Full authority fly-by-wire pedal system

Details Full authority fly-by-wire pedal system Full authority fly-by-wire pedal system

B - Operations, Transporting

64

C

B64C 19/02 (2006.01)

Patent

CA 2632130

A pedal system particularly tailored to a Fly-By-Wire (FBW) flight control system includes a double gradient linkage assembly. The double gradient linkage assembly includes a damper system and a spring system that improves yaw axis (azimuth) control of the aircraft. Control is only required when a change in the yaw axis state is demanded. Since only minimal displacement inputs to such a FBW flight control system is required, the travel of the pedals are exceeding compact, such that pilot workload is significantly reduced through the reduction in the frequency and magnitude of aircraft control inputs.

L'invention concerne un système de pédales particulièrement adapté à un système de commandes de vol électriques (Fly-By-Wire-FBW) qui comprend une timonerie à double gradient. La timonerie à double gradient comprend un système d'amortisseur et un système de ressort qui améliorent la commande d'axe de lacet (azimut) de l'avion. Une commande est uniquement nécessaire lorsqu'un changement dans l'état de l'axe de lacet est demandé. Étant donné que seules des entrées de déplacement minimal à un tel système de commandes de vol FBW sont nécessaires, le trajet des pédales est extrêmement compact, de telle sorte qu'une charge de travail du pilote est significativement réduite grâce à la réduction de la fréquence et de l'amplitude des entrées de commandes d'un avion.

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