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Downwards foldable-type multi-rotor wing unmanned aerial vehicle

A multi-rotor unmanned and unmanned aerial vehicle technology, applied in aircraft, rotorcraft, aircraft parts, etc., can solve the problems of large size, inconvenient carrying and storage of aircraft, and achieve the effect of reducing the volume

Inactive Publication Date: 2015-10-28
代一泓
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The rotors of existing multi-rotor unmanned aerial vehicles are supported by support arms, and the volume of the entire aircraft becomes very large, which causes great inconvenience to carrying and storage

Method used

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  • Downwards foldable-type multi-rotor wing unmanned aerial vehicle
  • Downwards foldable-type multi-rotor wing unmanned aerial vehicle
  • Downwards foldable-type multi-rotor wing unmanned aerial vehicle

Examples

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Embodiment Construction

[0040] The specific embodiments of the present invention will be further described below in conjunction with the accompanying drawings.

[0041] Embodiments of the present invention are described in detail below, examples of which are shown in the drawings, wherein the same or similar reference numerals designate the same or similar elements or elements having the same or similar functions throughout. The accompanying drawings are used to help understand various embodiments of the present invention, and the scales of the figures in the accompanying drawings may be different. The embodiments described below by referring to the figures are exemplary only for explaining the present invention and should not be construed as limiting the present invention. On the contrary, the embodiments of the present invention include all changes, modifications and equivalents coming within the spirit and scope of the appended claims. In the description of the present invention, it should be und...

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PUM

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Abstract

The invention discloses a downwards foldable-type multi-rotor wing unmanned aerial vehicle (1000) which comprises a power device (200), a camera shooting device (300), a cell system (400), a control circuit (600), a plurality of support arms (110), a central mounting seat (120) and a locking component (150), wherein the power device (200), the camera shooting device (300) and the cell system (400) are connected with the control circuit (600) separately; the support arms (110) are rotationally connected onto the central mounting seat (120); the locking component (150) is used for locking all the support arms (110) on the central mounting seat (120) simultaneously when the support arms (110) are unfolded. As the support arms are rotationally connected onto the central mounting seat and can be folded downwards, the size of the unmanned aerial vehicle is reduced to the great extent.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to a fold-down multi-rotor unmanned aerial vehicle. Background technique [0002] Unmanned aerial vehicles have unique flight capabilities and are small in size. They have broad prospects in aerial photography, atmospheric detection, traffic monitoring, resource exploration, power inspection, forest fire prevention, agriculture, and military use. Existing multi-rotor UAVs usually obtain lift by rotating the blades with motors. The rotors of existing multi-rotor unmanned aerial vehicles are supported by support arms, and the volume of the entire aircraft becomes very large, which causes great inconvenience to carrying and storage. Contents of the invention [0003] The purpose of the present invention is to provide a fold-down multi-rotor unmanned aerial vehicle, which can minimize the volume of the aircraft through folding. [0004] The present inven...

Claims

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Application Information

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IPC IPC(8): B64C1/06B64C27/08B64C25/10B64D47/08
Inventor 张子林袁博
Owner 代一泓
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