The invention belongs to the technical field of aerial refueling of aircrafts, and particularly relates to a self-rotating wing ring type aerial refueling active stability augmentation taper sleeve. According to the technical scheme, the self-rotor ring type air refueling active stability augmentation taper sleeve comprises a taper inner ring, at least two self-rotor rings are rotationally connected to the taper inner ring, a flight control system, a positioning system and a radio high-speed data transmission system are further installed on the taper inner ring, a plurality of servo motors are installed on the taper inner ring, and the servo motors are connected with the self-rotor rings. A driving assembly is connected between the output end of the servo motor and the spin wing ring; the positioning system and the radio high-speed data transmission system are both electrically connected with the flight control system, and the flight control system is electrically connected with the servo motor. According to the self-rotating wing ring type air refueling active stability augmentation taper sleeve provided by the invention, the taper sleeve butt joint efficiency, precision and safety are improved and accidents are reduced by inhibiting the phenomena of drifting and'head wave 'of a hose taper sleeve system in the air refueling butt joint process.

    本发明属于飞行器空中加油技术领域,特别涉及一种自旋翼环式空中加油主动增稳锥套。其技术方案为:一种自旋翼环式空中加油主动增稳锥套,包括锥体内环,锥体内环上转动连接有至少两个自旋翼环,锥体内环上还分别安装有飞行控制系统、定位系统、无线电高速数据传输系统,锥体内环上安装有若干伺服电机,伺服电机的输出端与自旋翼环之间连接有驱动组件;所述定位系统和无线电高速数据传输系统均与飞行控制系统电连接,飞行控制系统与伺服电机电连接。本发明提供了一种自旋翼环式空中加油主动增稳锥套,通过抑制空中加油对接过程中软管锥套系统出现的飘摆和“头波”现象,提高锥套对接的效率、精度和安全性,减少意外事故的发生。


    Access

    Download


    Export, share and cite



    Title :

    Self-rotating wing ring type air refueling active stability augmentation taper sleeve


    Additional title:

    一种自旋翼环式空中加油主动增稳锥套


    Contributors:
    HUANG JIANGTAO (author) / SHAN ENGUANG (author) / ZHU ZHE (author) / DU XIN (author) / WANG YINZHU (author) / HU BIN (author) / ZHANG SHENG (author) / WANG CHUNYANG (author) / CHEN QISHENG (author) / ZHENG HAOYU (author)

    Publication date :

    2024-10-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Aerial refueling taper sleeve stability augmentation ring

    SHAN ENGUANG / HUANG JIANGTAO / LEI PENGXUAN et al. | European Patent Office | 2022

    Free access

    Device and method for suppressing swinging of self-rotating wing ring type active stability augmentation air refueling taper sleeve

    ZHU ZHE / HUANG JIANGTAO / SHAN ENGUANG et al. | European Patent Office | 2024

    Free access

    Spinning type active stability augmentation air refueling taper sleeve

    HUANG JIANGTAO / SHAN ENGUANG / ZHU ZHE et al. | European Patent Office | 2024

    Free access

    Inflatable air refueling active stability augmentation taper sleeve

    SHAN ENGUANG / HUANG JIANGTAO / HU BIN et al. | European Patent Office | 2024

    Free access

    Grid rudder type air refueling active stability augmentation taper sleeve

    HU BIN / HUANG JIANGTAO / SHAN ENGUANG et al. | European Patent Office | 2024

    Free access