The invention discloses an airfoil steering engine connecting rod structure and an airfoil zero setting method, and relates to the field of aviation parts. One end of the extension rod front section is in threaded connection with the other end of the adapter, and a groove is formed in the other end of the extension rod front section; one end of the extension rod rear section is used for being connected with the wing surface fixing end in a rotating mode, a screw is arranged at the other end of the extension rod rear section, the head of the screw is matched with the opening of the groove in a clamping mode, and the connecting rod structure is a steering engine connecting rod which is simple, practical and high in adjustability.

    本发明公开了一种翼面舵机连杆结构及翼面的调零方法,涉及航空部件领域,包括:转接件,一端用于与舵机螺纹连接;延长杆前段,一端与转接件的另一端螺纹连接,延长杆前段的另一端开设有凹槽;延长杆后段,一端用于与翼面固定端转动连接,延长杆后段的另一端设置有螺钉,螺钉的头部与凹槽的开口卡接配合,该连杆结构为一种简单、实用、可调性高的舵机连杆。


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    Titel :

    Airfoil steering engine connecting rod structure and airfoil zero setting method


    Weitere Titelangaben:

    一种翼面舵机连杆结构及翼面的调零方法


    Beteiligte:
    WANG XIAODONG (Autor:in) / YIN YANBIN (Autor:in) / CHEN ZHU (Autor:in) / YAN DONG (Autor:in) / XING HUANKUI (Autor:in)

    Erscheinungsdatum :

    31.03.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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