The invention provides a large-load undercarriage spring which comprises an outer barrel, an inner barrel, a spring and a spring body. The outer barrel is provided with a single-lug structure and a barrel-shaped structure. The plug cap is arranged at the end part of the cylindrical structure of the outer cylinder and is used for supporting the cylindrical structure of the outer cylinder; the piston rod is provided with a round rod structure and a single-lug structure, the round rod structure of the piston rod penetrates through the plug cap and partially extends into the cylindrical structure of the outer cylinder, and an end bolt is installed at the end of the round rod structure; the front supporting sleeve and the rear supporting sleeve are installed on the cylindrical structure inner round rod structure extending into the outer cylinder, the front supporting sleeve is in contact with the outer cylinder, and the rear supporting sleeve is in contact with the plug cap; the spring is arranged on the front supporting sleeve and the rear supporting sleeve in a sleeving mode and located in the cylindrical structure of the outer cylinder, the two ends of the spring make contact with the front supporting sleeve and the rear supporting sleeve respectively, and the spring is a compression spring. The undercarriage tension spring can solve the problems that a tension spring is insufficient in bearing capacity and poor in stability.

    本申请提供了一种大载荷起落架弹簧,包括:外筒,该外筒具有单耳结构及筒状结构;堵帽,该堵帽设置在外筒的筒状结构端部,用于支撑所述外筒的筒状结构;活塞杆,该活塞杆具有圆杆结构及单耳结构,所述活塞杆的圆杆结构穿过堵帽而部分的伸入至所述外筒的筒状结构内,所述圆杆结构的端部安装有端头螺栓;前支撑套和后支撑套,该前支撑套和后支撑套安装在伸入至外筒的筒状结构内圆杆结构上,该前支撑套与外筒相接触,所述后支撑套与堵帽相接触;弹簧,所述弹簧套在所述前支撑套和后支撑套上,且位于外筒的筒状结构内,弹簧的两端分别接触于前支撑套和后支撑套,其中,弹簧为压缩弹簧。该起落架拉簧能解决拉簧承载能力不足、稳定性差的问题。


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    Titel :

    Large-load undercarriage tension spring


    Weitere Titelangaben:

    一种大载荷起落架拉簧


    Beteiligte:
    ZHANG JIANJIAN (Autor:in) / ZHANG GUONING (Autor:in) / LI ZHAORUI (Autor:in) / ZHANG LIJUN (Autor:in)

    Erscheinungsdatum :

    2023-01-24


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    F16F SPRINGS , Federn / B64C AEROPLANES , Flugzeuge / F16N LUBRICATING , Schmierung



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