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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    Titel :

    AIRCRAFT SYSTEM, AIRCRAFT FUEL SYSTEM AND METHOD


    Beteiligte:
    THORNER CALLUM (Autor:in) / JAMES DYLAN BENEDICT (Autor:in) / SAVIN DAVID (Autor:in)

    Erscheinungsdatum :

    2023-12-14


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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