A magnetic shock absorber (11) comprising a first body (12) slidably coupled to a second body (14) via a first bearing (24a) arranged to move in sliding engagement with a first counter-face portion (26a). A first array of magnets (18) associated with the first body is arranged to magnetically interact with a second array of magnets (22) is associated with the second body to absorb compression or extension loads applied to the shock absorber. The first bearing and the first counter-face portion each have a non-circular cross section profile (27) to inhibit axial relative rotation between the bodies.


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    Titel :

    AIRCRAFT LANDING GEAR SHOCK ABSORBER


    Weitere Titelangaben:

    FLUGZEUGFAHRWERKSTOSSDÄMPFER
    AMORTISSEUR DE CHOCS POUR TRAIN D'ATTERRISAGE D'AERONEF


    Beteiligte:
    SIMONNEAUX YANN (Autor:in) / WHITMAN STEVE (Autor:in)

    Erscheinungsdatum :

    18.01.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16F SPRINGS , Federn / B64C AEROPLANES , Flugzeuge



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