| 摘要 |
There is declared an aircraft with a lifting fuselage, comprising a wing, on outboard wing panels of which there are mounted engines, the fuselage width is considerably more than its height, but a front portion of the fuselage in plane smoothly transforms from a narrower nose portion into a wide base portion, therewith, the tail assembly has two stabilizers with control surfaces, the stabilizers are spaced from one another along the fuselage width aside from the longitudinal vertical plane of the aircraft and are installed at angle with respect to it, on each of the stabilizers it is installed an all-movable arrow-type yaw rudder with forming a T-shaped tail assembly, the axis of turn of said yaw rudder is positioned on the stabilizer in the plane of the yaw rudder, but construction planes of the stabilizers intersect with one another in the plane of the aircraft symmetry plane on the base longitudinal axis of the aircraft or below it.
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