A pressure equalization vent (314) for use in an aircraft assembly (102) is provided. The pressure equalization vent includes an opening (500) having a first end (502) and a second end (504) opposite the first end, and a first side (506) and a second side (508) opposite the first side. The vent further includes a plurality of louvers (510) positioned within the opening. Each louver is positioned a predetermined distance (d) from an adjacent louver to form a gap (512) therebetween. Each louver includes an airfoil-shaped cross-section configured to increase airflow efficiency across the vent.


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    Titel :

    Pressure equalization vent for use in an aircraft assembly


    Beteiligte:

    Erscheinungsdatum :

    2015-07-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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