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Multifunctional unmanned aerial vehicle

A UAV, multi-functional technology, applied in the direction of airframe, vehicle energy storage, aircraft control, etc., can solve problems such as interference and inaccurate positioning

Pending Publication Date: 2020-10-27
广东北研航空遥感科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In order to solve the problem in the prior art that the camera and other video components and object-carrying components of the UAV are likely to interfere with each other, resulting in inaccurate positioning, the present invention provides a multifunctional UAV

Method used

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Embodiment Construction

[0032] 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. 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.

[0033] see Figure 1-Figure 4 As shown, according to the embodiment of the present invention, the multifunctional UAV includes a nose assembly 1 and a battery quick loading and unloading structure 2, and the battery quick loading and unloading structure 2 is fixedly arranged on the bottom of the nose assembly 1, and also includes a pan platfo...

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Abstract

The embodiment of the invention provides a multifunctional unmanned aerial vehicle. The multifunctional unmanned aerial vehicle comprises a machine head assembly and a quick battery assembling and disassembling structure; the quick battery assembling and disassembling structure is fixedly arranged at the bottom of the machine head assembly; the multifunctional unmanned aerial vehicle further comprises a holder frame assembly and a hook assembly body, the holder frame assembly is fixedly arranged on the side edge of the bottom of the quick battery assembling and disassembling structure, an obliquely-arranged rain shielding cover is arranged at the top of the holder frame assembly, a load frame is fixedly arranged at the bottom of the quick battery assembling and disassembling structure, andthe hook assembly body is fixedly arranged on the load frame. The hook assembly body is arranged at the bottom of the unmanned aerial vehicle body through the load frame, vibration generated in the flying process or the sampling process can only act on the load frame and cannot be transmitted to the holder frame assembly through the unmanned aerial vehicle body, and then the problem that due to the fact that the view field of a camera on the holder frame assembly is limited, positioning of the unmanned aerial vehicle is inaccurate is solved.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to a multifunctional unmanned aerial vehicle. Background technique [0002] Unmanned aircraft, referred to as "UAV", is an unmanned aircraft that is controlled by radio remote control equipment and its own program control device. UAV is actually a general term for unmanned aerial vehicles. It has the advantages of small size, low cost, convenient use, low requirements for combat environment, and strong battlefield survivability. [0003] The UAV is equipped with video components such as cameras and a loading component, wherein the video components such as cameras are used for shooting and collecting images, and the loading components are used for transporting loads to be moved. In the prior art, the video components such as cameras and the object-carrying components are all arranged on the same bracket at the bottom of the UAV fuselage. question. Contents of the...

Claims

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Application Information

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IPC IPC(8): B64D47/08B64D27/24B64C1/30B64D1/00B60L53/80
CPCB64C1/30B64D1/00B64D27/24B64D47/08B60L53/80Y02T10/70Y02T10/7072Y02T90/16
Inventor 张宝华黄开生
Owner 广东北研航空遥感科技有限公司
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