An aeronautical propulsion system (200), comprises a propeller (202) mounted to a propeller shaft (204) defining a propeller axis (214); an electric motor (208) comprising a motor output shaft defining a motor axis (216); wherein the motor output shaft and propeller shaft are connected by a linkage such that, in use, driving the motor output shaft for rotation drives rotation of the propeller via the propeller shaft and linkage; and a motor power unit configured to receive power from a power source and provide a motor drive signal to the motor; wherein the motor power unit is spaced along the motor axis from the motor.


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    Title :

    AERONAUTICAL PROPULSION SYSTEM


    Additional title:

    AERONAUTISCHES ANTRIEBSSYSTEM
    SYSTÈME DE PROPULSION AÉRONAUTIQUE


    Contributors:
    HART SIMON (author) / PATEL MUKESH (author) / BURNS CHRIS (author)

    Publication date :

    2025-06-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64U / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen



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