Foldable unmanned aerial vehicle

Abstract

The invention provides a foldable unmanned aerial vehicle comprising a fuselage and an information acquisition device, wherein the information acquisition device is installed on the fuselage; the unmanned aerial vehicle further comprises a first connecting piece, a second connecting piece, at least two rotor shafts, and at least three undercarriages, wherein the rotor shafts are movably connected with the fuselage through the first connecting piece; the at least three undercarriages are movably connected with the fuselage through the second connecting piece. When the unmanned aerial vehicle performs no flight work, the rotor shafts and the undercarriages can be located at a retractive state relative to the fuselage, so as to facilitate carrying by a worker during field operation, meanwhile when the unmanned aerial vehicle needs to perform flight work, the undercarriages can be in the retractive state relative to the fuselage, so that the acquisition device can fly for 360 degrees without being shielded to achieve acquisition work.

Description

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AI Technical Summary

Problems solved by technology

[0004] 1. The landing gear and the rotor shaft are in an open state relative to the UAV body, which makes the overall volume of the UAV large and takes up storage space;

[0005] 2. During the flight operation of the UAV, the landing gear is always in an open state relative to the UAV. However, this state makes the camera in the info

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