The invention provides a rotor wing propeller hub centering structure of a rotorcraft and the rotorcraft, and relates to the technical field of rotorcraft design, the rotor wing propeller hub centering structure is used for centering and assembling a propeller hub of the rotorcraft on a rotor wing shaft of the rotorcraft, the propeller hub is connected with the rotor wing shaft through a spline, the centering structure comprises two centering rings, the two centering rings are connected and clamped on the rotor wing shaft in a sleeving mode, and the two centering rings are connected through a spline. The two centering rings are respectively arranged above and below the propeller hub; the rotor shaft is sleeved with the two bearing parts, the two bearing parts are connected to the top and the bottom of the propeller hub correspondingly, and the top and the bottom of the inner side of one bearing part are connected with one centering ring and the top of the inner side of the propeller hub in an attached mode through conical surfaces correspondingly; the bottom and the top of the inner side of the other bearing component are connected with the bottom of the inner side of the other centering ring and the bottom of the inner side of the propeller hub in an attached mode through conical surfaces. The coaxiality of the propeller hub and the rotor shaft is effectively guaranteed, high-precision centering of the propeller hub is achieved, precise control over the torque of the rotor is facilitated, and the maneuverability of the whole machine is improved.

    本发明提供一种旋翼机的旋翼桨毂定心结构及旋翼机,设计旋翼机技术领域,用于将旋翼机的桨毂定心装配在旋翼机的旋翼轴上,桨毂与旋翼轴通过花键连接,该定心结构包括:两定心环,两定心环套接且卡定在旋翼轴上,两定心环分别设置在桨毂上方和下方;两承载部件,两承载部件套接在旋翼轴上,两承载部件分别连接在桨毂的顶部和底部,其中一个承载部件的内侧顶部和底部分别通过锥面与其中一个定心环和桨毂的内侧顶部贴合连接,另一个承载部件的内侧底部和顶部分别通过锥面与另一个定心环和桨毂的内侧底部贴合连接;有效保证了桨毂和旋翼轴的同轴度,实现了桨毂的高精度定心,有利于旋翼力矩的精准控制,提高了整机的操纵性。


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    Title :

    Rotor propeller hub centering structure of rotorcraft and rotorcraft


    Additional title:

    一种旋翼机的旋翼桨毂定心结构及旋翼机


    Contributors:
    WANG BINGCHAO (author) / XU ZHIXIONG (author) / WANG TIANYUAN (author)

    Publication date :

    2024-11-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64U



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