The invention discloses a high-lift system for an aircraft. With the high-lift system for the aircraft adopted, the mechanical control of a pilot can be accurately acquired, an effective system instruction can be selected, and the usability of a system can be improved. The high-lift system for the aircraft comprises two dual-channel computers and a single-channel computer; a control handle is provided with rotary variable differential pressure transducers, wherein the number of the rotary variable differential pressure transducers is the same as that of five channels in the high-lift system for the aircraft. Each of the five channels exchanges the signals and signal instructions of the corresponding rotary variable differential transformer sensor with each other in the same time sequence.And after a certain number of system instructions are received in a certain channel, namely a to-be-voted channel, effective system instructions are selected in the to-be-voted channel through a voting mechanism, and are sent to a motor of a power driving unit corresponding to the to-be-voted channel.

    一种飞机高升力系统,能精准地获知飞行员的机械操纵,选择有效的系统指令,提高系统的可用性。所述飞机高升力系统包括两个双通道计算机和一个单通道计算机,操纵手柄具有与所述飞机高升力系统中所具有的五个通道相同数量的旋转可变差动变压传感器,五个通道中的每个都在相同的时间序列内相互交换各自的对应的所述旋转可变差动变压器传感器的信号与信号指令,在某一通道即待表决通道中收到一定数量的系统指令后,在待表决通道内部通过表决机制,选择出有效系统指令,并发送至与待表决通道对应的动力驱动单元的马达。


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    Titel :

    High-lift system for aircraft


    Weitere Titelangaben:

    飞机高升力系统


    Beteiligte:
    WANG WEIDA (Autor:in) / CHEN YONG (Autor:in) / YANG ZHIDAN (Autor:in) / WANG XIAOYI (Autor:in) / FANG FENG (Autor:in) / LIU JINTAO (Autor:in)

    Erscheinungsdatum :

    2020-06-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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