The invention relates to a micro-flow storage and supply system and method. The micro-flow storage and supply system comprises a gas storage and control module, a propellant storage and supply module and a micro-flow control module. The gas storage and control module adjusts input high-pressure gas to the gas pressure needed by the propellant storage and supply module through a mechanical pressure reduction part, and constant output pressure is provided for the liquid propellant stored in the propellant storage and supply module. The propellant storage and supply module does piston motion under constant output pressure, and the stored liquid propellant is discharged to the micro-flow control module; the micro-flow control module provides preset flow resistance for the system, and the output of the liquid propellant is adjusted to reach the ultra-micro flow of the magnitude of ten nanoliters per second. According to the invention, a certain volume of liquid propellant can be stored for a small spacecraft propulsion system, and nanoliter per second-order flow output can be provided.

    本发明涉及一种微流量贮存供给系统及方法,包括:气体贮存与控制模块、推进剂贮存供给模块、微流量控制模块;气体贮存与控制模块将输入的高压气体经过机械式减压部件调节至推进剂贮存供给模块所需的气体压力,为推进剂贮存供给模块存储的液体推进剂提供恒定的输出压力;推进剂贮存供给模块在恒定的输出压力下做活塞运动,将存储的液体推进剂排出至微流量控制模块;微流量控制模块为系统提供预设流阻,调节液体推进剂的输出达到十纳升每秒量级的超微流量。本发明能够为小型空间飞行器推进系统贮存一定容量的液体推进剂,并提供纳升每秒量级的流量输出。


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    Titel :

    Micro-flow storage and supply system and method


    Weitere Titelangaben:

    一种微流量贮存供给系统及方法


    Beteiligte:
    QU ZHEN (Autor:in) / LIU XUHUI (Autor:in) / WEI YANMING (Autor:in) / GUAN CHANGBIN (Autor:in) / JIANG HUA (Autor:in) / LI YONG (Autor:in) / YAO ZHAOPU (Autor:in) / LIN XINGRONG (Autor:in) / LONG JUN (Autor:in) / ZHENG WEIJIE (Autor:in)

    Erscheinungsdatum :

    2024-01-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F02K JET-PROPULSION PLANTS , Strahltriebwerke



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