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
2023-04-27
Patent
Electronic Resource
English