The invention discloses a vacuum container for space environment simulation of spaceflight equipment, and relates to the field of vacuum testing, the vacuum container comprises a vacuum tank main body, a main control module and an adjusting component, one side of the vacuum tank main body is provided with the main control module, and the vacuum tank main body is internally provided with the adjusting component, the server serves as a carrying end of each functional part and functional module and provides a test target accommodating environment; the main control module is used for providing a vacuum environment, performing temperature control and pressure control and correcting an abnormal state; the adjusting part is used for adjusting the testing posture of a testing target and collecting volatile products, by arranging the adjusting part, the testing material can generate posture adjustment of a certain amplitude in the testing process, the pressed and heated environment of the testing material can be adjusted, when local pressure and temperature unbalance occurs, feedback adjustment can be carried out in time, and the testing efficiency is improved. Volatile gas in the vacuum tank main body can be conveniently emptied, and smooth proceeding of subsequent testing procedures is facilitated.
本发明公开了航天设备太空环境模拟用真空容器,涉及真空测试领域,包括真空罐主体、主控模组和调节部件,所述真空罐主体的一侧安装有主控模组,所述真空罐主体的内部安装有调节部件,其中:真空罐主体,作为各功能部件与功能模块的搭载端,提供测试目标容纳环境;主控模组,用于提供真空环境,进行温度控制和压力控制,纠正异常状态;调节部件,用于对测试目标进行测试姿态调节与挥发产物收集,通过设置调节部件,使得测试材料在测试过程中,可产生一定幅度的姿态调节,使其受压和受热环境进行调整,当出现局部压力和温度失衡情况时,可及时进行反馈调整,便于将真空罐主体内挥发气体排空,便于后续测试工序的顺利进行。
Vacuum container for space environment simulation of aerospace equipment
航天设备太空环境模拟用真空容器
2025-02-14
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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|AIAA | 1966
|TIBKAT | 1968
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