FIELD: aviation.
SUBSTANCE: invention relates to aircraft flight control means. Control member includes an aerodynamic surface, a rudder with an axis of rotation, a command lever with a tie-rod, a rudder frame which is assembled from the stiffening ribs arranged along the flow and side aerodynamic panels with possibility of successive shift of each of them relative to frame with formation of holes between panel and frame for air flow through steering wheel.
EFFECT: invention is aimed at reduction of hinge moment and force to command control lever.
1 cl, 2 dwg
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| FRAMEWORK | 2016 |
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