The invention relates to a rudder wing servo driving system integrated with a feedback mechanism, belongs to the technical field of servo control, and solves the problem of low control accuracy caused by the fact that the actual rotating angle of a rudder wing cannot be monitored in real time when the existing servo mechanism drives the rudder wing to rotate in the prior art. A rudder wing servo driving system integrated with a feedback mechanism comprises an electric servo rotary steering engine, a rudder wing assembly and the feedback mechanism. The number of the rudder wing assemblies is two, and each rudder wing assembly comprises a rudder wing mounting seat, a torsional spring and a rudder wing; the rudder wing is rotationally mounted on the rudder wing mounting seat, and a torsional spring is arranged between the rudder wing and the rudder wing mounting seat; the two ends of an output shaft of the electric servo rotary steering engine are fixedly connected with the two rudder wing mounting seats respectively; the feedback mechanism is used for monitoring the rotation angle of the output shaft. According to the invention, rotation driving of the rudder wing and real-time monitoring of the rotation angle of the rudder wing are realized, and feedback control of the rudder wing is realized.

    本发明涉及一种集成反馈机构的舵翼伺服驱动系统,属于伺服控制技术领域,解决了现有技术中现有的伺服机构驱动舵翼转动时不能实时监测舵翼的实际转角,导致控制准确度低的问题。一种集成反馈机构的舵翼伺服驱动系统,包括:电动伺服旋转舵机、舵翼组件和反馈机构;所述舵翼组件有两组,所述舵翼组件包括:舵翼安装座、扭簧和舵翼;所述舵翼转动安装在舵翼安装座上,且舵翼和舵翼安装座之间设有扭簧;所述电动伺服旋转舵机的输出轴的两端分别与两个舵翼安装座固定连接;所述反馈机构用于监测所述输出轴的旋转角度。本发明实现了对舵翼的旋转驱动以及对舵翼转角的实时监测,实现了对舵翼的反馈控制。


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    Title :

    Rudder wing servo driving system of integrated feedback mechanism


    Additional title:

    一种集成反馈机构的舵翼伺服驱动系统


    Contributors:
    WENG JIA (author) / LIU BING (author) / HUANG FEI (author) / HUANG ZHIPENG (author) / WANG ZHANJIE (author) / LIU CHENGYANG (author) / LIN XINGJIE (author) / GAO WEIGUO (author)

    Publication date :

    2023-03-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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