The present invention discloses a helicopter undercarriage having a vibration reduction function. The helicopter undercarriage comprises a base plate and a support plate connected to the base plate, wherein an included angle is formed between the planes of the base plate and the support plate, and the base plate and the support plate are made from carbon fibers. According to the present invention, the included angle is arranged between the planes of the base plate and the support plate, and the base plate and the support plate are made from the carbon fibers, such that the buffer effect can be provided when the helicopter lands, and the impact force generated during the helicopter landing can be subtracted so as to effectively prevent the helicopter from damage caused by the undercarriage or prevent the equipment or instruments arranged inside the helicopter body from damage.


    Access

    Download


    Export, share and cite



    Title :

    Helicopter undercarriage having vibration reduction function


    Contributors:
    JIANG LEI (author)

    Publication date :

    2016-01-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Helicopter undercarriage with protection function

    HU ZHENBO | European Patent Office | 2021

    Free access

    Helicopter wheel undercarriage sled

    SONG XIANLONG | European Patent Office | 2015

    Free access

    Helicopter undercarriage fixing device

    LIU DENGYAO / HU HAO / GENG JIPENG et al. | European Patent Office | 2023

    Free access

    Vibration reduction undercarriage of aircraft

    SUN XIKUO / SUN XIYI | European Patent Office | 2015

    Free access

    Helicopter pillar type undercarriage

    WANG LE / FANG JIANYI / YANG YUN | European Patent Office | 2023

    Free access