A pitch control system configured to vary a pitch angle of a plurality of propeller blades of a propeller system is provided including a motor having a motor shaft configured to rotate about an axis. A rotary switch having a tab protruding generally outwardly is coupled to the motor shaft and is configured to move between a first position and a second position. The pitch control system also includes a position sensor configured to monitor the position of the rotary switch. The position of the rotary switch is proportional to the pitch angle of the plurality of propeller blades.
PITCH CONTROL SYSTEM
ANSTELLWINKELSTEUERUNGSSYSTEM
SYSTÈME DE COMMANDE DE PAS
2018-04-25
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |