THE AIRCRAFT SUPPORTING THE WING AT BOTH ENDS Russian patent published in 2012 - IPC B64C39/04 

FIELD: aeronautics.
SUBSTANCE: aircraft includes a main body, the right building, located on one side of the main body, left body that located on the other side of the main body. The front ends of left and right housings are located behind the front end of the main body. The wing is supported by the main body, right body and left body and has a front end, which is located behind the front left and right ends of buildings. Air channel is defined in the longitudinal direction of the aircraft surface of the lower part of the wing and the inner side surfaces of left and right blocks. The horizontal stabilizer is turned to the wing near the gap, formed between the front edge of the horizontal stabilizer and the trailing edge of the wing and the wing upside down relative to the vertical cross section. Device that creates traction is in the interval, the vertical fin in the middle of the horizontal stabilizer, rudder at the rear end of the vertical fin and the elevator in the back end of the horizontal stabilizer.

EFFECT: stable flight at low speed.

9 cl, 4 dwg