A shimmy damper assembly may comprise: a damper piston including a piston head, the piston head comprising a first permanent magnet, a shimmy cylinder including a second permanent magnet disposed on an axial surface of the shimmy cylinder, and a gland nut coupled to the shimmy cylinder, the gland nut including a third permanent magnet spaced apart axially from the second permanent magnet, the piston head disposed between the first permanent magnet and the second permanent magnet.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    SELF-SUSTAINING SHIMMY DAMPER SYSTEM FOR LANDING GEAR SHOCK STRUT ASSEMBLIES


    Beteiligte:
    NAGARAJA HEMANTH (Autor:in) / BODKI BASAVARAJ (Autor:in) / JAIN BHUWAN (Autor:in)

    Erscheinungsdatum :

    15.06.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F16F SPRINGS , Federn



    SELF-SUSTAINING SHIMMY DAMPER SYSTEM FOR LANDING GEAR SHOCK STRUT ASSEMBLIES

    NAGARAJA HEMANTH / BODKI BASAVARAJ / JAIN BHUWAN | Europäisches Patentamt | 2023

    Freier Zugriff

    SELF-SUSTAINING SHIMMY DAMPER SYSTEM FOR LANDING GEAR SHOCK STRUT ASSEMBLIES

    NAGARAJA HEMANTH / BODKI BASAVARAJ / JAIN BHUWAN | Europäisches Patentamt | 2023

    Freier Zugriff

    Landing gear shimmy damper and aircraft

    ZOU XIANGFU / LI FUYOU | Europäisches Patentamt | 2024

    Freier Zugriff

    Friction-based shimmy damper for landing gear

    NARAYAN KARTHIK | Europäisches Patentamt | 2016

    Freier Zugriff

    SHOCK STRUT ASSEMBLIES FOR LANDING GEAR

    FAZELI AMIR / REBER SUSANNE M | Europäisches Patentamt | 2022

    Freier Zugriff