Patent ID: 8544790

Claim:
An aircraft comprising a fuselage and main aircraft elements connected thereto, in particular, takeoff and landing wings; horizontal nose stabilizers; horizontal tail stabilizers; vertical tail fin, and engines, the takeoff and landing wings being connected to the fuselage through fitting units having shafts possessing one degree of freedom and positioned above the middle line of the fuselage along the longitudinal axis of symmetry thereof for the takeoff and landing wings to turn relative to their respective axes of the fitting units for moving the takeoff and landing wings to the unfolded position thereof at takeoff and landing or to the folded position in cruising flight and at parking, the takeoff and landing wings being positioned when folded below the fitting units along the longitudinal axis of symmetry of the fuselage, the outer surface of the takeoff and landing wings being extensions of the outer surface of the fuselage, and the folded takeoff and landing wings covering at least 30% of the area of the fuselage surface between the horizontal nose stabilizers and the horizontal tail stabilizers.