The invention relates to a vibration reduction undercarriage of an aircraft. The vibration reduction undercarriage is installed on an aircraft support. The vibration reduction undercarriage comprises an undercarriage body with the annular section. The undercarriage body is sleeved with at least four rubber rings. During working, the undercarriage body is fixed to the bottom of the support. According to the vibration reduction undercarriage of the aircraft, rubber is installed on the aircraft so that the vibration reduction effect is achieved and the deformation of a rack is avoided, and therefore the service life of the aircraft is prolonged.


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    Title :

    Vibration reduction undercarriage of aircraft


    Contributors:
    SUN XIKUO (author) / SUN XIYI (author)

    Publication date :

    2015-10-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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