HYBRID AIRCRAFT Russian patent published in 2019 - IPC B64C27/22 B64B1/34 B64C29/00 

FIELD: aviation.

SUBSTANCE: invention relates to the field of aviation, in particular, to structures of vertical take-off and landing aircraft, using as aerostatic and aerodynamic lifting force of a shell with a carrier gas and thrust propulsion. Hybrid aircraft contains a power frame, shells with a carrier gas, engines with screws, controls, cabin. Cabin is located under the power frame, shells with a carrier gas during the flight – over the power frame, have aerostatic lifting force equal to at most half the dry weight of the aircraft. Carrier gas shells are equipped with a displacement device from the upper position to the lower position relative to the carrier frame, and the dimensions and shape of the shells provide aerodynamic lifting force during horizontal flight and the necessary area for a smooth decline in an emergency.

EFFECT: possibility of landing on slopes, loose surfaces and on the water, mooring to high-altitude objects.

1 cl, 2 dwg