WIDE-BODY AIRCRAFT WING (VERSIONS) Russian patent published in 2015 - IPC B64C17/02 B64C9/02 B64C3/32 

FIELD: aircraft engineering.

SUBSTANCE: claimed wing comprises the carcass, skin, top and bottom airfoils, airflow deflectors and turbojet/jet engine. In compliance with the first version, carcass has the round through hole provided with hollow disc running on disc exposed to incident airflow and having the rim, convexed top airfoil and flat bottom airfoil. Annular slot is arranged between said disc and the carcass. Disc holder is fixed to the carcass along the fuselage axial line. Said holder is composed of top and bottom ribs with the flange for drive revolution. In compliance with the second version, the round through opening for yaw rudder shaft fitted from the side of bottom airfoil. Said yaw rudder is arranged from the side of the bottom/top airfoils.

EFFECT: higher lift and in-flight stability.

2 cl, 5 dwg