The invention belongs to the technical field of air refueling, and particularly relates to an air refueling stability augmentation taper sleeve based on active jet flow control. According to the technical scheme, the aerial refueling stability augmentation taper sleeve based on active jet flow control comprises an oil conveying pipeline, a taper cup is connected to one end of the oil conveying pipeline, a plurality of gas conveying pipelines are arranged on the oil conveying pipeline, a plurality of jet flow openings are formed in the outer wall of the taper cup, and the gas conveying pipelines communicate with the jet flow openings in a one-to-one correspondence mode; a flight control system, a positioning system and a radio high-speed data transmission system are mounted in the conical cup; the jet system and the air supply device are arranged in the oiling machine, the jet system is electrically connected with the air supply device, 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 jet system. The invention provides an aerial refueling stability augmentation taper sleeve based on active jet flow control, so that the posture of the taper sleeve is actively controlled through jet flow, and the butt joint efficiency and precision of the taper sleeve are improved.
本发明属于空中加油技术领域,特别涉及一种基于主动射流控制空中加油增稳锥套。其技术方案为:一种基于主动射流控制空中加油增稳锥套,包括输油管道,输油管道的一端连接有锥杯,输油管道上设置有若干输气管道,锥杯的外壁上设置有若干射流口,输气管道与射流口一一对应连通,锥杯内安装有飞行控制系统、定位系统和无线电高速数据传输系统;还包括设置于加油机内的射流系统和供气装置,射流系统与供气装置电连接,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,飞行控制系统与射流系统电连接。本发明提供了一种基于主动射流控制空中加油增稳锥套,以实现通过射流主动控制锥套的姿态,提高锥套对接的效率和精度。
Aerial refueling stability augmentation taper sleeve based on active jet flow control
一种基于主动射流控制空中加油增稳锥套
2024-11-08
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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