FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft engineering, namely, to VTOL aircraft. Aircraft comprises a bearing frame of a spatial structure, a seat, controls, propulsion units, a control system, a remote control system. Base bearing frame is made with a central part and with at least two peripheral clusters. Central part and the peripheral clusters of the frames are made as a spatial structure. Each peripheral cluster is made as a truss structure of at least three identical segments connected to each other. Inside each segment there is a propulsion unit containing at least one engine and at least one propeller of horizontal rotation.
EFFECT: use of the invention provides higher fault tolerance and safety, better reparability of the vertical take-off and landing aircraft.
24 cl, 12 dwg
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