A fixed-wing aircraft at least includes at least one vortex generator movable through an outer surface of the aircraft between a retracted state and a fully extended state by at least one electric motor, the at least one electric motor being exclusively adapted to actuate this at least one vortex generator, and including an electronic control unit adapted to control operation of the at least one electric motor for actuation of the at least one vortex generator.
Aircraft having retractable vortex generators
29.04.2025
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |