An aircraft rudder pedal includes a frame, a pair of pedals, an output shaft and a mechanical kinematic chain for transmitting to the output shaft a displacement of at least one of the pedals relative to the frame. The mechanical kinematic chain comprises a central transmission part able to be rotated relative to the frame by a displacement of one of the pedals relative to the frame. The mechanical kinematic chain also includes a transmission mechanism joining the central transmission part to the output shaft. The transmission mechanism includes a homokinetic association of two universal joints between said central transmission part and the output shaft.
PALONNIER D'AÉRONEF AVEC CHAÎNE CINÉMATIQUE MÉCANIQUE DE TRANSMISSION
AIRCRAFT RUDDER BAR WITH MECHANICAL TRANSMISSION DRIVE TRAIN
FLUGZEUGSPREIZER MIT MECHANISCHEM ANTRIEBSSTRANG
30.07.2025
Patent
Elektronische Ressource
Französisch
IPC: | B64C AEROPLANES , Flugzeuge |
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