A control input operable by a user for controlling movement of an aircraft includes a base portion configured for coupling to a support surface, the base portion biased towards a neutral position defined along a central axis and pivotable to a plurality of angular positions relative to the central axis. The control input also includes a grip portion having inputs for controlling movement of the aircraft and pivotally coupled to the base portion, the grip portion pivotable between a first position in which the grip portion extends from the base portion and a second position in which the grip portion is pivoted relative to the base portion. Further, the control input includes a lock mechanism for locking the grip portion in the first position wherein releasing the lock mechanism allows the grip portion to move to the second position.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    FOLDING CONTROL STICK AND LOCKING MECHANISM


    Beteiligte:

    Erscheinungsdatum :

    2024-05-02


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    FOLDING CONTROL STICK AND LOCKING MECHANISM

    YERANT JOHN STEPHEN / BEAN TIMOTHY HEISING / POULIN STEPHEN V | Europäisches Patentamt | 2024

    Freier Zugriff

    Folding locking mechanism

    ZHU WANQUAN / YUAN JIALIANG | Europäisches Patentamt | 2024

    Freier Zugriff

    Folding joint locking mechanism

    ZHENG HANXIN | Europäisches Patentamt | 2024

    Freier Zugriff

    Folding mechanism, walking stick stool and walking stick stool shopping cart

    LIN ZIJIE | Europäisches Patentamt | 2015

    Freier Zugriff

    Locking mechanism and folding airfoil with locking mechanism

    ZHANG MENG / ZHANG MINGZHONG / LI WEI et al. | Europäisches Patentamt | 2020

    Freier Zugriff