Low latency pitch adjustable rotors are disclosed. A disclosed example rotor includes a rotor hub to rotate about a rotational axis, rotor blades coupled to the rotor hub, the rotor blades being pitch adjustable and having corresponding pitch angles, and a reaction hinge operatively coupled between the rotor hub and the rotor blades, the reaction hinge to move relative to the rotor hub in response to an angular acceleration or deceleration of the rotor hub to adjust the pitch angles.


    Access

    Download


    Export, share and cite



    Title :

    Low latency pitch adjustable rotors


    Contributors:

    Publication date :

    2023-05-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    LOW LATENCY PITCH ADJUSTABLE ROTORS

    SARTORIUS THOMAS SKYLER | European Patent Office | 2020

    Free access

    Pitch Control for Helicopter Rotors

    Jeffery, P. / Luecke, G. | NTRS | 1986


    Variable-pitch ringed rotors for aircraft

    SINUSAS ERIC ALBERT / PARHAM JR THOMAS C / BRAND ALBERT GERARD | European Patent Office | 2020

    Free access

    VARIABLE-PITCH RINGED ROTORS FOR AIRCRAFT

    SINUSAS ERIC ALBERT / PARHAM JR THOMAS C / BRAND ALBERT GERARD | European Patent Office | 2020

    Free access

    Smooth pitch control for propellers and rotors

    HINKS WILLIAM L | European Patent Office | 2019

    Free access