A the hydrogen aircraft includes: an engine that uses hydrogen as a fuel; a fuel tank that stores the fuel; and a fuel supply line to supply the fuel from the fuel tank to the engine. The fuel tank or the fuel supply line includes a cooling medium supply port. The fuel supply line includes a cooling medium recovery port that is located downstream of the cooling medium supply port in terms of a flow of the fuel. A precooling system for precooling the fuel supply line of the hydrogen aircraft includes: a cooling medium supply line to supply a cooling medium to the cooling medium supply port; and a cooling medium recovery line to recover the cooling medium from the cooling medium recovery port. The precooling system supplies the cooling medium from the cooling medium supply line to the fuel supply line through the cooling medium supply port and recovers the cooling medium that has been supplied to the fuel supply line by the cooling medium recovery line through the cooling medium recovery port to precool the fuel supply line.


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    Title :

    HYDROGEN AIRCRAFT, PRE-COOLING EQUIPMENT, AND PRE-COOLING SYSTEM AND PRE-COOLING METHOD FOR FUEL SUPPLY LINE OF HYDROGEN AIRCRAFT


    Additional title:

    WASSERSTOFFFLUGZEUG, VORKÜHLAUSRÜSTUNG UND VORKÜHLSYSTEM UND VORKÜHLVERFAHREN FÜR KRAFTSTOFFZUFUHRLEITUNG EINES WASSERSTOFFFLUGZEUGS
    AÉRONEF À HYDROGÈNE, ÉQUIPEMENT DE PRÉ-REFROIDISSEMENT, SYSTÈME DE PRÉ-REFROIDISSEMENT ET PROCÉDÉ DE PRÉ-REFROIDISSEMENT POUR LIGNE D'ALIMENTATION EN CARBURANT D'UN AÉRONEF À HYDROGÈNE


    Contributors:

    Publication date :

    2024-09-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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