AIRCRAFT CONTROL SYSTEM Russian patent published in 2017 - IPC B64D31/04 B64C13/04 

FIELD: aviation.

SUBSTANCE: aircraft control system contains the steering wheel, the steering column and at least one traction control body with the electric drive. The traction control body is structurally connected to the aircraft power plant, and the electric drive is installed with the possibility of the traction control body moving. The traction control body includes the switching facilities with two lobes, mounted to the left and right from the steering wheel symmetry plane with the possibility to control the traction control body position. The switching facilities are made in the form of three-position switch, containing the switch housing, the contact group, the return springs with rods and the traverse. The petals are mounted on the traverse, the traverse is hingedly mounted in the switch housing and spring-loaded by the return springs. The contact group is mounted on the switch housing and the traverse, and it is connected to the electric drive with the possibility of the handle electric drive reversing, and the switch housing is installed between the steering wheel and the steering column.

EFFECT: power plant traction control convenience is improved, simplification of the training and reduction of the pilot errors probability.

7 cl, 4 dwg