A decompression assembly (10) for use in an aircraft comprises a cabin lining element (12), an opening (18) formed in the cabin lining element (12), and an air channel (22) which is arranged adjacent to a rear face (24) of the cabin lining element (12) and connected to the opening (18) formed in the cabin lining element (12). The air channel (22) is provided with an air outlet (28) which, during normal operation of the decompression assembly (10), is adapted to discharge air exiting an aircraft cabin region (26) delimited by the cabin lining element (12) through the opening (18) formed in the cabin lining element (12) into an aircraft area (30) located between the cabin lining element (12) and an aircraft outer skin (32), a first decompression opening (42), and a first decompression flap (46) which, during normal operation of the decompression assembly (10), is adapted to close the first decompression opening (42) provided in the air channel (22) and which, in the event of a rapid decompression, is adapted to open the first decompression opening (42) so as to allow a pressure equalization between the aircraft cabin region (26) delimited by the cabin lining element (12) and the aircraft area (30) located between the cabin lining element (12) and the aircraft outer skin (32).


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    Titel :

    DECOMPRESSION ASSEMBLY WITH AN AIR CHANNEL


    Weitere Titelangaben:

    DEKOMPRIMIERUNGSANORDNUNG MIT EINEM LUFTKANAL
    ENSEMBLE DE DÉCOMPRESSION AVEC UN CANAL D'AIR


    Beteiligte:
    SCHNEIDER UWE (Autor:in)

    Erscheinungsdatum :

    2020-04-08


    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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