Unmanned aerial vehicle body

Abstract

The invention relates to an unmanned aerial vehicle body, which belongs to the technical field of unmanned aerial vehicles. The unmanned aerial vehicle body comprises a cockpit, central supporting arms, cantilevers, landing frames, a buoys, rotor wings and an anti-collision ring, wherein the central supporting arms are mounted on the circumference of the cockpit; the central supporting arms are cross-shaped hollow structures; the cantilevers are Y-shaped hollow structures; one ends of the cantilevers are inserted into the central supporting arms and connected with the cockpit through the central supporting arms; the other two ends of the cantilevers are connected with the inner circumference of the anti-collision ring through anti-collision supporting arms; the upper ends of the landing frames are connected with the central supporting arms; the lower ends of the landing frames are fixed together with the buoys; and rotor wings driven by a motor is arranged on the cantilevers. The invention is applied to the manufacturing of unmanned aerial vehicle bodies and has the advantages of light mass, high strenght, amphibious property and the like.

Description

technical field [0001] The invention relates to a drone body and a manufacturing method thereof, belonging to the technical field of drone facilities. Background technique [0002] At present, drones are developing rapidly, resulting in multi-style and multi-purpose drones. The body of conventional drones is mostly made of metal materials such as steel and aluminum alloy, which has a large take-off weight and insufficient endurance; at the same time, the landing gear of conventional drones is mostly bracket type, skid type, etc. Landing gear is only suitable for landing on land or flat ground, with limited functions and narrow application fields; and during flight, the space environment is relatively complex, and the blades are easily damaged by impacts from solid garbage, birds and other unknown objects. Leaf damage will directly affect the flight effect of the entire UAV, which is not conducive to the normal operation of its work. [0003] Based on this, this application...

AI Technical Summary

Problems solved by technology

The body of conventional drones is mostly made of metal materials such as steel and aluminum alloy, which has a large take-off weight and insufficient endurance; at the same time, the landing gear of conventional drones is mostly bracket type, skid type, etc. Landing gear is only suitable for landing on land or flat ground, with limited functions and narrow application fields; and during flight, the space environment is relatively complex, and the blades are easily damaged by impacts from solid garbage, birds and other unknown objects. Leaf damage will directly affect the flight effect of the entire UAV, which is not conducive to the normal operation of its work.

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