The invention relates to an aircraft landing gear which is simple in structure, direct in energy transfer, not easy to cause loss and not easy to damage. An aircraft landing gear, comprising: a wheel, the wheel comprising a hub; a landing gear support shaft inserted through the hub and allowing the wheel to rotate; the undercarriage power device drives the hub to rotate, and the undercarriage power device is arranged in a space defined by the outer surface of the axial side of the hub and the circumferential side face of the undercarriage supporting shaft. The landing gear power device is meshed with a hub side gear arranged on the inner ring of the hub through a power device side gear.

    一种飞机起落架,其结构简单,能量传递直接且不容易产生损失,并且不容易发生损坏。飞机起落架,包括:机轮,所述机轮包括轮毂;起落架支撑轴,插通于所述轮毂,供所述机轮旋转;以及起落架动力装置,所述起落架动力装置驱动所述轮毂旋转,所述起落架动力装置配置在由所述轮毂的轴向一侧的外表面与所述起落架支撑轴的周向侧面围成的空间内,所述起落架动力装置通过动力装置侧齿轮与配置在所述轮毂的内圈的轮毂侧齿轮啮合。


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    Titel :

    Aircraft landing gear


    Weitere Titelangaben:

    飞机起落架


    Beteiligte:
    ZOU XINHUANG (Autor:in) / BAO YUTING (Autor:in) / PENG ZIRUI (Autor:in) / HA WEN (Autor:in) / LI XIAOMING (Autor:in) / YUAN NINGNING (Autor:in)

    Erscheinungsdatum :

    2022-03-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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