The invention belongs to the technical field of air refueling, and particularly relates to an active control hose air refueling system and an airplane with the same. The active control hose aerial refueling system comprises a refueling hose, a refueling connector, a drag parachute, an electric steering engine and a binocular vision sensor. The refueling joint is mounted at one end of the refueling hose; the drag parachute and the refueling connector are coaxially arranged and fixedly connected. The refueling hose is coaxially sleeved with an electric steering engine, the electric steering engine is close to the drag parachute, and a pneumatic rudder is installed on the electric steering engine; the binocular vision sensor is fixedly installed in the drag parachute, and the binocular vision sensor is used for feeding back a relative position signal between the drag parachute and the oil receiving probe to the electric steering engine. Through the relative position feedback of the binocular vision sensor, the electric steering engine and the pneumatic rudder are used for actively controlling the refueling hose, the butt joint of the oil receiving probe and the refueling connector is assisted, and the butt joint efficiency and success rate are remarkably improved.
本申请属于空中加油技术领域,特别涉及一种主动控制软管空中加油系统及具有其的飞机。主动控制软管空中加油系统包括:加油软管、加油接头、阻力伞、电动舵机以及双目视觉传感器。加油接头安装在所述加油软管的一端;阻力伞与所述加油接头同轴设置并固定连接;电动舵机同轴套设在所述加油软管上,且靠近所述阻力伞布置,所述电动舵机上安装有气动舵;双目视觉传感器固定安装在所述阻力伞的内部,所述双目视觉传感器用于将所述阻力伞与受油探头之间的相对位置信号反馈给所述电动舵机。本申请可以通过双目视觉传感器的相对位置反馈,利用电动舵机和气动舵对加油软管进行主动控制,辅助开展受油探头与加油接头的对接,显著提升对接效率和成功率。
Active control hose air refueling system and airplane with same
一种主动控制软管空中加油系统及具有其的飞机
2022-07-22
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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