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.
MULTI-STAGE EVACUATION SYSTEMS AND METHODS FOR AIRCRAFT
MEHRSTUFIGE EVAKUIERUNGSSYSTEME UND -VERFAHREN FÜR FLUGZEUGE
SYSTÈMES ET PROCÉDÉS D'ÉVACUATION MULTI-ÉTAGES POUR AÉRONEF
26.04.2023
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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