空间星冕仪滤光轮机构设计与试验研究

Design and experimental study of filter wheel mechanism of space coronagraph

  • 摘要: 为实现中国空间站巡天光学望远镜空间星冕仪的多谱段成像,将不同光谱透过率的滤光片分时切入光路,本文设计了一种结构紧凑的滤光轮机构。由于空间星冕仪需长期在轨观测,要求滤光轮机构能够在轨长期高稳定性地切入切出,设计了基于小模数蜗轮蜗杆作为机械传动机构的滤光轮,具有结构紧凑、刚度高、机构单向360°旋转和反向自锁功能等特点;详细分析了机构的运动精度和刚度及其动力学性能,并在振动试验前后对滤光轮机构进行了精度测试。测试结果表明:滤光轮定位精度满足≤±0.5 mm要求,机构的3个方向一阶模态均>100 Hz。根据振动试验分析结果可知,设计的滤光轮的刚度、动力学性能均满足航天力学环境要求,能够保证空间复杂工况下多谱段成像。

     

    Abstract: In order to realize multi-spectral imaging of space coronagraph of Chinese space station survey optical telescope, a compact filter wheel mechanism was designed to cut the filters with different spectral transmittance into the optical path. Because the space coronagraph needed long-term observation in orbit, the high stability requirement for the filter wheel mechanism was put forward. A filter wheel based on small modulus worm gear as a mechanical transmission mechanism was designed, which had the features of compact structure, high stiffness, one-way 360° rotation and reverse self-locking function. The precision, stiffness, and mechanical properties of the mechanism were analyzed, and the precision of the filter wheel was tested before and after the vibration test. The test results show that the positioning accuracy of the filter wheel is less than or equal to ±0.5 mm, and the first-order modes of the three directions of mechanism are all greater than 100 Hz. The vibration test analysis results show that the designed stiffness and dynamic performance of the mechanism can meet the requirements of aerospace mechanics environment, which can ensure the multi-spectral imaging under complex spatial conditions.

     

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