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.
Foldable unmanned aerial vehicle
2015-05-06
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |