The invention belongs to the field of aircraft system control, and particularly relates to an aircraft dual-redundancy front wheel turning system control device. Comprising a first signal input unit, a first signal processing unit and a front wheel main channel electromagnetic valve, and the first signal processing unit processes a signal of the first signal input unit to obtain a front wheel main control signal; the front wheel main control signal is sent to the front wheel main channel electromagnetic valve; the front wheel standby servo channel electromagnetic valve control module comprises a second signal input unit, a second signal processing unit and a front wheel standby channel electromagnetic valve, and the second signal processing unit processes a signal of the second signal input unit to obtain a front wheel standby control signal; and the front wheel standby control signal is sent to the front wheel standby channel electromagnetic valve. It can be guaranteed that a pilot accurately controls the front wheel turning deflection position of the aircraft, and the front wheel turning reliability is improved.

    本申请属于飞机系统控制领域,特别涉及一种飞机两余度前轮转弯系统控制装置。包括:所述前轮主伺服通道电磁阀控制模块包括第一信号输入单元、第一信号处理单元以及前轮主通道电磁阀,所述第一信号处理单元通过对所述第一信号输入单元的信号进行处理,得到前轮主控制信号,并将所述前轮主控制信号发送给所述前轮主通道电磁阀;所述前轮备伺服通道电磁阀控制模块包括第二信号输入单元、第二信号处理单元以及前轮备通道电磁阀,所述第二信号处理单元通过对所述第二信号输入单元的信号进行处理,得到前轮备控制信号,并将所述前轮备控制信号发送给所述前轮备通道电磁阀。本申请能够保证飞行员精确控制飞机前轮转弯偏转位置,提高前轮转弯的可靠性。


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    Titel :

    Airplane dual-redundancy front wheel turning system control device


    Weitere Titelangaben:

    一种飞机两余度前轮转弯系统控制装置


    Beteiligte:
    ZHAO ZHONGRUI (Autor:in) / YU MINGDONG (Autor:in) / ZHANG LEI (Autor:in) / LUO JIANING (Autor:in)

    Erscheinungsdatum :

    2024-01-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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