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
2023-04-26
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |