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.
Cyclone in-orbit gas-liquid separation apparatus
2015-11-18
Patent
Electronic Resource
English
Reduced Pressure Cyclone Separation Studies Using Synthetic Lunar Regolith
British Library Conference Proceedings | 2010
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