An electrical power system is disclosed for an aircraft having a hybrid-electric propulsion system, which includes a battery assembly for storing energy, an electric motor controller operatively connected to the battery assembly for conditioning and controlling power to an electric motor, and an electric motor receiving power through the motor controller for delivering torque to a shaft of the hybrid-electric propulsion system.


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    Title :

    ELECTRICAL POWER SYSTEM FOR AIRCRAFT HAVING HYBRID-ELECTRIC PROPULSION SYSTEM


    Contributors:
    SMITH ANDREW D (author) / IVES KYLE (author) / BAIG ZUBAIR A (author)

    Publication date :

    2020-09-03


    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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