A propulsion system, comprising: a motor assembly including a stator and a rotor, a heat exchanger configured to receive air to cool a liquid, and a thermal plate including one or more channels configured to convey the liquid from the heat exchanger to the motor assembly. The heat exchanger is mechanically and fluidically coupled to the thermal plate.


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    Title :

    SYSTEMS AND METHODS FOR IMPROVED AIRCRAFT ELECTRIC ENGINES


    Additional title:

    SYSTEME UND VERFAHREN FÜR VERBESSERTE ELEKTRISCHE FLUGZEUGMOTOREN
    SYSTÈMES ET PROCÉDÉS POUR DES MOTEURS ÉLECTRIQUES D'AÉRONEF AMÉLIORÉS


    Contributors:

    Publication date :

    2025-08-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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