The invention belongs to the technical field of air refueling, and particularly relates to a self-rotating type active stability augmentation air refueling taper sleeve. According to the technical scheme, the spinning type active stability augmentation air refueling taper sleeve comprises a taper sleeve body, at least two rotating cylinders are rotationally connected to the taper sleeve body, bias momentum rings are connected to the rotating cylinders, and an included angle is formed between the axis of each bias momentum ring and the axis of the taper sleeve body; a flight control system, an attitude sensor and a radio high-speed data transmission system are further installed on the taper sleeve body, a plurality of motors are installed on the taper sleeve body, and driving assemblies are connected between the output ends of the motors and the rotating cylinder; the attitude sensor 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 motor. According to the self-rotating type active stability augmentation air refueling taper sleeve, the taper sleeve butt joint efficiency and progress can be improved, and accidents are reduced.
本发明属于空中加油技术领域,特别涉及一种自旋式主动增稳空中加油锥套。其技术方案为:一种自旋式主动增稳空中加油锥套,包括锥套本体,锥套本体上转动连接有至少两个转动筒,转动筒上连接有偏置动量环,偏置动量环的轴线与锥套本体的轴线具有夹角,锥套本体上还分别安装有飞行控制系统、姿态传感器、无线电高速数据传输系统,锥套本体上安装有若干电机,电机的输出端与转动筒之间连接有驱动组件;所述姿态传感器和无线电高速数据传输系统均与飞行控制系统电连接,飞行控制系统与电机电连接。本发明提供了一种自旋式主动增稳空中加油锥套,可提高锥套对接的效率和进度,减少意外事故的发生。
Spinning type active stability augmentation air refueling taper sleeve
一种自旋式主动增稳空中加油锥套
25.10.2024
Patent
Elektronische Ressource
Chinesisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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