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Unmanned aerial vehicle

A technology of drones and steering gears, applied in the field of drones, can solve the problems of unfavorable quadrotor drones flying, long lateral width, etc.

Active Publication Date: 2019-07-09
黄迅
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The quadrotor UAV realizes the flight of the UAV through the rotor power components on both sides. However, the rotor power components on both sides make the lateral width of the rotor UAV long, which is not conducive to the flight of the quadrotor UAV in narrow areas.

Method used

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Embodiment Construction

[0025] This part will describe the specific embodiment of the present invention in detail, and the preferred embodiment of the present invention is shown in the accompanying drawings. Each technical feature and overall technical solution of the invention, but it should not be understood as a limitation on the protection scope of the present invention.

[0026] In the description of the present invention, it should be understood that the orientation descriptions, such as up, down, front, back, left, right, etc. indicated orientations or positional relationships are based on the orientations or positional relationships shown in the drawings, and are only In order to facilitate the description of the present invention and simplify the description, it does not indicate or imply that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus should not be construed as limiting the present invention.

[0027] I...

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Abstract

The invention discloses an unmanned aerial vehicle. The unmanned aerial vehicle comprises a main rack, an upper driving mechanism, a lower driving mechanism and an angle adjusting mechanism, wherein the upper driving mechanism is arranged on the upper portion of the main rack and is provided with a first propeller; the lower driving mechanism is arranged on the lower portion of the main rack and is provided with a second propeller, and the second propeller and the first propeller are of a forward and reverse paddle structure; the angle adjusting mechanism is arranged in the main rack and movably connected with the lower driving mechanism, and the axial angle of the lower driving mechanism is adjusted so as to change the air blowing direction of the second propeller. The unmanned aerial vehicle has the advantages that hovering, steering and forward acceleration flying can be realized, and the flying action is flexible; the horizontal width of the unmanned aerial vehicle is small, and the unmanned aerial vehicle can fly in a narrow area.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle. Background technique [0002] UAV is an unmanned aircraft controlled by radio remote control equipment or self-contained program control device. UAVs are widely used in both military and civilian applications. UAVs play an important role in different fields such as aerial photography, power inspection, express transportation and disaster relief. The quadrotor UAV realizes the flight of the UAV through the rotor power components on both sides, but the rotor power components on both sides make the lateral width of the rotor UAV long, which is not conducive to the flight of the quadrotor UAV in a narrow area. Contents of the invention [0003] The purpose of the present invention is to at least solve one of the technical problems in the prior art, and provide an unmanned aerial vehicle with a small lateral width, which can fly in a na...

Claims

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Application Information

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IPC IPC(8): B64C27/08B64C27/12B64C9/00B64C1/06
CPCB64C27/08B64C27/12B64C9/00B64C1/061
Inventor 黄迅
Owner 黄迅