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
27.04.2023
Patent
Elektronische Ressource
Englisch
Multi-stage evacuation systems and methods for aircraft
Europäisches Patentamt | 2024
|MULTI-STAGE EVACUATION SYSTEMS AND METHODS FOR AIRCRAFT
Europäisches Patentamt | 2024
|Multi-stage evacuation systems and methods for aircraft
Europäisches Patentamt | 2024
|MULTI-STAGE EVACUATION SYSTEMS AND METHODS FOR AIRCRAFT
Europäisches Patentamt | 2023
|MULTI-STAGE EVACUATION SYSTEMS AND METHODS FOR AIRCRAFT
Europäisches Patentamt | 2023
|