FIELD: aviation.
SUBSTANCE: invention relates to aviation, specifically to multi-rotor rotary-wing aircraft (AC) with vertical take-off and landing. A vertical take-off and landing aircraft with additional cargo modules and retractable propellers contains a fuselage, a cockpit, main wing, empennage, propeller-driven groups to create lift and thrust, a power plant for power supply, propeller-driven groups with controllers, a flight computer, a sensor system for flight monitoring and control, avionics, rescue system and other flight and safety systems. At the same time, additional cargo modules with retractable propellers are attached to the aircraft, providing lift sufficient for take-off/landing and hovering of the aircraft with additional aerodynamic resistance modules during cruise flight.
EFFECT: increase in the carrying capacity and useful volume of the aircraft fuselage while maintaining the economy of cruise flight.
1 cl, 8 dwg
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Authors
Dates
2021-11-09—Published
2021-05-24—Filed