The invention discloses a hydraulic actuator fault monitoring method for an aircraft flight control system. The method comprises the following steps: firstly, creating fault model classification; creating an actuator state equation expression under a normal working condition; then creating an actuator state equation expression in a fault state; performing hydraulic actuator fault detection by using an equivalent space method; fault estimation is carried out on the hydraulic actuator; and finally, monitoring the fault of the hydraulic actuator according to a fault estimation result. The fault of the hydraulic actuator can be identified, and the health state of the hydraulic actuator can be monitored, so that the possible fault opportunity and the residual life of the aircraft can be accurately predicted, and the aircraft can be ensured to fly as safely and reliably as possible.

    本发明公开了一种飞机飞行控制系统的液压作动器故障监测方法,首先创建故障模型分类;接下来创建正常工作情况下作动器状态方程表达式;然后创建故障状态下作动器状态方程表达式;使用等价空间法进行液压作动器故障检测;再进行液压作动器故障估计;最终根据故障估计结果,实现对液压作动器故障的监测。本发明可以识别液压作动器故障,并且可以对液压作动器健康状态进行监控,从而对飞机可能出现的故障时机和剩余寿命进行准确预测,确保飞机尽可能地安全可靠飞行。


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    Titel :

    Fault monitoring method for hydraulic actuator of aircraft flight control system


    Weitere Titelangaben:

    一种飞机飞行控制系统的液压作动器故障监测方法


    Beteiligte:
    LIU ZHENBAO (Autor:in) / WANG LINA (Autor:in) / DANG QINGQING (Autor:in) / ZHAO WEN (Autor:in) / ZHANG CHAO (Autor:in)

    Erscheinungsdatum :

    2023-01-06


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung



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