A method for combined cooling and heating in an aircraft, the aircraft including an engine configured to use dihydrogen as fuel, the dihydrogen being stored in liquid form in a tank and being used in gas form in the engine, the dihydrogen being conveyed from the tank to the engine by a main pipe. The method includes the steps of branching off a part of the flow of dihydrogen in a bypass pipe, in parallel with a predefined segment of the main pipe, circulating a first heat transfer fluid in a first closed circuit, carrying out a first heat exchange between the first heat transfer fluid and the dihydrogen circulating in the bypass pipe and carrying out at least one secondary heat exchange. Each secondary heat exchange is carried out between the first heat transfer fluid and a working fluid used in the aircraft which needs to be cooled.


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    Titel :

    SYSTEME DE CHAUFFAGE DE DIHYDROGENE ET DE REFROIDISSEMENT DE FLUIDE COMBINES POUR AERONEF, ET AERONEF COMPRENANT UN TEL SYSTEME


    Weitere Titelangaben:

    COMBINED DIHYDROGEN HEATING AND FLUID COOLING SYSTEM FOR AN AIRCRAFT, AND AIRCRAFT COMPRISING SUCH A SYSTEM
    KOMBINIERTES SYSTEM ZUR ERWÄRMUNG VON WASSERSTOFF UND KÜHLUNG VON FLÜSSIGKEIT FÜR EIN FLUGZEUG UND FLUGZEUG MIT SOLCH EINEM SYSTEM


    Beteiligte:

    Erscheinungsdatum :

    11.09.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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