An emergency evacuation system is configured to be stored in a compartment below an exit door of a vehicle, such as an aircraft. The emergency evacuation system includes a first floatation device, a second floatation device, and a regulation device configured to sequentially direct gas to the first floatation device and the second floatation device.


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    Titel :

    Multi-stage evacuation systems and methods for aircraft


    Beteiligte:

    Erscheinungsdatum :

    24.12.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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