The invention discloses a rudder control system and a rudder pedal jamming slowing down method, so that a flight control system of an aircraft can slow down the adverse effect of a rudder pedal on lateral course control and ground direction control of the aircraft when the rudder pedal is jammed and jammed at a certain large angle (position). The invention relates to a rudder control system (10) for an aircraft to enable the aircraft to continue to fly and land safely, the rudder control system (10) comprising a flight control unit (120), and the flight control unit can receive a second rudder control instruction which is different from the first rudder control instruction received when the rudder pedal works normally from the rudder control signal output unit (11) when the rudder pedal is blocked or fails, so as to instruct the rudder deflection actuating unit (122) to deflect the rudder.

    一种方向舵控制系统和方向舵脚蹬卡阻减缓方法,使得飞机的飞控系统能够在方向舵脚蹬发生卡阻并且卡阻在某一较大的角度(位置)时减缓此时的方向舵脚蹬对飞机的横航向操纵和地面方向控制的不利影响,以使飞机能够继续安全飞行和着陆,所述方向舵控制系统(10)包括飞行控制单元(120),所述飞行控制单元能在方向舵脚蹬发生卡阻或失效时接受来自方向舵控制信号输出单元(11)中的与在方向舵脚蹬正常工作时接受到的第一方向舵控制指令不同的第二方向舵控制指令,来指令方向舵偏转作动单元(122)使方向舵偏转。


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    Titel :

    Rudder control system and rudder pedal jamming retarding method


    Weitere Titelangaben:

    方向舵控制系统和方向舵脚蹬卡阻减缓方法


    Beteiligte:
    WANG ZHENHUA (Autor:in) / YU MIAO (Autor:in) / SHENG WEIQIANG (Autor:in) / LI HONGYU (Autor:in) / QIAO WENFENG (Autor:in) / LIU QINGTAO (Autor:in)

    Erscheinungsdatum :

    15.11.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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