An emergency evacuation system (102) is configured to be stored in a compartment below an exit door of an aircraft (10). The emergency evacuation system (102) includes a first floatation device including an internal inflator (126), and a second floatation device including an open inflation system (130). The second floatation device is coupled to the first floatation device.


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    Titel :

    MULTI-STAGE EVACUATION SYSTEMS AND METHODS FOR AIRCRAFT


    Weitere Titelangaben:

    MEHRSTUFIGE EVAKUIERUNGSSYSTEME UND -VERFAHREN FÜR FLUGZEUGE
    SYSTÈMES ET PROCÉDÉS D'ÉVACUATION MULTI-ÉTAGES POUR AÉRONEF


    Beteiligte:

    Erscheinungsdatum :

    26.04.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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