FIELD: aircraft industry.
SUBSTANCE: invention relates to aircraft flight controls. The aerodynamic rudder consists of a front and rear links, one of which is supported during its rotation on the other, with a rear link made with axial compensation, with a profiled gap between the rudder links.
EFFECT: invention increases 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.
6 cl, 11 dwg
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