FUSELAGE OF 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. Unmanned aerial vehicle (UAV) fuselage is a monocoque made of composite materials, and contains a cavity for the onboard equipment accommodation in the fuselage front part, space for sustainer module to be located at fuselage rear and wing joint assembly arranged atop fuselage and including fasteners for wing attachment. Fuselage also contains a central frame made in the form of a ring from the profile enclosing the fuselage inner surface in the area under the interface with the wing, and a rear frame made in the form of a ring from a profile covering the fuselage inner surface at the edge of its rear part.

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

7 cl, 7 dwg