FLAP ACTUATOR

摘要

A flap actuator is provided for controlling movement of a flap on a wing of an aircraft. The flap actuator includes a shaft extending along a longitudinal axis and having a terminal end operatively connectable to the flap. The shaft is movable between a first retracted position and a second extended position. A no-back assembly is operatively connectable to the shaft. The no-back assembly prevents movement of the shaft toward the retracted position in response to a compressive force generated by the flap.