A cryogenic fuel system for an aircraft, the cryogenic fuel system includes a fuel tank assembly that is configured to store a cryogenic fuel in a liquid phase during aircraft operation, and a cooling system that is associated with the fuel tank assembly. The cooling system is configured to maintain the fuel tank assembly within a predefined temperature range during non-flight operation.


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    Titel :

    COOLING OF AIRCRAFT CRYOGENIC FUEL TANK ASSEMBLY


    Beteiligte:

    Erscheinungsdatum :

    17.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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