A door assembly configured to be positioned between a first compartment and a second compartment that includes a main door portion having a first decompression opening defined therein, at least a first panel portion positioned in a first position within the first decompression opening, and a decompression sensor. The first panel portion is movable linearly between the first position and a second position and is pivotable between the second position and a third position. In the third position the first compartment is in fluid communication with the second compartment via the first decompression opening.


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    Titel :

    Aircraft door with sliding decompression panel


    Beteiligte:
    SATTAYATAM PANADE (Autor:in) / TANG HAI V (Autor:in)

    Erscheinungsdatum :

    05.04.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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