An evacuation system is provided. The system may comprise a girt coupled to a door sill and an evacuation slide. The evacuation slide may comprise a head end coupled to the girt, an extension, a hinge portion coupled between the head end and the extension, and a lane diverter coupled to the evacuation slide. A method is also provided. The method may include opening a door to expose a door sill, inflating the evacuation slide with the evacuation slide coupled to the door sill, bending a hinge portion of the slide in response to a door sill height being less than or equal to a predetermined height, and redirecting a slide lane to a side exit.


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    Titel :

    Aircraft sill height compensating evacuation system


    Beteiligte:
    HARTMAN DREW (Autor:in) / VOLNY JARO (Autor:in)

    Erscheinungsdatum :

    2017-11-07


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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