Quick-release connecting assembly for a compound wing unmanned aerial vehicle

The design of the quick-release connection component solves the transportation difficulties and damage problems caused by the fixed connection between the wings and the fuselage of the compound wing UAV, enabling rapid installation and disassembly, improving transportation efficiency and the service life of the wings.

CN224546330UActive Publication Date: 2026-07-24华启天成(深圳)智能科技有限公司
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
华启天成(深圳)智能科技有限公司
Filing Date
2025-08-29
Publication Date
2026-07-24

AI Technical Summary

Technical Problem

The existing compound-wing drones have wings that are fixedly connected to the fuselage, resulting in a large overall space occupation, difficult transportation, and easy damage to the wings, which increases maintenance costs.

Method used

Design a quick-release connection assembly that utilizes the cooperation of first and second lifting rods, springs, and locking blocks to achieve rapid installation and disassembly of fixed-wing and multi-rotor aircraft. The matching of inserts and slots enables rapid connection and separation between the fuselage and the fixed-wing aircraft.

Benefits of technology

It simplifies the transportation process of drones, reduces the risk of wing damage, extends the service life of the wings, and improves transportation efficiency and equipment lifespan.

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Abstract

The utility model discloses a kind of quick-release connection components for composite wing unmanned aerial vehicle, including fuselage and fixed wing installed on fuselage, both sides of fixed wing are equipped with mounting seat, and detachable multi-rotor mounting frame is installed on mounting seat.The beneficial effects of the utility model are as follows: by setting first spring, first lifting rod and installation pipe cooperation can make first lifting rod and first lifting plate can be lifted along installation pipe, drive the first locking groove on locking block and the locking block on fixed wing are inserted and locked, complete the quick installation of fuselage and fixed wing, second lifting rod is inserted into second locking groove under the action of second spring, complete the locking installation of mounting seat and multi-rotor mounting frame, so as to realize the quick installation and disassembly of multi-rotor on multi-rotor mounting frame, facilitate the disassembly and transportation of unmanned aerial vehicle, avoid wing damage in the process of transportation, knock damage, prolong the service life of unmanned aerial vehicle wing.
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