The present invention discloses a cyclone in-orbit gas-liquid separation apparatus, which can achieve gas and liquid separation in a microgravity environment. The designed cyclone in-orbit gas-liquid separation apparatus comprises a circle of spiral pipeline and two branch pipelines, wherein the cross section of the pipeline is circular, a separation plate is arranged inside the pipeline, the cross section of the pipeline is divided into two semi-circular cross sections after flowing a circle, and two leading-out pipe are respectively used for leading a liquid propellant and gas. The cyclone on-track gas-liquid separation apparatus of the present invention has characteristics of high efficiency and strong anti-interference capability, and provides a novel simple and efficient gas-liquid separation method for propellant in-orbit supply.


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    Title :

    Cyclone in-orbit gas-liquid separation apparatus


    Contributors:
    WANG HUA (author) / CUI CUNYAN (author) / SI PINGJUN (author) / ZHANG YU (author) / HU JINGHUI (author) / CHEN JINGPENG (author) / XIN CHAOJUN (author) / FAN DONGLEI (author) / WANG YAN (author) / WANG PING (author)

    Publication date :

    2015-11-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B01D SEPARATION , Trennen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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