The invention provides a dual-redundancy flap automatic control system which comprises a dual-redundancy channel and further comprises a handle control mechanism, a flap control mechanism and a flap control mechanism. The flap control computer is connected with the handle control mechanism; the combination valve is connected with the flap control computer; the flap position output mechanism is connected with the combination valve, and the flap position output mechanism is used for driving a flap transmission line system and a flap to be folded or unfolded; wherein the flap control computer controls the flap position output mechanism based on an instruction position signal generated by the handle control mechanism, meanwhile, the flap control computer collects and processes a real-time flap position signal, and when the real-time flap position signal is consistent with the instruction position signal generated by the handle control mechanism, the flap position output mechanism outputs the flap position signal to the flap control computer. The flap position output mechanism stops working; the invention further provides an automatic control method for the dual-redundancy flap.
本申请提供了一种双余度襟翼自动控制系统,所述控制系统包括双余度通道,所述控制系统包括:手柄操纵机构;襟翼控制计算机,与所述手柄操纵机构连接;组合阀,与所述襟翼控制计算机连接;襟翼位置输出机构,与所述组合阀连接,所述襟翼位置输出机构用于驱动襟翼传动线系及襟翼收上或放下;其中,所述襟翼控制计算机基于所述手柄操纵机构产生的指令位置信号,控制所述襟翼位置输出机构,同时,所述襟翼控制计算机采集和处理实时襟翼位置信号,当所述实时襟翼位置信号与所述手柄操纵机构产生的指令位置信号一致时,所述襟翼位置输出机构停止工作;本申请还提供了一种双余度襟翼自动控制方法。
Dual-redundancy flap automatic control system and method
一种双余度襟翼自动控制系统和方法
2024-04-09
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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