Disclosed is a blade lock assembly, which may include a drag brace coupled to a fold crank assembly and to a rotary wing blade and may further include an actuator assembly configured to be coupled to a rotary wing cuff. The actuator assembly may include an actuator pin housing, an actuation pin at least partially sheathed by the actuator pin housing, and an actuator configured to extend and retract the actuation pin away from and toward the actuator pin housing.
Chord lock assembly for a tiltrotor aircraft
2024-12-10
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |