FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to VTOL unmanned aerial vehicle. Multi-rotor VTOL aircraft comprises left and right side compartments connected by inner side walls by means of wings. Groups of front, rear, first central and second central engine-engine-propeller pairs, containing at least one propeller and one engine, are symmetrically located on the left and right side compartments using rigid brackets. First central and second central engine-propeller pairs are secured on outer lateral sides of side compartments in opposite directions from aircraft vertical axis.
EFFECT: improved flight characteristics of aircraft, reduced power consumption in all flight modes.
2 cl, 7 dwg
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