Rudder pedal and brake inceptor devices are described that utilize a straight-line mechanism and rotary joints to achieve straight line motion in a compact volume. The devices can include four or more bar linkages that translate forward motion of a pedal into a rotary motion of a common shaft, such that forward motion of one pedal causes the other pedal to retract while allowing for yaw motion control of the aircraft.
RUDDER PEDAL DEVICE
RUDERPEDALVORRICHTUNG
DISPOSITIF DE PÉDALES DE PALONNIER
2025-08-06
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |