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Foldable variable-pitch propeller for fixed-wing unmanned aerial vehicle

A variable-pitch propeller, UAV technology, applied in propellers, aircraft parts, transportation and packaging, etc., can solve problems such as adverse effects on the flight performance of fixed-wing UAVs, and achieve the effect of improving stability and reducing air resistance

Inactive Publication Date: 2021-01-22
GUANGDONG GUOSHIJIAN TECH DEV CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] A foldable variable-pitch propeller for a fixed-wing unmanned aerial vehicle proposed by the present invention solves the problem that the fixed-pitch blade has an adverse effect on the flight performance of a fixed-wing unmanned aerial vehicle

Method used

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  • Foldable variable-pitch propeller for fixed-wing unmanned aerial vehicle
  • Foldable variable-pitch propeller for fixed-wing unmanned aerial vehicle
  • Foldable variable-pitch propeller for fixed-wing unmanned aerial vehicle

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Embodiment Construction

[0021] 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.

[0022] refer to Figure 1-3 , a foldable variable-pitch propeller for a fixed-wing unmanned aerial vehicle, comprising a casing 1, a cavity 2 is opened in the casing 1, and bearings 3 are inlaid on both sides of the casing 1, and the bearings 3 are symmetrically distributed with respect to the shell 1, and the bearings 3 are parallel to each other, and both sides of the shell 1 are matched with paddle clips 4, and the two sets of paddle clips 4 are coaxial, and the two sets of Both ends of the paddle clips 4 that are close to each other pass through the bearing 3 and extend into the cavity 2, and the two ends of the two groups of paddle clips 4 that are far away from...

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Abstract

The invention discloses a foldable variable-pitch propeller for a fixed-wing unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles. The foldable variable-pitch propeller comprises a shell, a cavity is formed in the shell, bearings are embedded in the two sides of the shell, the bearings are symmetrically distributed relative to the shell, and the bearings are parallel to each other; propeller clamps are installed on the two sides of the shell in a matched mode, and the two sets of propeller clamps are coaxial; the two ends, close to each other, of the two setsof propeller clamps penetrate through the bearing and extend into the cavity, and clamping grooves are formed in the two ends, away from each other, of the two sets of propeller clamps in the axial direction; and blades are hinged into the clamping grooves in a matched mode. The foldable variable-pitch propeller is novel in structure and simple and reliable in structure, and the problem that thefixed-pitch blades have adverse effects on the flight performance of the fixed-wing unmanned aerial vehicle is effectively solved.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicle equipment, in particular to a foldable variable-pitch propeller for a fixed-wing unmanned aerial vehicle. Background technique [0002] UAV is an unmanned and autonomous aircraft. The image of UAV in people's impression generally stays on a multi-rotor aircraft. In fact, as long as it has out-of-control autonomous flight, can automatically identify and judge Those who respond should be included in the category of unmanned aerial vehicles, including unmanned multi-rotor aircraft, helicopters, fixed-wing aircraft and even hot air balloons. At present, there has been no major breakthrough in battery technology. Most of the man-machines use fixed-wing aircraft, and use internal combustion engines as driving power, and fixed-wing aircraft have a flight speed and higher survivability that multi-rotor aircraft cannot match. [0003] Most of the current civilian fixed-wing UAVs use fixed-pitch blad...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C11/32
CPCB64C11/32
Inventor 王志成黄嘉盛
Owner GUANGDONG GUOSHIJIAN TECH DEV CO LTD
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