FIELD: control systems.
SUBSTANCE: invention relates to aircraft flight control means. Controller includes deflectors – wings, installed in front of the steering wheel with axial compensation along the aerodynamic surface next to its rear. Front edge of the deflectors is in front of the gap between the aerodynamic surface and the steering wheel. Additionally, the shaping of the cutout in front of the steering wheel can be selected on the aerodynamic surface. Deflectors – the wings can be installed both on one and both sides of the steering wheel, as well as in the retracted state in niches on the aerodynamic surface. Deflectors can be fixed motionless or move and rotate when the rudder deflects.
EFFECT: invention is aimed at increasing the efficiency of the helm with axial aerodynamic compensation at a small hinge moment.
5 cl, 6 dwg
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