FIELD: aircraft engineering.
SUBSTANCE: group of inventions refers to an adaptive flight control system for an aircraft, a pusher propeller power transmission system and aircraft. Adaptive control system includes a control means, a control mechanism, control means with a control rod, data return means for the flight control system. Pusher propeller power transmission system comprises an adaptive flight control system and a pusher propeller gear box. Aircraft comprises a flight control system, a flight mechanism, a pusher propeller power transmission system, a mechanical kinematic flight control circuit, arranged in a certain way.
EFFECT: improved reliability of the adaptive flight control system.
16 cl, 6 dwg
