, and the amount of this deformation is very small in considering of the mechanical structure dimensions and weight of the lunar simulator.

     

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出版历程
  • 收稿日期:  2015-02-03
  • 修回日期:  2015-03-03
  • 刊出日期:  2015-09-15

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