Unmanned aerial vehicle control system loading platform based on carbon fiber reinforced PA material and unmanned aerial vehicle

By utilizing a drone control system loading platform made of carbon fiber reinforced PA material and employing a linkage design between the lifting mechanism and the winding device, the problems of complex structure and insufficient adaptability of existing drone loading platforms are solved. This enables adaptive clamping of the drone and continuous operation of the sealing cover, thereby improving the automation and reliability of the loading platform.

CN120840916AInactive Publication Date: 2025-10-28DONGGUAN WEILI NEW MATERIALS CO LTD
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Patent Information

Application Number
CN202510997223.8
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2025-07-18
Publication Date
2025-10-28
Estimated Expiration
Not applicable · inactive patent

AI Technical Summary

Technical Problem

Existing drone mounting platforms have complex structures, multiple and independent drive sources, and cannot be adapted to drone brackets of different sizes. They also lack automatic reset functions, resulting in complex mechanical structures, high energy consumption, and discontinuous operation.

Method used

The drone control system loading platform, made of carbon fiber reinforced PA material, uses a linkage design of lifting mechanism, winding device and sealing cover. The lifting platform is driven by telescopic cylinder, the worm gear and worm wheel of the transmission unit mesh to drive the winding wheel to rotate, the elastic rope clamps the drone, and the spiral spring provides an automatic reset function, realizing the adaptive clamping of the drone and continuous operation of the sealing cover.

Benefits of technology

It achieves precise fixing and resetting of drones, simplifies the mechanical structure, reduces energy consumption, improves adaptability to different models and operational continuity, and ensures high reliability and sealing during the loading process.

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Abstract

The invention relates to the technical field of unmanned aerial vehicle loading systems, in particular to an unmanned aerial vehicle control system loading platform based on a carbon fiber reinforced PA material and an unmanned aerial vehicle, the unmanned aerial vehicle control system loading platform comprises a loading box, a lifting mechanism and four winders, and the lifting mechanism drives the unmanned aerial vehicle to ascend and descend in the loading box and drives the winders on the outer sides of the corners of the unmanned aerial vehicle; the top space of the loading box is controlled to open and close. A telescopic cylinder drives a lifting table to ascend and descend, a worm and a worm gear of a transmission part are meshed to drive a winding wheel to rotate, an elastic rope is used for tightening and pulling a clamping plate to move along a guide groove, an unmanned aerial vehicle support is clamped in a self-adaptive mode, accurate fixing and resetting of an unmanned aerial vehicle are synchronously completed through a single driving source, and an extra power device is not needed; the adaptability to different types of unmanned aerial vehicles is remarkably improved, meanwhile, through flexible clamping of the elastic rope and automatic reset of the outer sleeve spring, damage to the vehicle body caused by rigid clamping is avoided, and high reliability in a frequent loading and unloading scene is ensured.
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