FUSELAGE OF VERTICAL TAKEOFF AND LANDING (VTOL) UNMANNED AERIAL VEHICLE Russian patent published in 2025 - IPC B64U20/50 B64C1/26 

FIELD: aircraft engineering.

SUBSTANCE: invention relates to aircraft, in particular to the design of a disassemblable unmanned aerial vehicle. Fuselage of an unmanned aerial vehicle with vertical take-off and landing (VTOL) is a monocoque made of composite materials and comprising a cavity for accommodating on-board equipment in the front part of the fuselage, cavity for accommodation of sustainer module in fuselage rear part, wing junction unit is arranged above fuselage and comprises fasteners for wing attachment. Central frame made in the form of a ring from the profile covering the fuselage inner surface in the area under the wing interface, rear frame made in the form of a ring from a profile enveloping the inner surface of the fuselage at the edge of its rear part and embedded elements at the bottom of the fuselage for fastening the supports. Wherein said front insert element arranged at fuselage front is provided with at least one lengthwise guide to secure onboard equipment without contact with the other fuselage part.

EFFECT: simplified and accelerated assembly/disassembly of UAV, higher reliability and safety of disassemblable UAV.

6 cl, 7 dwg