An aircraft includes an electrical system having at least one cooled electrical component. The at least one cooled electrical component is a low grade heat source. The aircraft further includes a cooling system with a coolant loop passing through the at least one cooled electrical component and through a first adsorption cooler. The first adsorption cooler is configured to cool coolant in the cooling loop using an adsorption process.


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    Titel :

    ADSORPTION BASED AIRCRAFT COOLANT SYSTEM


    Beteiligte:
    KILCHYK VIKTOR (Autor:in) / BARTOSZ LANCE R (Autor:in)

    Erscheinungsdatum :

    31.07.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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