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.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Vibration reduction undercarriage of aircraft


    Beteiligte:
    SUN XIKUO (Autor:in) / SUN XIYI (Autor:in)

    Erscheinungsdatum :

    21.10.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    "Aircraft Undercarriage"

    Scoles, J. J. / Canadian Aeronautics and Space Institute | British Library Conference Proceedings | 1997


    AIRCRAFT UNDERCARRIAGE

    LUXMOORE BENJAMIN / GRUNDY JACOB / MCDONALD PAUL et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Aircraft undercarriage

    Europäisches Patentamt | 2021

    Freier Zugriff

    Aircraft undercarriage

    BENJAMIN FAIRFAX LUXMOORE / JACOB JOSEPH GRUNDY / PAUL ROBERT MCDONALD et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    AIRCRAFT UNDERCARRIAGE

    LUXMOORE BENJAMIN FAIRFAX / GRUNDY JACOB JOSEPH / MCDONALD PAUL ROBERT et al. | Europäisches Patentamt | 2024

    Freier Zugriff