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.
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
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.
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.
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.