The invention discloses a single-degree-of-freedom less-drive full-deformation wing mechanism based on multiple connecting rods. The single-degree-of-freedom less-drive full-deformation wing mechanism comprises a fixedly arranged wing front edge, a wing middle part, a wing rear edge, a plurality of connecting rods, a plurality of connecting rods, a plurality of connecting rods and a plurality of connecting rods, the connecting rod assembly is hinged to the wing middle part and the wing rear edge and drives the wing middle part and the wing rear edge to change the bending degree; the power assembly drives the connecting rod assembly; wherein the connecting rod assembly comprises a connecting inclined rod, a connecting cross rod, a first transmission cross rod, a first transmission inclined rod, a second transmission cross rod, a second transmission inclined rod, a third transmission cross rod, a third transmission inclined rod and a fourth transmission cross rod. According to the invention, not only can large-range bending deformation of the wings be realized, but also linkage deformation of the whole wings can be realized only through one power source.

    本发明公开了一种基于多连杆的单自由度少驱动全变形机翼机构包括固定设置的机翼前缘、与机翼前缘活动连接且弯度可变的机翼中部、与机翼中部活动连接且弯度可变的机翼后缘、分别与机翼前缘、机翼中部和机翼后缘相铰接并带动机翼中部和机翼后缘改变弯度的连杆组件以及为连杆组件驱动的动力组件,其中连杆组件包括连接斜杆、连接横杆、第一传动横杆、第一传动斜杆、第二传动横杆、第二传动斜杆、第三传动横杆、第三传动斜杆和第四传动横杆。本发明不仅能够实现机翼大范围的弯度变形,而且还能仅通过一个动力源就能实现整个机翼的联动变形。


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    Titel :

    Single-degree-of-freedom less-drive full-deformation wing mechanism based on multiple connecting rods


    Weitere Titelangaben:

    一种基于多连杆的单自由度少驱动全变形机翼机构


    Beteiligte:
    GUO JINWEI (Autor:in) / HE JIANLIANG (Autor:in) / ZHANG GUOXING (Autor:in) / XIA XINLU (Autor:in) / LAN KAISHUN (Autor:in) / WANG JIA (Autor:in) / LI CHONG (Autor:in)

    Erscheinungsdatum :

    2022-07-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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