An inflatable evacuation device for an aircraft may include at least one chamber (22, 24) and at least one canopy support (50) in fluid communication with the at least one chamber. A retention device (52) may be configured to restrict inflation of the at least one canopy support during inflation of the at least one chamber.
INFLATABLE EVACUATION SYSTEM WITH CANOPY SUPPORT
AUFBLASBARES EVAKUIERUNGSSYSTEM MIT DACHUNTERSTÜTZUNG
SYSTÈME D'ÉVACUATION GONFLABLE AYANT UN SUPPORT D'AUVENT
2022-03-16
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Telescopic canopy support for an inflatable evacuation device
Europäisches Patentamt | 2019
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