Foldable wings of unmanned aerial vehicle

A drone and wing technology, applied in wing adjustment, unmanned aerial vehicles, motor vehicles, etc., can solve problems such as inconvenience, inability to fold and operate, damage, etc., to avoid losses, structural science, use handy effect

Inactive Publication Date: 2016-12-21
四川精诚至强科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In terms of military use, drones are divided into reconnaissance aircraft and target drones. In civilian use, drones + industrial applications are the real needs of drones. However, the wings of current drones are fixed and cannot be folded. It is not very convenient to operate the drone when it is being transported, and it may be damaged if you are not careful.

Method used

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  • Foldable wings of unmanned aerial vehicle
  • Foldable wings of unmanned aerial vehicle
  • Foldable wings of unmanned aerial vehicle

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Embodiment Construction

[0014] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0015] see Figure 1-3 , an embodiment provided by the present invention: a foldable wing of an unmanned aerial vehicle, including a wing fixing device 1 and a driven gear 2, a mounting shaft 13 is installed on the inner side wall of the wing fixing device 1, and the The shaft 13 is fixed with a rotating mounting part 11, and the inside of the wing fixing device 1 is fixed with a rotating motor body 14 by bolts. The rotating motor body 14 is equipped with a ro...

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Abstract

The invention discloses a foldable wing of an unmanned aerial vehicle. The foldable wing comprises a wing fixing device and a driven gear part. A rotary motor main body is fixed in the wing fixing device through a bolt. A rotary driving motor is installed on the rotary motor main body. A rotary motor driving wheel is fixed to the output end of the rotary motor main body. The driven gear part is installed on the wing fixing device through a rotary gear main body. A main swing body is installed on one side of the wing fixing device. A swing folding motor is installed on a center rotary shaft in the main swing body. An auxiliary swing body is installed on one side of the main swing body. A folding motor shell is installed at the top of the swing folding motor. A folding motor stator winding is installed in the folding motor shell through a fixing device. According to the foldable wing of the unmanned aerial vehicle, the swing bodies of the unmanned aerial vehicle can be folded at two degrees, can be turned over and can be folded rotationally at the same time.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicle mechanical equipment, in particular to a foldable wing of an unmanned aerial vehicle. 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. From a technical point of view, it can be divided into: unmanned fixed-wing aircraft, unmanned vertical take-off and landing aircraft, unmanned Manned airships, unmanned helicopters, unmanned multi-rotor aircraft, unmanned parawing aircraft, etc. UAVs can be divided into military and civilian applications according to their application fields. For military use, drones are divided into reconnaissance aircraft and target drones. For civilian use, drones + industrial applications are the real needs of drones. However, the wings of current drones are fixed and cannot be folded. It is not particularly convenient to operate the dro...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C3/56
CPCB64C3/56B64U10/25
Inventor 刘若愚
Owner 四川精诚至强科技有限公司
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