The wing combined with the fly wheel-equipped rotating wing for improvement of the wing stability.

摘要

The present invention relates to a fixed wing with improved stability combined with a rotor blade having an inertia wheel, and more particularly, in the fixed blades of the main blade of the aircraft, such as aircraft, glider, kite, by combining the rotor blades integrally with the inertia wheel It utilizes the rotational lift and balance restoring action of the rotor blade without lifting loss to maximize the stability of the fixed wing, absorbs the strong wind energy, absorbs the stall speed, lowers the stall speed, the parachute in case of a sudden descent, shortening and takeoff and landing distance, etc. It is characterized by the stability of the fixed wing structure combined with a rotor blade having the inertial wheels to provide a low speed low-flying aircraft with excellent stability that is impossible with the conventional fixed wing aircraft.