The invention belongs to the technical field of aircraft front wheel turning systems, and relates to a high-reliability aircraft front wheel turning system which comprises a turning instruction sensor, a turning control valve, a turning control unit, a turning execution mechanism, a turning angle feedback sensor, a brake control unit and a comprehensive management computer. After the turning control unit receives the aircraft wheel speed signal and the ground speed signal at the same time, large and small angle control law switching logic is executed according to the aircraft wheel speed signal; when it is judged that the aircraft wheel speed signal fails, whether the received ground speed signal is effective or not is judged, and if the received ground speed signal is effective, the turning control unit executes large and small angle control law switching logic according to the received ground speed signal; the aircraft wheel speed signal and the ground speed signal are introduced at the same time, when the aircraft wheel speed signal loses efficacy, the ground speed signal can still control the front wheel to make large-angle turning, the situation that when the aircraft wheel speed signal loses efficacy, the front wheel turning system cannot make large-angle turning is prevented, and the task reliability of the aircraft is improved.
本申请属于飞机前轮转弯系统技术领域,为一种高可靠性飞机前轮转弯系统,包括转弯指令传感器、转弯控制阀、转弯控制单元、转弯执行机构、转弯角度反馈传感器、刹车控制单元和综合管理计算机;转弯控制单元在同时接收到飞机轮速信号和地速信号后,根据飞机轮速信号执行大小角度控制律切换逻辑;当判断飞机轮速信号失效后,判断接收到的地速信号是否有效,若有效,则转弯控制单元根据接收到的地速信号执行大小角度控制律切换逻辑;通过同时引用飞机轮速信号和地速信号,在飞机轮速信号失效时,通过采用地速信号仍然能够控制前轮进行大角度的转弯,防止飞机轮速信号失效时,前轮转弯系统不能进行大角度转弯,提高飞机的任务可靠性。
High-reliability aircraft front wheel turning system
一种高可靠性飞机前轮转弯系统
2023-03-28
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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