An inflatable slide for use in an emergency evacuation system of an aircraft includes a main body having a top surface and a bottom surface and that is configured to inflate in response to receiving a flow of fluid. The inflatable slide further includes a first lanyard coupled to the main body. The inflatable slide further includes an airfoil coupled to the first lanyard and configured to exert a force on the main body in a downward direction corresponding to a direction of gravity in response to receiving a wind flow.
EVACUATION SLIDE ROTATION INDUCER
2018-09-06
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |