某超音速风洞大尺寸光学玻璃观察窗优化设计
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中国空气动力研究与发展中心高速空气动力研究所

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Optimization design of large-size optical glass observation
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High Speed Aerodynamic Research Institute, China Aerodynamics Research and Development Center

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    摘要:

    针对某超音速风洞?800mm光学玻璃在试验过程中出现裂纹问题,详细分析了裂纹产生原因,并对光学玻璃结构形式及装配方法开展了优化设计。首先,在满足强度要求的情况下减小玻璃厚度,避免因轴向温度梯度差异过大导致应力集中;然后,设计易安装调节的低应力台阶式光学玻璃以减少因安装操作失误对光学玻璃的损伤,并利用Solidworks软件计算在合适预紧力及内外压差为一个大气压下两种结构形式的应力区别;最后运用Abaqus软件分析风洞试验过程中温度对光学玻璃的影响。结果表明:压差对观察窗强度影响不大,台阶式光学玻璃应力小于原结构形式;高马赫数、增压情况下的温度骤降将造成观察窗中间部位应力集中。

    Abstract:

    In view of the crack problem of 800mm optical glass in a supersonic wind tunnel during the test, the causes of cracks are analyzed in detail, and the structural form and assembly method of optical glass are optimized. Firstly, the thickness of glass is reduced to meet the strength requirements, so as to avoid the stress concentration caused by the large difference of the axial temperature gradient. Then, a low-stress stepped optical glass that is easy to install and adjust is designed to reduce the damage to the optical glass due to installation and operation errors, and Solidworks software is used to calculate the stress difference between the two structural forms under appropriate preload and internal and external pressure difference. Finally, Abaqus software is used to analyze the influence of temperature on optical glass during the wind tunnel test. The results show that the pressure difference has little effect on the strength of the observation window, and the stress of the stepped optical glass is less than that of the original structure. The temperature drop in the case of high Mach number and pressurization will cause stress concentration in the middle of the observation window.

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  • 收稿日期:2024-04-10
  • 最后修改日期:2024-04-15
  • 录用日期:2024-04-19
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