FIELD: aeronautical engineering.
SUBSTANCE: proposed flying vehicle has fuselage 10 with tail 11, aerodynamic lifting tractor-type propeller mounted at side of tail 11, tail rotor 12 whose rotation shaft 13 is mounted horizontally and is turnable in horizontal plane through angle of 90°; it is also movable in vertical plane. Propeller axle 1 is shifted relative to horizontal plane of symmetry of fuselage 10 to side opposite to tail rotor 12 and is inclined from vertical through angle lesser than 10°. Tail rotor 12 may be made as two-stage version at opposite rotation of stages.
EFFECT: extended range of capabilities.
2 cl, 3 dwg
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