Unmanned aerial vehicle with retractable comprehensive protection device

Abstract

The invention discloses an unmanned aerial vehicle with a retractable comprehensive protection device. The unmanned aerial vehicle structurally comprises an anti-shake system, a holder, a camera, a fuselage, four driving motors, retractable protective casings, four sets of wings and ground brackets. The holder is arranged on the lower surface of the fuselage and is connected with the lower surfaceof the fuselage in a riveting mode by bolts, and the upper portion of the camera is embedded in the inner lower portion of the holder. The anti-shake system is arranged in the holder and the lower portion of the anti-shake system is connected with the camera. The four driving motors are separately installed at four corners of the fuselage, and the retractable protective casings are arranged at the periphery of the upper portion of the fuselage and connected with the periphery of the upper portion of the fuselage by fastening. The wings are separately and electrically connected with the driving motors. Through the arrangement of the anti-shake system, the unmanned aerial vehicle does not interfere with the shooting of the camera when swings left and right during flight, and at the same time, the camera is always in a horizontal state, so that the shooting quality is improved; and meanwhile, a pushing mechanism is used for strengthening the firmness of internal parts and reducing the probability of parts falling off.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicles, more precisely, it is an unmanned aerial vehicle with a retractable full protection device. 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 equipment such as autopilot and program control device are installed. 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. When recovering, it can automatically land in the same way as the common aircraft landing process, and can also be recovered by remote ...

AI Technical Summary

Problems solved by technology

[0005] In view of the deficiencies in the prior art, the object of the present invention is to provide a UAV with a retractable comprehensive protection device, so as to solve the problem that the UAV in the prior art cannot ensure that the pan / tilt is in a left-right balance state during the flight shooting process. The shooting effect is extremely poor, because the drone swings from side to side when flying, it will cause the internal parts of the gimbal to vibrate, and then some parts will fall off.

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