AIRCRAFT Russian patent published in 2017 - IPC B64C13/46 B64C25/28 

FIELD: aviation.

SUBSTANCE: aircraft contains a glider, power unit, control system in bank, pitch and yawing channels, a control station with pedals and a chassis made in the form of at least two supports. The aircraft also contains display means structurally connected to the pedals and mounted to transfer kinesthetic information about the change of the position of the chassis supports to the pilot's feet by moving the pedals. The control station contains main hydraulic cylinders, and the pedals are made in the form of control pedals, each of which consists of a base and a platform. The main hydraulic cylinders are installed on pedal bases and are kinematically connected to the platforms. The chassis support comprises of a brake mechanism (14) of the wheel (5), including a working (8) hydraulic cylinder. The display means are in the form of feedback hydraulic cylinders (15). The working cavities of the feedback hydraulic cylinders (15) communicate with the main and working (8) hydraulic cylinders. One end of the feedback hydraulic cylinder (15) is fixed to the pivoting arm (10) of the chassis support, and the second - to the glider.

EFFECT: invention improves piloting of an aircraft, increases flight safety.

3 cl, 4 dwg