An emergency evacuation system includes a first floatation device, an inflator operably coupled to the first floatation device, and a second floatation device coupled to the first floatation device. The inflator is configured to inflate the first floatation device to deploy the emergency evacuation system outside of a compartment, such as proximate to a door of a vehicle.
MULTI-STAGE EVACUATION SYSTEMS AND METHODS FOR AIRCRAFT
29.08.2024
Patent
Elektronische Ressource
Englisch
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