AIRCRAFT FLIGHT CONTROL DEVICE Russian patent published in 2022 - IPC G05G5/03 

FIELD: aircraft engineering.

SUBSTANCE: invention relates to a flight control device of an aircraft. The invention relates to a device containing a control lever connected to a frame on which the first block connected to the frame is mounted, the second block connected to the first block, while the control lever is connected to the second block, the first transmission shaft mounted with the possibility of rotation relative to the frame, the first mechanism for connecting the control lever to the first transmission shaft so that the rotation of the control lever around the first axis (X) causes rotation of the first shaft around the fourth axis (A), the second transmission shaft mounted with the possibility of rotation relative to the frame, the second mechanism for connecting the control lever to the second transmission shaft so that the rotation of the control lever around the second axis (Y) causes the rotation of the second shaft around the sixth axis (D), the platform connected to the frame, while the second connection mechanism is rotatable on the platform and rotatable on the control lever.

EFFECT: claimed solution is aimed at ensuring the application of less force, noticeable at the level of the control lever while turning around the first (X) and second axes (Y) when controlling the flight of an aircraft without the need for additional hardware drives.

10 cl, 6 dwg