FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to structures of flying platforms. Hybrid multi-rotor flying platform comprises mounting frame, on which four motors are installed in pairs, diametrically opposite to each other, on each of which there installed on the top are one screw propeller of angular stabilization. Electric motors are connected to onboard storage battery via flight microcontroller. At least two hinged aerodynamic steering wheels are installed under the frame, under angular stabilization screws, diametrically opposite to each other, with steering machines that are electrically connected to the flight microcontroller. Four rotors connected via coupling with internal combustion engine shaft, which is fixed under the frame in the center, are installed under the frame between angular stabilization air screws, in pairs, diametrically opposite to each other. Shaft of internal combustion engine is mechanically connected to electric generator connected to onboard accumulator battery.
EFFECT: enabling increase in the multi-rotor platform flight capacity and duration.
1 cl, 1 dwg
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Authors
Dates
2020-01-14—Published
2019-03-06—Filed