An emergency evacuation system is configured to be stored in a compartment below an exit door of an aircraft. The emergency evacuation system includes a first floatation device including an internal inflator, and a second floatation device including an open inflation system. The second floatation device is coupled to the first floatation device.
Multi-stage evacuation systems and methods for aircraft
04.06.2024
Patent
Elektronische Ressource
Englisch
Multi-stage evacuation systems and methods for aircraft
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