The invention relates to the technical field of aero-engines, in particular to an aero-engine fuel regulator detection circuit and method, the circuit comprises a processor, a drive circuit, an analog-to-digital conversion circuit and a signal generation circuit, the processor is connected to the drive circuit, the drive circuit is used for connecting a stepping motor, and the analog-to-digital conversion circuit is connected to the signal generation circuit. The processor is connected to the analog-to-digital conversion circuit, the analog-to-digital conversion circuit is used for being connected to an RVDT sensor, the processor is connected to the signal generation circuit, and the signal generation circuit is connected to the RVDT sensor. The regulator detection method and device have the advantages that the regulator detection cost can be reduced, and regulator detection convenience is improved.

    本申请涉及航空发动机的技术领域,尤其是涉及一种航空发动机燃油调节器检测电路及检测方法,其电路包括处理器、驱动电路、模数转换电路和信号发生电路,所述处理器连接于所述驱动电路,所述驱动电路用于连接步进电机,所述处理器连接于所述模数转换电路,所述模数转换电路用于连接于RVDT传感器,所述处理器连接于所述信号发生电路,所述信号发生电路连接于所述RVDT传感器。本申请具有能够降低调节器检测的成本,提高调节器检测的便利性的效果。


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    Title :

    Aero-engine fuel regulator detection circuit and detection method


    Additional title:

    一种航空发动机燃油调节器检测电路及检测方法


    Contributors:
    HUANG XUEFENG (author) / JING XUN (author) / CHE YINGNA (author) / FENG YANQI (author)

    Publication date :

    2023-10-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / 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



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