FIELD: aviation.
SUBSTANCE: invention relates in particular to structures of the bearing elements of aircraft heavier than air. The aircraft comprises a body with a supporting device, for example, a landing gear, a propeller, a flight control system, at least one engine, and one rotor-type carrier wing placed on the body. The rotary wing has a drive and a device for regulating the speed of rotation, as well as a device for blowing the wing with its own drive. The rotor wing and the device for blowing it are placed in a box open in the front and rear parts, and the device for blowing the wing can be installed anywhere in the box - both in front of the wing and behind it.
EFFECT: increased manoeuvrability of the apparatus in flight, the possibility of its vertical take-off and landing, and a reduction in specific energy consumption for cargo transportation.
9 cl, 2 dwg
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