A thermal management system (120) enables fluid coupling of the cooling circuits (122, 126, 128) for the battery (112) and the propeller arrangements (108). More than one propeller arrangement (108)can be serviced by the same cooling circuit, but distribution of the coolant may be finessed. Optional pathways are provided to use heated coolant for heating (e.g., de-icing, cabin heating, etc.) before cooling the coolant. Fluid coupling of conduits between and/or within the cooling circuits provide redundancy to accommodate various faults and equipment malfunctions.


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    Title :

    THERMAL MANAGEMENT SYSTEM


    Additional title:

    WÄRMEVERWALTUNGSSYSTEM
    SYSTÈME DE GESTION THERMIQUE



    Publication date :

    2023-03-01


    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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