The invention provides a novel double-cavity undercarriage buffer device, and belongs to the technical field of undercarriage buffer design, an oil injection and inflation nozzle of a buffer is installed at the left end of the upper portion of a first outer cylinder, and an upper anti-torsion arm is hinged to the lower portion of the first outer cylinder; the lower anti-torsion arm is hinged to the inner cylinder, and the airplane wheel is connected to the right end below the inner cylinder; the supporting ring is mounted on the inner cylinder to form an inner cylinder assembly; the valve is placed in the damping plate, the third nut is in threaded connection with an inner threaded hole of the damping plate, and the damping plate is in threaded connection with the lower end of the oil needle to form an oil needle assembly; the oil needle assembly is installed in the inner cylinder assembly and installed in the first outer cylinder together with the inner cylinder assembly, the upper end is connected with the first outer cylinder, and the lower end fixes the supporting ring and the first outer cylinder through a connecting piece. The piston is arranged in the second outer cylinder; the high-pressure cavity structure and the low-pressure cavity structure are relatively independent, and design is facilitated; the landing load process is relatively smooth, and the maximum load is lower; the position coordination difficulty of the undercarriage and the high-pressure cavity can be reduced according to the arrangement of the fuselage mounting position.

    本申请提供一种新型双腔起落架缓冲器装置,属于起落架缓冲器设计技术领域,缓冲器的注油充气嘴安装在第一外筒上方左端,上防扭臂铰接在第一外筒下方;下防扭臂铰接在内筒上,机轮连接在内筒下方右端;支撑环安装在内筒上,形成内筒组件;活门放置在阻尼板内,第三螺母螺接在阻尼板的内螺纹孔上,阻尼板螺接在油针的下端,形成油针组件;油针组件安装在内筒组件中,一并装入第一外筒中,且上端与第一外筒连接,下端通过连接件将支撑环与第一外筒固定;活塞装入第二外筒内;本申请高、低压腔结构相对独立,利于设计;着陆载荷过程相对平缓,最大载荷更低;可根据机身安装位置布置,降低起落架和高压腔的位置协调难度。


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    Titel :

    Novel double-cavity undercarriage buffer device


    Weitere Titelangaben:

    一种新型双腔起落架缓冲器装置


    Beteiligte:
    JI MAOLING (Autor:in) / LI PENG (Autor:in) / REN LUBING (Autor:in) / LI YAN (Autor:in) / WANG ZHEN (Autor:in) / GAO LIN (Autor:in) / ZHOU BIN (Autor:in)

    Erscheinungsdatum :

    2023-09-29


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    F16F SPRINGS , Federn / B64C AEROPLANES , Flugzeuge



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