FIELD: aviation.
SUBSTANCE: invention is related in particular to designs of multi-rotor unmanned aerial vehicles (UAVs). The multicopter contains load-bearing beams-brackets having a tubular cross-section and mounted on the central part of the body. At their outer ends there are mounting tips that carry electric motors with propellers, and a vertical landing gear post is attached to the bottom of each tip. The body is made as a three-part body, including the central part of the body, as well as removable upper and lower caps. The upper cap is equipped with a cargo bracket located and oriented along the angle between the supporting beams-brackets. The central part of the body is equipped with internal partitions with the possibility of placing components of the electronic flight control unit in cells formed by the internal partitions and the outer wall of the central part of the body.
EFFECT: possibility of using UAV units as the basic aviation platform of a family of multicopters, the production of which can be mastered in the shortest possible time.
8 cl, 4 dwg
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Authors
Dates
2024-02-02—Published
2023-09-26—Filed