A fixed-wing aircraft (1) at least comprises at least one vortex generator (6, 7, 8, 11) movable through an outer surface of the aircraft (1) between a retracted state and a fully extended state by at least one electric motor (12), this at least one electric motor (12) being exclusively adapted to actuate this at least one vortex generator (6, 7, 8, 11), and comprises an electronic control unit (13) adapted to control operation of the at least one electric motor (12) for actuation of the at least one vortex generator (6, 7, 8, 11).
AIRCRAFT HAVING RETRACTABLE VORTEX GENERATORS
FLUGZEUG MIT EINZIEHBAREN WIRBELGENERATOREN
AÉRONEF DOTÉ DE GÉNÉRATEURS DE VORTEX ESCAMOTABLE
2022-07-27
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |