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

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, in particular to a foldable unmanned aerial vehicle. Background technique [0002] Unmanned aircraft, referred to as "UAV", is an unmanned aircraft controlled by radio remote control equipment and its own program control device. There is no cockpit on board, but it is equipped with autopilot, program control device, information collection device and other equipment. The personnel on the ground, on the ship, or at the remote control station of the parent aircraft track, locate, remotely control, telemeter and digitally transmit it through radar and other equipment. Under the radio control, it can take off like an ordinary aircraft or be launched into the air with a booster rocket, and it can also be taken into the air by the parent aircraft for flight. [0003] The UAV includes a fuselage, an information collection device (cloud platform control system), a rotor shaft, and a rot...

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 information collection device rotate 360° during the collection operation. In the same direction, the landing gear will often block part of the image and video information, which will cause the phenomenon of "missing" in the information collection device, making the information collected by the information collection device incomplete

Images