The invention provides an airplane auxiliary balancing system and an airplane. The system comprises a central oil tank, a left wing oil tank, a right wing oil tank and a first oil pump; the central oil tank is arranged in the middle of wings, the left wing oil tank and the right wing oil tank are arranged on a left wing and a right wing of the airplane respectively, and the central oil tank is communicated with the left wing oil tank and the right wing oil tank through oil way pipelines respectively; the outlets of the central oil tank, the left wing oil tank and the right wing oil tank are each provided with a valve correspondingly, and the first oil pump is arranged between the central oil tank and a corresponding valve; and the central oil tank, the left wing oil tank and the right wing oil tank are each provided with an oil quantity sensor. The current gravity center and the optimal gravity center of the airplane are judged according to the collected oil quantity information, the valve and the first oil pump are controlled according to the gravity center and the optimal gravity center to adjust the position and weight distribution of fuel oil, balancing can be carried out in real time, the balancing precision is high, stable flight of the airplane is facilitated, and the accident rate is reduced.
本发明提供一种飞机辅助配平系统及飞机,其中,系统包括:中央油箱、左翼油箱、右翼油箱和第一油泵;所述中央油箱设置在机翼的中部,所述左翼油箱和所述右翼油箱分别设置在飞机的左翼和右翼,所述中央油箱通过油路管道分别与所述左翼油箱和所述右翼油箱连通;所述中央油箱、左翼油箱和右翼油箱的出口处均对应设置有阀门,所述第一油泵设置在所述中央油箱与其对应的阀门之间;所述中央油箱、左翼油箱和右翼油箱上均设置有油量传感器;根据采集的油量信息判断飞机目前的重心和最佳重心,根据所述重心和最佳重心控制阀门和所述第一油泵以调整燃油的位置和重量分布,能实时进行配平,且配平精度高,有利于飞机稳定飞行,降低事故发生率。
Aircraft auxiliary balancing system and airplane
一种飞机辅助配平系统及飞机
2021-06-11
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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