Chemical defense rotor unmanned aerial vehicle mounting mechanism

By quickly fixing the jaws with a motor-driven bidirectional threaded rod and slide plate in the mount mechanism of the chemical-proof rotor UAV, and buffering the landing impact through the hinge block and slide rod assembly, the low loading efficiency and faults in the prior art are solved. Frequent problems have improved the efficiency of use and the life of the drone.

CN222179822UInactive Publication Date: 2024-12-17丁纯伟
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Patent Information

Application Number
CN202421071903.4
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-05-16
Publication Date
2024-12-17
Estimated Expiration
Not applicable · inactive patent

AI Technical Summary

Technical Problem

When replacing different types of hooks, the existing chemical-proof rotor drone mounting mechanism requires the use of tools to rotate multiple sets of bolts to fix it. It is inefficient and may fail to throw the mounted items, which affects the use effect.

Method used

A mounting mechanism including a fixing shell, jaw, buffer assembly and motor is designed to achieve rapid fixing and throwing of jaws by driving the bidirectional threaded rod and slide plate. The hinge block and slide rod assembly are used to reduce the landing impact and improve the Efficiency and practicality of use.

Benefits of technology

It realizes rapid fixing and throwing of jaws, improves working efficiency, reduces the impact force of the drone when landing, and extends the service life of the drone.

✦ Generated by Eureka AI based on patent content.

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    Figure CN222179822U_ABST
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Abstract

The utility model relates to the field of unmanned aerial vehicles, and discloses a chemical defense rotor unmanned aerial vehicle mounting mechanism which comprises an unmanned aerial vehicle body, a dismounting assembly is arranged on the lower surface of the unmanned aerial vehicle body, a buffer assembly is arranged at the right end of the unmanned aerial vehicle body, the dismounting assembly comprises a fixing shell, and the fixing shell is fixedly connected to the lower surface of the unmanned aerial vehicle body. A clamping jaw is in contact with the inner wall of the fixing shell, a first rectangular groove is formed in the right surface of the top end of the clamping jaw, a sliding plate is slidably connected to the rear surface of the fixing shell in a penetrating mode, the buffering assembly comprises a hinge block, and the hinge block is fixedly connected to the outer wall of the right end of the unmanned aerial vehicle body. According to the clamping jaw device, the clamping jaw can be fixed only by inserting the clamping jaw into the inner wall of the fixing shell and then starting the motor, the mode of rotating multiple sets of bolts is not needed, the clamping jaw device is rapid and convenient to use, the working efficiency is improved, meanwhile, when the clamping jaw loses efficacy and cannot throw objects, the clamping jaw can be limited through contact of the motor, the objects can be thrown, and practicability is improved.
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