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

摘要

The present invention combines the stability of the wheel inertia flywheel with enhanced fixed-wing , in more detail aircraft , gliders , etc. in the year of the main wing fixed-wing aircraft , combined with the flywheel inertia wheel integrally nophyeo possible by the stability of fixed-wing ever used with a rotary action of the rotary-wing lift and balance recovery without loss of lift fixed-wing that effect , the energy absorption cushioning effect of the intense winds , the effect of lowering the stall speed , crashed during a dive parachute effect , take-off and landing distances , such as shortening effect been made for the safe low-speed low-altitude flying aircraft that can provide excellent stability with non- conventional fixed-wing aircraft as this combined with the stability flywheel inertia wheel is characterized in the structure of the improved fixed-wing .