An inflatable slide for use in an emergency evacuation system of an aircraft includes a main body having a top surface and a bottom surface and that is configured to inflate in response to receiving a flow of fluid. The inflatable slide further includes a first lanyard coupled to the main body. The inflatable slide further includes an airfoil coupled to the first lanyard and configured to exert a force on the main body in a downward direction corresponding to a direction of gravity in response to receiving a wind flow.


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    Titel :

    EVACUATION SLIDE ROTATION INDUCER


    Beteiligte:
    KRUTS IVAN (Autor:in) / VOLNY JARO S (Autor:in) / HARTMAN DREW (Autor:in)

    Erscheinungsdatum :

    2018-09-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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