An emergency oxygen system for an internal cabin of a vehicle includes a housing including one or more compartments, and one or more oxygen assemblies. The one or more oxygen assemblies include a mask and a fluid conduit. The mask is configured to be stowed within and deployed from the one or more compartments. A door is moveably secured to the housing. The door is moveable between a closed position underneath the one or more compartments to secure the mask within the one or more compartments, and an open position during a deployment event in which the mask drops down and laterally out of the one or more compartments. The mask is configured to hang down from a portion of the door when the door is in the open position. The emergency oxygen assemblies can be separate and distinct from passenger service units (PSUs).


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    Title :

    EMERGENCY OXYGEN SYSTEMS FOR INTERNAL CABINS OF AIRCRAFT


    Additional title:

    NOTSAUERSTOFFSYSTEME FÜR FLUGZEUGINNENRAUM
    SYSTÈMES D'OXYGÈNE D'URGENCE POUR CABINES INTERNES D'AÉRONEFS



    Publication date :

    2024-10-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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