FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft, in particular to the design of a disassemblable unmanned aerial vehicle. Aircraft type unmanned aerial vehicle (UAV) contains fuselage, located in the fuselage rear cavity sustainer module, onboard equipment arranged at least in front cavity of fuselage, wing attached to fuselage, beams attached to wing and containing fin and electric motors, stabilizer attached to beams, and supports attached to fuselage. Fuselage is a monocoque made of composite materials and containing a wing coupling assembly located above the fuselage and containing fasteners for attaching the wing, a central frame made in the form of a ring from a profile covering the fuselage inner surface in the region under the wing coupling assembly, 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
Title | Year | Author | Number |
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FUSELAGE OF UNMANNED AERIAL VEHICLE | 2024 |
|
RU2838933C1 |
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FUSELAGE OF UNMANNED AERIAL VEHICLE | 2024 |
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VERTICAL TAKE-OFF AND LANDING (VTOL) UNMANNED AERIAL VEHICLE WING CENTRE SECTION | 2024 |
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UNMANNED AERIAL VEHICLE AND METHOD OF ITS ASSEMBLY | 2024 |
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WING OF AIRCRAFT-TYPE UNMANNED AERIAL VEHICLE WITH VERTICAL TAKEOFF AND LANDING (VTOL) | 2024 |
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RU2830730C1 |
WING CENTRE SECTION OF AIRCRAFT-TYPE UNMANNED AERIAL VEHICLE WITH VERTICAL TAKE-OFF AND LANDING (VTOL) | 2024 |
|
RU2828443C1 |
BEAM OF AIRCRAFT-TYPE UNMANNED AERIAL VEHICLE WITH VERTICAL TAKE-OFF AND LANDING (VTOL) | 2024 |
|
RU2830728C1 |
WING CONSOLE OF AIRCRAFT TYPE UAV WITH VERTICAL TAKE-OFF AND LANDING (VTOL) | 2024 |
|
RU2828508C1 |
Authors
Dates
2025-04-24—Published
2024-10-03—Filed