A propeller includes a blade free to rotate. A first stop is positioned to mechanically engage one or both of a first portion of the blade and a first structure coupled to the blade when the blade is in a first position at a first end of the rotational range of motion. A second stop is positioned to mechanically engage one or both of a second portion of the blade and a second structure coupled to the blade when the blade is in a second position at a second end of the defined rotational range. The blade rotates to the first position against the first stop when the propeller is rotated in a first direction and to the second position against the second stop when the propeller is rotated in a second direction.


    Access

    Download


    Export, share and cite



    Title :

    Bistable pitch propeller system with bidirectional propeller rotation


    Contributors:

    Publication date :

    2023-07-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64U



    Bistable pitch propeller system with bidirectional propeller rotation

    VANDER LIND DAMON / REICHERT TODD | European Patent Office | 2022

    Free access

    BISTABLE PITCH PROPELLER SYSTEM WITH BIDIRECTIONAL PROPELLER ROTATION

    VANDER LIND DAMON / REICHERT TODD | European Patent Office | 2022

    Free access

    Bistable pitch propeller system with bidirectional propeller rotation

    VANDER LIND DAMON / REICHERT TODD | European Patent Office | 2020

    Free access

    BISTABLE PITCH PROPELLER SYSTEM WITH BIDIRECTIONAL PROPELLER ROTATION

    VANDER LIND DAMON / REICHERT TODD | European Patent Office | 2020

    Free access

    BISTABLE PITCH PROPELLER SYSTEM WITH BIDIRECTIONAL PROPELLER ROTATION

    VANDER LIND DAMON / REICHERT TODD | European Patent Office | 2018

    Free access