The invention relates to an underground vacuum tube ejection type microgravity experimental device and experimental method.The underground vacuum tube ejection type microgravity experimental device comprises an overground part and an underground part, the overground part comprises a debugging control area and an experimental load and equipment replacement and installation area, and the debugging control area is located on one side of the experimental load and equipment replacement and installation area; the underground part comprises a vacuum pump set mounting area and a vacuum shaft, the experimental load and equipment replacement mounting area is located above the vacuum shaft, a shaft vacuum cabin door is arranged between the experimental load and equipment replacement mounting area and the vacuum shaft, and the vacuum pump set mounting area is located on one side of the vacuum shaft; a vacuum pump set for vacuumizing the vacuum shaft and the experimental load and equipment replacement mounting area is arranged in the vacuum pump set mounting area; a row of experiment cabin operation driving mechanisms and experiment cabins are arranged in the vacuum vertical shaft, the experiment cabin operation driving mechanisms upwards extend into the experiment load and equipment replacement installation area, and the experiment cabins are installed on the experiment cabin operation driving mechanisms and vertically operate under the driving of the driving mechanisms.

    本发明涉及一种地下真空管弹射式微重力实验装置及实验方法,地下真空管弹射式微重力实验装置包括地上部分和地下部分,地上部分包括调试控制区、实验载荷及设备更换安装区,调试控制区位于实验载荷及设备更换安装区的一侧;地下部分包括真空泵组安装区和真空竖井,实验载荷及设备更换安装区位于真空竖井的上方且与真空竖井之间设有竖井真空舱门,真空泵组安装区位于真空竖井的一侧,真空泵组安装区内设有用于真空竖井和实验载荷及设备更换安装区抽真空的真空泵组;真空竖井内设有一列实验舱运行驱动机构和实验舱,实验舱运行驱动机构向上延伸至实验载荷及设备更换安装区内,实验舱安装在实验舱运行驱动机构上并在驱动机构的驱动下竖直运行。


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    Titel :

    Underground vacuum tube ejection type microgravity experiment device and experiment method


    Weitere Titelangaben:

    一种地下真空管弹射式微重力实验装置及实验方法


    Beteiligte:
    ZHANG JIANQUAN (Autor:in) / DONG WENBO (Autor:in) / ZHANG YONGKANG (Autor:in) / ZHANG XIN (Autor:in) / WANG ZHE (Autor:in) / CAI ZHIWEI (Autor:in) / GUO RUICHENG (Autor:in)

    Erscheinungsdatum :

    2024-04-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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