The invention discloses a transmission mechanism of an aircraft aileron, which comprises a wing, an aileron, a bevel gear transmission mechanism and a driving transmission mechanism, and the driving transmission mechanism is a main motion control and power output component and is fixed at the root of the wing. And the driving transmission mechanism drives the aileron to perform fixed-axis rotation through the bevel gear transmission mechanism, so that the attitude adjustment of the aircraft is realized. According to the transmission mechanism of the aircraft aileron, the longitudinal layout mode along the wing root is adopted, and straight tooth bevel gears are used for transmission. Therefore, the whole transmission mechanism has the characteristics of compact structure, high transmission efficiency and the like.

    本发明公开了一种飞机副翼的传动机构,包括机翼、副翼、锥齿轮传动机构和主动传动机构,主动传动机构为主要运动控制和动力输出部件,被固定在机翼的翼根处。所述主动传动机构通过锥齿轮传动机构带动副翼进行定轴转动,实现飞机姿态调整。本发明所提供的一种飞机副翼的传动机构,采用沿着机翼翼根的纵向布局方式,并且使用直齿圆锥齿轮传动。因此,整个传动机构具有结构紧凑、传动效率高等特点。


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    Title :

    Transmission mechanism of aircraft aileron


    Additional title:

    一种飞机副翼的传动机构


    Contributors:
    WANG ZHENWEI (author) / YANG YU (author) / WANG RUILIN (author) / ZHAO HAN (author)

    Publication date :

    2025-01-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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