A landing gear control lever system including a lever assembly, a locking assembly, and a switch assembly is disclosed herein. The locking assembly is connected to the lever assembly. The locking assembly has a rotary actuator and a Scotch yoke member operably connected to a portion of the rotary actuator such that rotation of the rotary actuator causes linear movement of the Scotch yoke member. The locking assembly can further include a locking arm operably coupled to the Scotch yoke member and moveable between locked and unlocked positions upon rotation of the rotary actuator.
LANDING GEAR CONTROL SYSTEM
FAHRWERKSTEUERUNGSSYSTEM
SYSTÈME DE COMMANDE DE TRAIN D'ATTERRISSAGE
2018-10-03
Patent
Elektronische Ressource
Englisch