FIELD: transport.
SUBSTANCE: proposed drone comprises fuselage, two outer wings and parachute-landing system including pilot parachute, main parachute, slings and suspension system. Parachute system is arranged inside fuselage. Parachute system slings are laid in common protective jacket while suspension system slings are fastened to wing tips by three-degree-of-freedom hinges and holders. Sections of outer wings may turn relative to axis parallel about wing chord and are furnished with retainers.
EFFECT: reliable and safe landing.
2 cl, 6 dwg
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