FRAMEWORK Russian patent published in 2018 - IPC B64C13/30 B64C9/12 

FIELD: aviation.

SUBSTANCE: invention relates to winged aircraft. Airframe of the aircraft comprises a wing and a control system in the longitudinal channel, including a control element, hinged steering wheel and steering wheel. Reference rudder in flight is oriented in the direction of the oncoming stream. Control is installed with the possibility of changing the relative position of the elevator and the steering elevator. Steering link is made in the form of a control. Control is mounted on the glider with the ability to correlate the position of the elevator at a zero pitch moment acting on the glider of the aircraft. Glider contains divider, kinematic connections and control. Reference rudder and the steering wheel are linked through kinematic links. Design of the divider provides a deflection in the antiphase of the reference and steering elevator with the control unit stationary and the deflection of the reference and steering wheel height in phase with the deviation of the control from the neutral position.

EFFECT: invention is aimed at improving flight safety while ensuring a high level of fuel efficiency and simplicity of the piloting process.

1 cl, 4 dwg