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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    Title :

    ADSORPTION BASED AIRCRAFT COOLANT SYSTEM


    Contributors:

    Publication date :

    2025-07-31


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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