A system for cooling a superconducting motor includes a combustor (270) and fuel tank (210) that contains a fuel. The system further includes a cooling system (200) that provides the fuel to the superconducting motor or a cryocooler to cool the superconducting motor, resulting in at least partially vaporized fuel coming out of the superconducting motor or cryocooler. The cooling system also a cryocooler and a twophase ejector that mixes the fuel from the tank and the at least partially vaporized fuel to produce a mixed fuel. The combustor receives the mixed fuel and generates electric power due its combustion. The power can be provided to the superconducting motor.


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    Titel :

    COOLING ARCHITECTURE USING CRYOGENIC FUELS


    Weitere Titelangaben:

    KÜHLARCHITEKTUR MIT KRYOGENEN BRENNSTOFFEN
    ARCHITECTURE DE REFROIDISSEMENT UTILISANT DES CARBURANTS CRYOGÉNIQUES


    Beteiligte:

    Erscheinungsdatum :

    2024-06-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES



    COOLING ARCHITECTURE USING CRYOGENIC FUELS

    ALAHYARI ABBAS A | Europäisches Patentamt | 2024

    Freier Zugriff

    Cryogenic fuels for aircraft

    Esgar, J. B. | NTRS | 1971


    Managing cryogenic fuels on heavy-duty HPDI vehicles

    Post, Adrian / Mumford, David / McDonald, Robbi et al. | Springer Verlag | 2020


    Cryogenic Cooling Systems in Space

    Jewell, C. I. | British Library Online Contents | 1996