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.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Bistable pitch propeller system with bidirectional propeller rotation


    Beteiligte:
    VANDER LIND DAMON (Autor:in) / REICHERT TODD (Autor:in)

    Erscheinungsdatum :

    2023-07-18


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64U



    Bistable pitch propeller system with bidirectional propeller rotation

    VANDER LIND DAMON / REICHERT TODD | Europäisches Patentamt | 2022

    Freier Zugriff

    BISTABLE PITCH PROPELLER SYSTEM WITH BIDIRECTIONAL PROPELLER ROTATION

    VANDER LIND DAMON / REICHERT TODD | Europäisches Patentamt | 2022

    Freier Zugriff

    Bistable pitch propeller system with bidirectional propeller rotation

    VANDER LIND DAMON / REICHERT TODD | Europäisches Patentamt | 2020

    Freier Zugriff

    BISTABLE PITCH PROPELLER SYSTEM WITH BIDIRECTIONAL PROPELLER ROTATION

    VANDER LIND DAMON / REICHERT TODD | Europäisches Patentamt | 2020

    Freier Zugriff

    BISTABLE PITCH PROPELLER SYSTEM WITH BIDIRECTIONAL PROPELLER ROTATION

    VANDER LIND DAMON / REICHERT TODD | Europäisches Patentamt | 2018

    Freier Zugriff