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. Fuselage of the unmanned aerial vehicle is a monocoque made of composite materials and contains a cavity for arrangement of 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. Fuselage also comprises a central frame made in the form of a ring from a profile enclosing the fuselage inner surface in the area under the interface with the wing, 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 rear insert arranged at fuselage rear makes the support for sustainer engine module.

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

6 cl, 7 dwg