The invention relates to a variable cycle aircraft paddle adjusting device and a control method thereof. Comprising a shell, a connecting shaft, a connecting shaft lifting module and a connecting shaft driving module, wherein the connecting shaft lifting and driving device consists of the connecting shaft, the connecting shaft lifting module and the connecting shaft driving module which are accommodated in the shell; the tilting motors are respectively arranged on the left side and the right side of the shell through transmission shafts; the power motor is respectively connected with main shafts of the first tilting motor and the second tilting motor through a buckling end on the left side or the right side of the connecting block; the main shafts are connected to a push-pull motor on the connecting block on one side opposite to the buckling end; a push rod motor in the connection shaft lifting module drives a connection shaft to ascend and descend, so that meshing transmission and separation between the connection shaft lifting module and the connection shaft rotation driving module are achieved, and nesting and separation between the connection shaft and a transmission shaft are achieved. The paddle adjusting device has the advantages of being high in flexibility, high in efficiency, convenient to design, use and maintain and the like.

    本发明涉及一种变循环飞行器桨叶调节装置及其控制方法,其中桨叶调节装置,包括:由外壳以及容纳于外壳内部的联络轴、联络轴提升模块和联络轴带转模块组成的联络轴提升与带转装置、经传动轴分别安装于外壳左、右两侧的倾转电机、通过连接块的左侧或右侧上的卡扣端分别连接第一倾转电机和第二倾转电机主轴的动力电机、主轴连接至与卡扣端相对一侧的连接块上的推拉电机;其中,由联络轴提升模块中的推杆电机驱动联络轴升降,实现联络轴提升模块与联络轴带转模块之间的啮合传动与分离,以及联络轴与传动轴之间的嵌套与分离。本发明桨叶调节装置具有灵活性强、效率高,设计、使用和维护方便等特点。


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    Titel :

    Variable cycle aircraft paddle adjusting device and control method thereof


    Weitere Titelangaben:

    一种变循环飞行器桨叶调节装置及其控制方法


    Beteiligte:
    GUO YUCHAO (Autor:in) / LI YI (Autor:in) / WANG WEITAO (Autor:in) / RUAN CHANGLONG (Autor:in) / ZHANG JIBO (Autor:in) / LIN ZONGYUAN (Autor:in) / DAI XIANDONG (Autor:in) / WANG WENZHI (Autor:in) / DING SHU (Autor:in) / ZHANG CHUNYAO (Autor:in)

    Erscheinungsdatum :

    23.06.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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