The invention discloses a buoy mechanism for a light amphibious aircraft, and relates to the technical field of buoy mechanisms of amphibious aircraft. The takeoff safety of an airplane is ensured. The buoy mechanism comprises two first buoy bodies and two second buoy bodies, a rotating roller is movably connected to the outer wall of one side of each first buoy body, two or more stirring pieces are arranged on the circumferential outer wall of each rotating roller, a rotating disc is arranged on the circumferential outer wall of each rotating roller, a rocker is movably connected to the outer wall of one side of each rotating disc, an adjusting frame is movably connected to one end of the rocker, a push rod is arranged on the outer wall of one side of the adjusting frame, a pressing disc is arranged on the outer wall of one side of the push rod, and two second convex columns are movably connected to the outer wall of one side of the pressing disc. The first buoy bodies and the second buoy bodies are connected and fixed, so that the first buoy bodies and the second buoy bodies integrally float on the water surface, and the whole aircraft body is conveniently supported.

    本发明公开了一种用于轻型水陆两栖飞机的浮筒机构,涉及水陆两栖飞机浮筒机构技术领域;为了保证飞机起飞的安全;包括两个浮筒主体一和两个浮筒主体二,所述浮筒主体一一侧外壁活动连接有转动辊,所述转动辊圆周外壁设置有两个以上拨动片,所述转动辊圆周外壁设置有转动盘,所述转动盘一侧外壁活动连接有摇杆,所述摇杆一端活动连接有调节架,所述调节架一侧外壁设置有推杆,所述推杆一侧外壁设置有压盘,所述压盘一侧外壁活动连接有两个凸形柱二。本发明通过将浮筒主体一和浮筒主体二之间进行连接固定,从而可以使得浮筒主体一和浮筒主体二整体漂浮在水面上,从而便于对飞机主体整体进行支撑。


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    Title :

    Buoy mechanism for light amphibious aircraft


    Additional title:

    一种用于轻型水陆两栖飞机的浮筒机构


    Contributors:
    ZENG RUHAI (author) / LI JINDONG (author) / HU DOU (author)

    Publication date :

    2021-09-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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