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An arm folding assembly and an unmanned aerial vehicle

A technology of folding components and arms, applied to aircraft parts, fuselage, aircraft control, etc., can solve the problems of inconvenient storage and large space occupation of drones

Active Publication Date: 2018-12-07
SHENZHEN XIANGNONG INNOVATION TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The purpose of the present invention is to provide an arm folding assembly and a drone to solve the problem that the drone takes up a lot of space due to inconvenient storage in the prior art

Method used

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  • An arm folding assembly and an unmanned aerial vehicle
  • An arm folding assembly and an unmanned aerial vehicle
  • An arm folding assembly and an unmanned aerial vehicle

Examples

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Embodiment Construction

[0030] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments It is a part of embodiments of the present invention, but not all embodiments. The components of the embodiments of the invention generally described and illustrated in the figures herein may be arranged and designed in a variety of different configurations.

[0031] Accordingly, the following detailed description of the embodiments of the invention provided in the accompanying drawings is not intended to limit the scope of the claimed invention, but merely represents selected embodiments of the invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art wi...

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Abstract

The invention relates to an arm folding assembly and an unmanned aerial vehicle, which relates to the technical field of the unmanned aerial vehicle. The arm folding assembly comprises a connecting member, a fixing sleeve, an arm receiving cylinder and a limit stopper. The connector comprises a connector body, two flanges extend to the same side at one end of the connector body and are arranged inparallel, and a plurality of anti-slip projections are arranged at the other end of the two flanges away from the connector body. The connector body is movably connected to the outer wall surface ofthe fixing sleeve. One end of the arm receiving cylinder is fixedly sleeved in the fixing sleeve. The limiting stopper comprises a bottom plate and two side plates extending upward from two sides of the bottom plate, and the other end of the arm receiving cylinder is movably connected between the two sides plates, one side of the two sides plates facing the arm receiving cylinder is formed with afirst notch, and one side of the two sides plates opposite to the first notch is formed with a second notch. The arm folding assembly solves the problem that the unmanned aerial vehicle occupies largespace and is inconvenient to store in the prior art.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular, to an arm folding assembly and an unmanned aerial vehicle. Background technique [0002] Unmanned aircraft is referred to as "UAV" for short, and the English abbreviation is "UAV". It is a general term for unmanned aerial vehicles. Compared with manned aircraft, it has the advantages of small size, low cost, convenient use, low requirements for combat environment, and strong battlefield survivability. Since unmanned aircraft is of great significance to future air combat, all major military countries in the world are stepping up the development of unmanned aircraft. [0003] The drone usually has an arm structure extending outward from the fuselage, and a propeller is installed on the arm structure for power generation. Due to the relatively large volume of space occupied by the arm after deployment, in order to ensure a certain strength requirement, the arm struc...

Claims

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Application Information

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IPC IPC(8): B64C1/30
CPCB64C1/30
Inventor 朱秋阳梁伟俊胡洁
Owner SHENZHEN XIANGNONG INNOVATION TECH CO LTD
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