An aircraft door architecture having: a door (1); an ejector (3); an inflatable evacuation device (4); an emergency energy source (6) connected to the ejector (3) and to the inflatable evacuation device (4); a control unit (9) having the two following operating states: a nominal operating state in which the inflatable evacuation device (4) is kept in its retracted position and the emergency energy source is deactivated; an emergency operating state in which the emergency energy source (6) activates the actuation device of the ejector (3) in an emergency opening mode of the door (1), and activates the inflation device of the inflatable evacuation device (4) in an emergency inflation mode.
ARCHITECTURE DE PORTE D'AERONEF COMPORTANT UNE SOURCE D'ENERGIE DE SECOURS
AIRCRAFT DOOR ARCHITECTURE COMPRISING AN EMERGENCY ENERGY SOURCE
FLUGZEUGTÜRARCHITEKTUR MIT EINER NOTENERGIEQUELLE
2025-05-21
Patent
Electronic Resource
French
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