The invention discloses a tilt rotor platform, which relates to the technical field of rotor aircrafts and comprises at least one rotor mounting mechanism. The tilting mechanism comprises a tilting mechanism and a rotating mechanism; the tilting mechanism comprises an input sleeve, an output sleeve and a tilting driver; the upper end of the input sleeve and the lower end of the output sleeve are rotationally connected around a first axis; a traction part is arranged on the outer side wall of the output sleeve, and the tilting driver can pull the traction part and enable the output sleeve to rotate around a first axis; the rotating mechanism comprises a rotating driver, an input transmission shaft, a universal joint assembly and an output transmission shaft; the output end of the rotary driver is fixedly connected with one end of the input transmission shaft; one end of the input transmission shaft is fixedly connected with one end of the universal joint assembly, and one end of the output transmission shaft is fixedly connected with one end of the universal joint assembly. Therefore, the rotor wing can perform the tilting action, the tilting transition state of the tilting rotor wing can be better simulated, and the test result is more suitable for the actual situation.

    本发明公开了一种倾转旋翼平台,涉及旋翼飞行器技术领域,包括至少一个旋翼安装机构;其包括倾转机构和旋转机构;倾转机构包括输入套筒、输出套筒和倾转驱动器;输入套筒的上端与输出套筒的下端绕第一轴线转动连接;输出套筒的外侧壁上设有牵引部,倾转驱动器能拉动牵引部并使输出套筒绕第一轴线转动;旋转机构包括旋转驱动器、输入传动轴、万向节组件和输出传动轴;旋转驱动器的输出端与输入传动轴的一端固定连接;输入传动轴的一端与万向节组件的一端固连,且输出传动轴的一端与万向节组件的一端固定连接。使旋翼能进行倾转动作,使其更好模拟倾转旋翼的倾转过渡状态,使测试结果更贴合实际情况。


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    Title :

    Tilting rotor platform


    Additional title:

    一种倾转旋翼平台


    Contributors:
    ZHAO QIJUN (author) / LIANG CHENGLIANG (author) / FEI ZHONGYANG (author) / CHEN XI (author) / ZHAO GUOQING (author) / CHEN ZHE (author)

    Publication date :

    2024-12-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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