FIELD: aviation.
SUBSTANCE: proposed control system includes control member, actuating mechanism for motion of control member and drive. Control member is mounted rotatably for motion from neutral position when load of air flow on its surface is minimum and deflected up and down positions when load of air flow is maximum. Actuating mechanism includes rotor mounted on wing for rotation around axis passing in direction of wing chord and crank member whose tip is shifted relative to axis of rotation. Crank member tip is slidably connected with guide boom. Drive is designed for rotation of rotor and motion of control member due to sliding joint of crank member with guide.
EFFECT: maximum mechanical efficiency at maximum load of air flow on wing.
15 cl, 17 dwg
