FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft designs of small aircraft engineering. Gyroplane consists of a fuselage, a wing, a spinning system for propeller rotor blades, rudder and chassis. Wing is made from composite material of streamlined curved shape in the form of isosceles triangle, top of which is directed to rear part of gyroplane, at that lateral tops of isosceles triangle are truncated. Wing is attached to tie rods located behind spinning system for propeller rotor blades. At that wing and spinning system for propeller rotor blades have feedback with control handle of pilot by gyroplane.
EFFECT: considerable reduction of the vibrations occurring during flight on the pilot control handle, improved controllability and reduced fatigue loads on the pilot hands during piloting.
1 cl, 4 dwg
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