A shimmy damper assembly (300) may comprise: a damper piston (126) including a piston head (314), the piston head comprising a first permanent magnet (316), a shimmy cylinder (322) including a second permanent magnet (325) disposed on an axial surface of the shimmy cylinder (322), and a gland nut (324) coupled to the shimmy cylinder (322), the gland nut (324) including a third permanent magnet (327) spaced apart axially from the second permanent magnet (325), the piston head (314) disposed between the first permanent magnet (316) and the second permanent magnet (325).


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    Titel :

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


    Weitere Titelangaben:

    SELBSTTRAGENDES FLATTERDÄMPFERSYSTEM FÜR FAHRWERKSFEDERBEINANORDNUNGEN
    SYSTÈME AMORTISSEUR DE SHIMMY AUTO-ENTRETENU POUR ENSEMBLES D'AMORTISSEURS DE TRAIN D'ATTERRISSAGE


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

    Erscheinungsdatum :

    21.06.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16F SPRINGS , Federn / B64C AEROPLANES , Flugzeuge



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