A wing panel actuator assembly comprising: an actuator housing (40); an actuator piston (50) arranged in the actuator housing and axially movable relative to the actuator housing; a connecting rod (60) attached, at one end (62), to an end (51) of the piston extending from the actuator housing; the actuator housing and piston arranged to be accommodated inside a movable panel (2) of an aircraft wing, the connecting rod arranged to be attached, in use, at its end (61) opposite the one end (62) attached to the piston, to a wing structure of the aircraft wing, the panel being pivotable about a pivot point P relative to the wing structure (1) by means of the actuator piston.
FLIGHT CONTROL ACTUATOR
ACTIONNEUR DE COMMANDE DE VOL
2023-09-01
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |