A propulsor assembly of an electric aircraft is described. The propulsor assembly includes an electric motor, where the electric motor includes a stator and a rotor. The assembly further includes a propulsor mechanically connected to the rotor of the electric motor. The assembly also includes a cyclic control assembly including an electric actuator and a push rod, wherein the push rod is mechanically connected to the actuator and the propulsor, the push rod is configured to increase a blade angle of the propulsor when the push rod is displaced in a first direction, and the push rod is configured to decrease the blade angle of the propulsor when the push rod is displaced in a second direction.


    Access

    Download


    Export, share and cite



    Title :

    Propulsor assembly of an electric aircraft


    Contributors:

    Publication date :

    2025-05-27


    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



    PROPULSOR ASSEMBLY OF AN ELECTRIC AIRCRAFT

    BROOKES KYLE | European Patent Office | 2024

    Free access

    AIRCRAFT WITH ELECTRIC PROPULSOR

    DIERKSMEIER DOUGLAS D | European Patent Office | 2020

    Free access

    Aircraft with electric propulsor

    DIERKSMEIER DOUGLAS D | European Patent Office | 2022

    Free access

    AIRCRAFT WITH ELECTRIC PROPULSOR

    DIERKSMEIER DOUGLAS D | European Patent Office | 2020

    Free access

    Multi-propulsor electric aircraft

    European Patent Office | 2021

    Free access