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.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Helicopter undercarriage having vibration reduction function


    Beteiligte:
    JIANG LEI (Autor:in)

    Erscheinungsdatum :

    20.01.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Helicopter undercarriage with protection function

    HU ZHENBO | Europäisches Patentamt | 2021

    Freier Zugriff

    Helicopter wheel undercarriage sled

    SONG XIANLONG | Europäisches Patentamt | 2015

    Freier Zugriff

    Helicopter undercarriage fixing device

    LIU DENGYAO / HU HAO / GENG JIPENG et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Vibration reduction undercarriage of aircraft

    SUN XIKUO / SUN XIYI | Europäisches Patentamt | 2015

    Freier Zugriff

    Helicopter pillar type undercarriage

    WANG LE / FANG JIANYI / YANG YUN | Europäisches Patentamt | 2023

    Freier Zugriff