FIELD: transport.
SUBSTANCE: invention relates to rotorcraft, namely, to VTOL aircraft. Claimed plane comprises fuselage, tail unit and fin arranged at fuselage tail, cantilevers located nearby gravity centre on fuselage both sides, cowls, columns, rotors with blades, wobble plates and wobble plate automatic control means. Said cantilevers are coupled with fuselage by pivots which allow the turn angle variation in the range of 100 to minus 10 degrees relative to horizon irrespective of each other. Columns are coupled with the cantilevers and closed by the cowls. The rotors comprise blades with jet engines connected with columns by torsions secured on column shafts free running bearings. Said jet engines are arranged the blades overhang and provided with the nozzles directed toward the blade trailing edge.
EFFECT: control over convertiplane solely by wobble plates.
22 cl, 4 dwg, 1 tbl
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