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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    Title :

    MULTI-STAGE EVACUATION SYSTEMS AND METHODS FOR AIRCRAFT


    Additional title:

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


    Contributors:

    Publication date :

    2023-04-26


    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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