A hinged propeller comprising a hub and one or more blades is disclosed. In various embodiments, a blade is connected to the hub via a hinge, wherein at least a substantial part of the blade has a longitudinal axis that is substantially parallel to a line extending radially from a center of the hub, and wherein the hinge has an axis of hinge rotation that is oriented at a non-zero acute angle to a line that is perpendicular, in a plane of rotation of the hub, to said longitudinal axis.


    Access

    Download


    Export, share and cite



    Title :

    Hinged rotor blade to provide passive variable pitch


    Contributors:

    Publication date :

    2023-11-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    HINGED ROTOR BLADE TO PROVIDE PASSIVE VARIABLE PITCH

    REICHERT TODD | European Patent Office | 2024

    Free access

    Hinged rotor blade to provide passive variable pitch

    REICHERT TODD | European Patent Office | 2019

    Free access

    Hinged rotor blade to provide passive variable pitch

    REICHERT TODD | European Patent Office | 2022

    Free access

    Hinged rotor blade to provide passive variable pitch

    REICHERT TODD | European Patent Office | 2021

    Free access

    Hinged rotor blade to provide passive variable pitch

    REICHERT TODD | European Patent Office | 2024

    Free access