Aerial photography folding wing unmanned aerial vehicle

A technology of folding wings and drones, applied in the field of drones, can solve the problems of poor stability of aerial cameras, fragile wings, and large storage space, and achieve the effects of improving stability, reducing flight resistance, and realizing shooting angles

Active Publication Date: 2016-06-01
郭兴仁
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The technical problem to be solved by the present invention is to provide an aerial photography folding-wing unmanned aerial vehicle to solve the technical pro

Method used

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  • Aerial photography folding wing unmanned aerial vehicle
  • Aerial photography folding wing unmanned aerial vehicle
  • Aerial photography folding wing unmanned aerial vehicle

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Embodiment Construction

[0021] In order to make the technical problems, technical solutions and advantages to be solved by the present invention clearer, the following will describe in detail with reference to the drawings and specific embodiments.

[0022] Such as figure 1 with figure 2 As shown, the embodiment of the present invention provides an aerial folding-wing unmanned aerial vehicle, comprising a fuselage 1 and a wing, the fuselage 1 is provided with an inner cavity, and the left and right sides of the inner cavity are connected, and the inner cavity The front plate 2 is provided with a first motor 3, which is connected with a screw 4 arranged in the same direction as the fuselage 1, and a gear 5 is meshed symmetrically on both sides of the screw 4. The center of 5 is connected on the fuselage 1 through central axis 6, and the side wall of described gear 5 is connected with rotating plate 7, and the outer end of described rotating plate 7 is vertically connected with support plate 8, and t...

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Abstract

The invention discloses an aerial photography folding wing unmanned aerial vehicle which comprises an airframe and wings. The airframe is provided with an inner cavity; the left side and the right side of the inner cavity are communicated; a first motor is arranged on a front plate of the inner cavity and connected with a lead screw arranged in the same direction as the airframe; gears are symmetrically arranged on the two sides of the lead screw in a meshed mode; the centers of the gears are connected to the airframe through center shafts; rotating plates are connected to the side walls of the gears; supporting plates are perpendicularly connected to the outer ends of the rotating plates; first cylinders are connected to the front ends of the supporting plates; second motors are connected to the front ends of the first cylinders; output shafts of the second motors are connected with first threaded rods; the front plate of the inner cavity is further provided with first nuts screwed to the first threaded rods; the side walls, on the same side as the rotating plates, of the supporting plates are provided with second cylinders. According to the aerial photography folding wing unmanned aerial vehicle, the wings can be folded, storage is convenient, and practicability is achieved.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to an aerial photography folding-wing unmanned aerial vehicle. Background technique [0002] The existing fixed-wing unmanned aerial vehicles, because the wings are fixed, so become one of the most vulnerable parts, and because the wings are fixed, the flight efficiency is not very ideal. [0003] Secondly, since the wings are fixed and cannot be folded, the storage space is too large and it is inconvenient to use. [0004] In addition, due to the poor stability of the aerial camera on the drone, the image quality is not high. Contents of the invention [0005] The technical problem to be solved by the present invention is to provide a drone with folding wings for aerial photography, so as to solve the technical problems of the prior art that the wings of the drone are easily damaged, the storage space is large, and the stability of the drone is poor. [0006] I...

Claims

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Application Information

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IPC IPC(8): B64C3/40B64C3/56
CPCB64C3/40B64C3/56
Inventor 舒丹丹
Owner 郭兴仁
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