A rope deployment mechanism for use on an aircraft is provided. The present invention includes a mounting bracket attachable to the aircraft. An arm assembly is pivotally connected to the mounting bracket about a vertical axis. A rope connector is disposed at an end of the arm assembly. The present invention further includes a dual link, compass style mechanism connecting the arm assembly to the support bracket and a locking mechanism operable to lock the rope deployment mechanism in a retracted position and a deployed position. Using the invention, the arm assembly may be pivoted to a deployed position, locked in the deployed position, and a rope may be attached to the rope connector all using one hand.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ROPE DEPLOYMENT MECHANISM FOR AN AIRCRAFT


    Beteiligte:
    BALTEN OVID (Autor:in)

    Erscheinungsdatum :

    29.12.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Rope deployment mechanism and method

    HAINSWORTH BARTON J / WISLOCKI ROBERT | Europäisches Patentamt | 2020

    Freier Zugriff

    ROPE DEPLOYMENT MECHANISM AND METHOD

    HAINSWORTH BARTON J / WISLOCKI ROBERT | Europäisches Patentamt | 2019

    Freier Zugriff

    ROPE DEPLOYMENT MECHANISM AND METHOD

    HAINSWORTH BARTON J / WISLOCKI ROBERT | Europäisches Patentamt | 2017

    Freier Zugriff

    ROPE DEPLOYMENT MECHANISM AND METHOD

    HAINSWORTH BARTON J / WISLOCKI ROBERT | Europäisches Patentamt | 2016

    Freier Zugriff

    Quick rope assisted deployment and extraction apparatus

    COCKELL II ROBERT C | Europäisches Patentamt | 2015

    Freier Zugriff