Butting and load-bearing device for unmanned aerial vehicle

A technology of a load-bearing device and an unmanned aerial vehicle, applied in the field of unmanned aerial vehicles, can solve the problems of high maintenance cost of the shooting parts of the unmanned aerial vehicle, damage to the unmanned aerial vehicle, and interference with the flying attitude of the unmanned aerial vehicle.

Inactive Publication Date: 2018-12-07
EWATT TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The technical problem to be solved by the present invention is that the maintenance cost of the shooting parts of the UAV is high; when the glass doors and windows are shot, the recoi

Method used

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  • Butting and load-bearing device for unmanned aerial vehicle
  • Butting and load-bearing device for unmanned aerial vehicle
  • Butting and load-bearing device for unmanned aerial vehicle

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Embodiment Construction

[0026] The invention discloses that the invention provides a docking load-bearing device for an unmanned aerial vehicle. By fixedly connecting the body of the docking component with the first joint surface, the second joint surface of the docking component is fixedly connected with the body, and the first clamping seat and the second clamping seat are arranged on the second joint surface, so that the body is positioned at the first Between the engaging surface and the second engaging surface, the first engaging seat and the second engaging seat are symmetrically distributed relative to the center of the second engaging surface, and the first engaging surface and the second engaging surface are symmetrically distributed relative to the body. Due to the detachable connection between the first connecting surface of the docking part and the fuselage, if the launch part and / or the docking part are damaged, the UAV does not need to be replaced, and only the launch part and / or the doc...

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Abstract

The invention discloses a butting and load-bearing device for an unmanned aerial vehicle, and belongs to the technical field of unmanned aerial vehicles. The butting and load-bearing device comprisesa butting component and a load-bearing component. The butting component comprises a first connecting surface, a body and a second connecting surface. The first connecting surface is detachably connected with a fuselage, the body is fixedly connected with the first connecting surface, the second connecting surface is fixedly connected with the body, and a first clamping and connecting seat and a second clamping and connecting seat are arranged on the second connecting surface. The load-bearing component comprises a first supporting arm and a second supporting arm. The first supporting arm is provided with a first end and a second end, wherein a first mounting hole is formed in the second end; the second supporting arm is provided with a third end and a fourth end, and a second mounting holeis formed in the fourth end; wherein a first limiting rod penetrates through the first mounting hole, and a second limiting rod penetrates through the second mounting hole. The butting and load-bearing device for the unmanned aerial vehicle achieves the technical effects that maintenance cost of a shooting component of the unmanned aerial vehicle is reduced; flight attitudes of the unmanned aerial vehicle are stabilized, and the unmanned aerial vehicle rescuing stranded personnel in high-housings in time is facilitated.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to a docking load-bearing device for unmanned aerial vehicles. Background technique [0002] Unmanned UAV, referred to as "UAV", is an unmanned UAV controlled by radio remote control equipment and its own program control device. There is no cockpit on board, but it is equipped with autopilot, program control device, information collection device and other equipment. The personnel on the ground, on the ship, or at the remote control station of the parent aircraft track, locate, remotely control, telemeter and digitally transmit it through radar and other equipment. It can take off like an ordinary UAV under radio remote control or be launched into the air with a booster rocket, or it can be brought into the air by the parent aircraft for flight. [0003] For the unmanned aerial vehicle, the unmanned aerial vehicle fuselage in the prior art is made of a ...

Claims

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Application Information

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IPC IPC(8): B64D1/02B64D47/00
CPCB64D1/02B64D47/00B64U2101/00
Inventor 不公告发明人
Owner EWATT TECH CO LTD
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