Locking quick-release assembly and unmanned aerial vehicle

By designing lock quick disassembly components and using structures such as fixtures and accommodation grooves, the problem of the drone arm and propeller unfolding or rotating by themselves during the handling process is solved, achieving more efficient and stable drone handling.

CN223031302UActive Publication Date: 2025-06-27WUHAN HUACE INNOVATION TECHNOLOGY CO LTD +1
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Patent Information

Application Number
CN202422340673.3
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-09-24
Publication Date
2025-06-27
Estimated Expiration
2034-09-24

AI Technical Summary

Technical Problem

During the handling process of the drone, the arm and the folded propeller are prone to unfold or rotate by themselves, causing trouble for the operator.

Method used

A locking quick-release assembly is designed, including a fixing member, the fixing member includes a first fixing portion and a second fixing portion fixedly connected to the first fixing portion, fixing the machine arm to the base through a first accommodation slot and a snap, and preventing the propeller from rotating and deploying through the second accommodation slot.

Benefits of technology

It significantly improves the convenience and efficiency of the drone body handling, ensures the stability and safety of the arm and propeller during the handling process, and optimizes the convenience of installation and disassembly.

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Abstract

The utility model provides a locking quick-release assembly and an unmanned aerial vehicle, and relates to the technical field of unmanned aerial vehicles. The locking quick-release assembly comprises a fixing piece, the fixing piece comprises a first fixing part and a second fixing part fixedly connected with the first fixing part, a first containing groove is formed in the side face of the first fixing part, and a second containing groove communicated with the first containing groove is formed in the side face of the second fixing part; the inner wall of the first containing groove is used for wrapping the side face of the base, a buckle is arranged on a groove opening of the first containing groove and used for being connected with the side face of the base in a clamped mode so that the first fixing part can be fixed to the base, and the inner wall of the second containing groove is used for wrapping the side face of the folded propeller so that the propeller can be prevented from rotating and unfolding. The locking quick-release assembly can lock the arms of the unmanned aerial vehicle body and the folded propellers at the same time, so that the carrying convenience and efficiency of the unmanned aerial vehicle body are remarkably improved. While the stability and the safety are ensured, the convenience of mounting and dismounting is also obviously optimized, and the manufacturing cost is reduced.
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