The invention discloses a connecting rod mechanism type power system tilting mechanism which comprises a driving mechanism, a mounting frame and a connecting rod mechanism. The driving mechanism comprises a driving device and a power rocker arm, two ends of the power rocker arm form a first end and a second end, and the first end is connected with an output end of the driving device; a propeller hub fixing part is formed on one side of the mounting frame, a mounting part is formed on the other side, and a first mounting part and a second mounting part are formed at two ends of the mounting part; the link mechanism comprises a first link, a second link and a third link; one end of the first connecting rod forms a first fixed end connected with an aircraft fuselage, and the other end is hinged with the second connecting rod; the other end of the second connecting rod is hinged with the first mounting part; and two ends of the third connecting rod are respectively hinged with the second mounting part and the fourth end part. The invention further discloses an aircraft. The method has the characteristics of high control precision and good control stability.

    本发明公开了一种连杆机构式动力系统倾转机构包括驱动机构、安装架与连杆机构;驱动机构包括驱动装置与动力摇臂,动力摇臂两端形成第一端部与第二端部,第一端部与驱动装置输出端连接;安装架一侧形成浆毂固定部,另一侧形成安装部,安装部两端形成第一安装部与第二安装部;连杆机构包括第一连杆、第二连杆与第三连杆;第一连杆一端形成与航空器机身连接的第一固定端,另一端与第二连杆铰接;第二连杆另一端与第一安装部铰接;第三连杆中段与第一连杆铰接,两端分别与第二安装部、第四端部铰接。本发明还公开了一种航空器。本发明具有控制精度高、控制稳定性好的特点。


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    Titel :

    Connecting rod mechanism type power system tilting mechanism and aircraft


    Weitere Titelangaben:

    一种连杆机构式动力系统倾转机构及航空器


    Beteiligte:
    HUANG PEIDONG (Autor:in) / LIU YITAO (Autor:in) / WANG WEIMIN (Autor:in)

    Erscheinungsdatum :

    2024-03-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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