The invention belongs to the technical field of airplane horizontal tail elevator maneuverability testing, and particularly relates to an airplane horizontal tail elevator maneuverability testing device and method, and the airplane horizontal tail elevator maneuverability testing device comprises a maneuvering rocker arm and a rotating shaft connected with an airplane horizontal tail elevator; operating the actuating cylinder; the control load sensor is connected between the rocker arm and the control actuating cylinder; manipulating the displacement sensor; the control displacement connecting wire is connected between the displacement sensor and the control actuating cylinder; the control controller is connected with the control actuating cylinder, the control load sensor and the control displacement sensor; an actuating cylinder is loaded; the loading load sensor is connected between the loading actuator cylinder and the plane horizontal tail stabilizer; and the loading controller is connected with the loading actuating cylinder and the loading load sensor.

    本申请属于飞机平尾升降舵操纵性能试验技术领域,具体涉及一种飞机平尾升降舵操纵性能试验装置及其方法,其中,飞机平尾升降舵操纵性能试验装置包括:操纵摇臂,连接飞机平尾升降舵的转轴;操纵作动筒;操纵载荷传感器,连接在摇臂、操纵作动筒之间;操纵位移传感器;操纵位移连接丝,连接在位移传感器、操纵作动筒之间;操纵控制器,连接操纵作动筒、操纵载荷传感器、操纵位移传感器;加载作动筒;加载载荷传感器,连接在加载作动筒、飞机平尾安定面之间;加载控制器,连接加载作动筒、加载载荷传感器。


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    Titel :

    Airplane horizontal tail elevator maneuverability test device and method thereof


    Weitere Titelangaben:

    一种飞机平尾升降舵操纵性能试验装置及其方法


    Beteiligte:
    ZANG WEIFENG (Autor:in) / CHENG HUA (Autor:in) / CHEN AN (Autor:in) / ZHANG HAIYING (Autor:in) / LI GANG (Autor:in)

    Erscheinungsdatum :

    2023-06-23


    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



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