The invention belongs to the field of flight control system design and test in the field of aircraft design, and particularly relates to an aircraft control device force displacement measuring device and method. The device comprises a clamping piece (1), an assembly frame (2), a grip (3), a force measurement unit and an inertia measurement unit, the clamping piece (1) is clamped on an aircraft control device, the grip (3) is fixedly connected with the clamping piece (1) through the assembly frame (2), and the force measurement unit and the inertia measurement unit are laid in the assembly frame (2). The inertia measurement unit and the force measurement unit are arranged to realize combined measurement of the force displacement of the aircraft control device, and the use is simple and convenient; the inertia measurement unit and the force measurement strain gauge are integrated by arranging the assembly frame, miniaturization and integration of the device are achieved, and the device is convenient to use in a small space and carry when people go out.

    本申请属于飞机设计领域的飞控系统设计与测试领域,特别涉及一种飞机操纵器件力位移测量装置及方法。包括夹持件(1)、组件框架(2)、握把(3)、力测量单元、惯性测量单元,夹持件(1)夹装于飞机操纵器件,握把(3)与通过组件框架(2)与夹持件(1)固连,力测量单元与惯性测量单元敷设于组件框架(2)中。通过设置惯性测量单元和力测量单元实现飞机操纵器件力‑位移的组合测量,在使用上简单便捷;通过设置组件框架对惯性测量单元和测力应变片进行集成,实现装置的小型化和集成化,便于在小空间内的使用以及外出携带。


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    Titel :

    Aircraft control device force displacement measuring device and method


    Weitere Titelangaben:

    一种飞机操纵器件力位移测量装置及方法


    Beteiligte:
    JIANG FEIHONG (Autor:in) / WANG HUI (Autor:in) / YANG LINYA (Autor:in) / DU XIAODONG (Autor:in)

    Erscheinungsdatum :

    2021-04-09


    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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