A decompression panel for use in a door of an aircraft disclosed herein includes bi-directional latching mechanisms. A differential pressure sensor disengages upon a decompression event in a compartment of an aircraft, allowing latch hooks to disengage from a panel latch of the decompression panel. Once disengaged, the decompression panel can rotate to vent air in a compartment of higher pressure to the compartment experiencing the decompression event.


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    Titel :

    Decompression panel and latch


    Beteiligte:
    BARRETT CASEY J (Autor:in) / NGUYEN KHOA DUY (Autor:in) / WOLF MARK A (Autor:in) / WU ANDREW H (Autor:in)

    Erscheinungsdatum :

    2015-08-25


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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