跨介质无人机载具及无人机发射方法

By installing deployable fins and attitude control modules on the cross-medium UAV carrier, the problems of single attitude and insufficient stability of the carrier under harsh sea conditions are solved, and stable ejection of UAVs at different takeoff attitude angles is achieved, thus improving the carrier's adaptability to the marine environment.

CN118770616BActive Publication Date: 2026-07-17CHINA SHIP SCIENTIFIC RESEARCH CENTER

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
CHINA SHIP SCIENTIFIC RESEARCH CENTER
Filing Date
2024-07-26
Publication Date
2026-07-17

AI Technical Summary

Technical Problem

Existing cross-medium UAV carriers are unable to meet the takeoff requirements of UAVs at different takeoff attitude angles under harsh sea conditions, and are easily swayed by ocean wave forces, which limits their applicability to the marine environment.

Method used

Design a cross-medium unmanned aerial vehicle (UAV) carrier, comprising a pressure-resistant tube, fins, and actuators. The carrier's attitude is adjusted by the deployment and retraction of the fins, and the fin angle is adjusted in real time by an attitude control module to achieve stable ejection of the UAV at the takeoff attitude angle.

Benefits of technology

It improves the stability and adaptability of the vehicle in harsh sea conditions, meets the takeoff attitude requirements of different types of UAVs, and enhances its adaptability and stability in harsh sea conditions.

✦ Generated by Eureka AI based on patent content.

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Abstract

本发明涉及一种跨介质无人机载具及无人机发射方法,包括两端贯通的耐压管体和弹射装置,耐压管体用于容纳无人机,耐压管体的一端密封安装有头罩,耐压管体的另一端密封安装有尾舱,耐压管体的外部设置有翅片和作动器,尾舱内安装有控制装置;翅片的一端与耐压管体的外部铰接,翅片与作动器的输出端连接,作动器用于驱动翅片摆动,进而改变翅片的轴线与耐压管体的轴线之间的夹角;当夹角为零时,翅片、耐压管体、头罩和尾舱整体呈流线旋成体;当夹角为预设角度且载具浮于水面时,耐压管体的轴线与水平面的夹角为无人机的起飞姿态角,从而实现载具姿态的调整,使无人机能够在姿态角下起飞,提高载具在恶劣海况下的适应性。
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