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
FLUGZEUG MIT EINZIEHBAREN WIRBELGENERATOREN
AÉRONEF DOTÉ DE GÉNÉRATEURS DE VORTEX ESCAMOTABLE
2024-10-23
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |