An aircraft system for handling cryogenic liquid. The aircraft system comprises a vessel configured to store cryogenic liquid, a vacuum ejector operable to cause at least some of the cryogenic liquid to be moved from the vessel, and a pump downstream of the vacuum ejector, wherein the vacuum ejector is fluidically connected to the pump.


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    Title :

    AIRCRAFT SYSTEM, AIRCRAFT FUEL SYSTEM AND METHOD


    Contributors:

    Publication date :

    2023-12-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT




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