无人机用夹持式感应节点投放结构

By using a clamping structure and the cooperation of a limiting block and a clamping arm, the problem of rotation and displacement during the deployment of drone sensing nodes is solved, thereby improving the accuracy of parachute positioning and installation efficiency. This method is suitable for multi-node deployment of small and medium-sized drones.

CN121871772BActive Publication Date: 2026-07-17FLIGHTWIN
View PDF 2 Cites 0 Cited by

Patent Information

Application Number
CN202511888729.1
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2025-12-15
Publication Date
2026-07-17
Estimated Expiration
2045-12-15

AI Technical Summary

Technical Problem

Existing drone sensor node deployment structures are prone to rotation or displacement during flight, resulting in inaccurate parachute deployment positions, low installation efficiency, and inability to adapt to sensor nodes of different sizes and weights.

Method used

The system employs a clamping structure, which, through the cooperation of the limiting block and the clamping arm, utilizes the automatic switching of the return spring and the cam to ensure that the parachute is always located at the top of the node. The mechanical rigidity of the limiting block and the clamping arm also enables rapid installation and stable clamping.

Benefits of technology

It ensures accurate parachute deployment, improves installation efficiency by over 60%, is compatible with sensing nodes of different sizes and weights, is suitable for small and medium-sized drones, is suitable for simultaneous deployment of multiple nodes, and is suitable for manual or remote control operation.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN121871772B_ABST
    Figure CN121871772B_ABST
Patent Text Reader

Abstract

本申请涉及无人机用夹持式感应节点投放结构,包括固定板、第一夹臂、第二夹臂和限位块,第一夹臂设置于固定板的一端,中部与固定板转动连接;第二夹臂设置于固定板的另一端,中部与固定板转动连接,第二夹臂与第一夹臂对称;限位块滑动设置于固定板上,位于第一夹臂与第二夹臂之间,限位块的边缘与第一夹臂、第二夹臂的上端相抵接,限位块能够沿固定板的高度方向移动至第一位置或第二位置;限位块通过移动至第一位置使第一夹臂与第二夹臂呈现释放姿态,通过移动至第二位置使第一夹臂与第二夹臂呈现夹持姿态。通过限位块与夹臂的配合实现机械刚性限位,避免感应节点在飞行振动或气流扰动下发生转动或位移,确保降落伞开伞时始终位于节点顶部。
Need to check novelty before this filing date? Find Prior Art

Citation Information

Patent Citations

  • Unmanned aerial vehicle transportation and distribution equipment

    CN111252249A

  • Carrying manipulator for medicine decocting pot

    CN116352739A