Butting and damping device for unmanned aerial vehicle

A shock absorbing device and a technology for unmanned aerial vehicles, which are applied in the field of unmanned aerial vehicles, can solve the problems of high maintenance cost of shooting parts of unmanned aerial vehicles, inability to eliminate adverse effects, and difficulty in rescuing trapped persons in high-rise residential buildings.

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

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Problems solved by technology

[0005] The technical problem to be solved by the present invention is that the

Method used

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  • Butting and damping device for unmanned aerial vehicle
  • Butting and damping device for unmanned aerial vehicle
  • Butting and damping device for unmanned aerial vehicle

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Embodiment Construction

[0029]The present invention provides a docking damping device for an unmanned aerial vehicle. The body of the docking part is fixedly connected to the first joint surface, the second joint surface of the docking part is fixedly connected to the body, and the second joint surface is provided on the second joint surface. A clamping seat and a second clamping seat, the main body is located between the first connecting surface and the second connecting surface, and the distribution of the first clamping seat and the second clamping seat is symmetrical with respect to the center of the second connecting surface , the first engaging surface and the second engaging surface are distributed symmetrically with respect 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 docking part need to be...

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Abstract

The invention discloses a butting and damping device for an unmanned aerial vehicle, and belongs to the technical field of unmanned aerial vehicles. The butting and damping device 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 dampingcomponent comprises first limiting rod, a second limiting rod, a first elastic assembly and a second elastic assembly. The first limiting rod is provided with a first fastening end and a second fastening end; the second limiting rod is provided with a third fastening end and a fourth fastening end; the first elastic assembly is arranged on the exterior of first limiting rod in a sleeving mode; and the second elastic assembly is arranged on the exterior of the second limiting rod in a sleeving mode. The butting and damping device for the unmanned aerial vehicle achieves the technical effects that maintenance cost of a shooting component of the unmanned aerial vehicle is reduced, eliminating the negative influence of recoil on the unmanned aerial vehicle is facilitated, so that the unmannedaerial vehicle can help stranded personnel to escape in time.

Description

technical field [0001] The invention belongs to the technical field of drones, and in particular relates to a docking damping device for drones. 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 one-piece structure. The drone is mainly...

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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