MULTICOPTER WITH FULL-TURN RUDDER, HYBRID PROPULSION SYSTEM AND COMBINED ENGINE-PROPELLER GROUPS Russian patent published in 2024 - IPC B64U10/14 B64C27/08 

FIELD: aviation.

SUBSTANCE: invention relates to designs of unmanned aerial vehicles. Multicopter with full-turn rudder, hybrid propulsion system and combined engine-propeller groups comprises chassis, on which there is an internal combustion engine (ICE) connected to a generator, and at least four engine-propeller groups made in the form of FPV-drones with electric motors located on top of multicopter beams. Said at least four FPV-drones can be separated from multicopter. FPV-drones have at least four engine-propeller groups with electric motors having each propeller. From below on beams of multicopter there located are engine-propeller groups of multicopter directly, propellers of electric motors of which are located in parallel planes. Thrust generated by the multicopter engine-propeller group propeller directly corresponds at least to the thrust of the propellers of the FPV-drone electric motors.

EFFECT: higher load capacity and range, higher flight safety and control efficiency.

3 cl, 7 dwg