一种航空分离对接装置
By designing an aviation separation and docking device, and utilizing the cooperation of limit pins and rotating shafts, a stable connection and flexible separation of the load and the carrier aircraft can be achieved. This solves the problems of stability and energy efficiency of the load and carrier aircraft during the flight of high-altitude UAVs, and improves the safety and stability of flight.
CN118025479BActive Publication Date: 2026-07-17SHENYANG AEROSPACE UNIVERSITY
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- SHENYANG AEROSPACE UNIVERSITY
- Filing Date
- 2024-01-26
- Publication Date
- 2026-07-17
AI Technical Summary
Technical Problem
How can high-altitude drones achieve stable separation and docking of the payload and the carrier aircraft during flight to improve flight stability, safety, and energy efficiency?
Method used
Design an aviation separation and docking device, including a guide head, a connecting seat, a positioning plate, a rotating shaft, and a rotating locking device. Through the cooperation of limit pins and limit grooves, the load and the carrier aircraft are fastened and separated. The rotation of the rotating shaft is used to achieve stable fixation and separation of the load.
Benefits of technology
It achieves stable connection and flexible separation between the payload and the carrier aircraft during flight, improving flight stability and safety, and enhancing energy efficiency.
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Figure CN118025479B_ABST
Abstract
本发明公开了一种航空分离对接装置，包括固定于载荷底部的引导头，引导头的中部设置限位销；连接座固定于载机顶部；定位板固定于连接座顶部并开设有限位槽，限位槽和限位销用以限制引导头旋转；旋转轴与连接座、引导头分别同轴转动连接；操控装置连接在连接座上并驱动旋转轴的底端转动；旋转锁定装置用以锁定或解锁引导头的底端和旋转轴的顶端；旋转轴转动至第一位置，引导头和旋转轴为解锁状态时，引导头沿其轴向下移使限位销插入限位槽；旋转轴转动至第二位置，引导头和旋转轴为锁定状态时，旋转轴限制引导头轴向移动。本发明能保证载荷与载机连接可靠,能快速、平滑地将固定装置旋转，使载荷通过自身的升力实现与载机的分离。
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