THE RUDDER OF THE AERODYNAMIC SURFACE OF THE AIRCRAFT Russian patent published in 2021 - IPC B64C13/30 B64C9/14 

FIELD: aircraft flight controls.

SUBSTANCE: rudder of the aerodynamic surface of the aircraft consists of front and rear links with mismatched axes of rotation, with a kinematic link for synchronizing the unidirectional rotation of the links. The axes of rotation of both links are located on the aerodynamic surface. The back link is axially compensated. A profiled slot is made between the front and rear rudder links. The axis of rotation of the front link is located behind the specified slot.

EFFECT: invention is aimed at increasing the efficiency of the rudder with a low power of the rudder drive or with no-booster control with the possibility of using kinematic links between the deviations of the rudder links based on the difference in the position of their axes of rotation.

3 cl, 6 dwg