The invention belongs to the technical field of air refueling, and particularly relates to a grid rudder type air refueling active stability augmentation taper sleeve. According to the technical scheme, the grid rudder type air refueling active stability augmentation taper sleeve comprises a taper cup, a plurality of sets of steering engines are installed on the taper cup, and the output ends of the steering engines are connected with curved-surface-shaped grid rudders; the attitude of the taper sleeve is actively controlled by controlling the deflection angles of the multiple sets of curved-surface-shaped grid rudders. By actively controlling the curved grid rudders in all the directions to deflect by different angles, lift force is generated in all the directions to form differential power to actively control the posture of the taper sleeve, so that the floating phenomenon and the'head wave 'influence of a hose taper sleeve system in the air refueling butt joint process are restrained, the butt joint efficiency, precision and safety of the taper sleeve are improved, and the service life of the taper sleeve is prolonged. And accidents are reduced.
本发明属于空中加油技术领域,特别涉及一种栅格舵式空中加油主动增稳锥套。其技术方案为:一种栅格舵式空中加油主动增稳锥套,包括锥杯,锥杯上安装有若干组转向舵机,转向舵机的输出端连接有曲面形栅格舵;通过控制若干组曲面形栅格舵的偏转角度主动控制锥套姿态。本发明通过主动控制各方向上的曲面形栅格舵偏转不同的角度,在各方向上产生升力形成差动力来实现主动控制锥套的姿态,从而抑制空中加油对接过程中软管锥套系统出现的飘摆现象和“头波”影响,提高锥套对接的效率、精度和安全性,减少意外事故的发生。
Grid rudder type air refueling active stability augmentation taper sleeve
一种栅格舵式空中加油主动增稳锥套
2024-12-10
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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