A bearing assembly 1 for installation in a through-hole 10 in a composite material 8, the bearing assembly comprising a first bush 2a and a second bush 2b, each of the first and second bushes 2a, 2b having a flange 6a, 6b. The first and second bushes 2a, 2b are held together such that, in use, when the bearing assembly 1 is installed in the through-hole 10 with the flanges 6a, 6b of the first and second bushes 2 on opposite sides of the material 8 the flanges 6a, 6b limit the axial movement of the bushes 2a, 2b relative to the through-hole 10. The bearing assembly 1 may also include an annular sleeve 18 which has a spherical bearing 20 mounted therein, and two inner bushes 22a, 22b mounted within the spherical bearing 20, at either end of the through-hole 10 and concentric with it.


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    Titel :

    Bearing assembly


    Beteiligte:

    Erscheinungsdatum :

    28.11.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F16C SHAFTS , Wellen



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