FIELD: aircraft engineering.
SUBSTANCE: invention relates to aviation technology. The robotic universal aviation system contains a load-bearing system, including the fuselage, wing, tail, nacelles with placed propulsion systems (6), a retractable landing gear (7, 8). An unmanned automated control system is located in the nose of the fuselage. At the rear of the nose and on the front section of the tail part of the fuselage there are fastening locks unified with the universal module-container fastening systems in the horizontal plane, while the placement of fastening locks in the vertical plane in the ventral space provides the possibility of using the universal module-container as a suspended container and as a payload.
EFFECT: increased efficiency and safety of the movement of people and goods is achieved.
5 cl, 4 dwg
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Authors
Dates
2021-09-21—Published
2020-11-06—Filed