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
2025-06-17
Patent
Electronic Resource
English