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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    Titel :

    Cyclone in-orbit gas-liquid separation apparatus


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

    Erscheinungsdatum :

    18.11.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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