An inflatable evacuation device for an aircraft may include at least one chamber and at least one canopy support in fluid communication with the at least one chamber. A retention device 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
2018-03-22
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
|