FIELD: vertical take-off and landing aircraft. SUBSTANCE: flying vehicle includes fuselage with air intake passages, aerodynamic planes partially mounted at angle of attack relative to flow of air, shield under them, drive with fans and tabs. Aerodynamic are located in air intake passages over perimeter of fuselage radially converging in trough-shaped under-fuselage cavity which is open downward. Shields close air intake passages at the bottom. EFFECT: simplified construction and increased load ratio. 1 dwg
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