An aircraft includes an airframe and a rotary component rotatably connected to the airframe by way of a plain bearing. The rotary component is part of a rotorcraft control system. The plain bearing includes an inner member rotatably engaged in at least two axes of rotation to an outer member. The inner member has a coefficient of thermal expansion (CTE) substantially less than that of the outer member.


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    Titel :

    SELF-LUBRICATED BEARINGS


    Beteiligte:
    BASKIN BRYAN K (Autor:in)

    Erscheinungsdatum :

    03.05.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16C SHAFTS , Wellen / B64C AEROPLANES , Flugzeuge



    Self-lubricated bearings

    BASKIN BRYAN K | Europäisches Patentamt | 2018

    Freier Zugriff

    The Influence of Misalignment on Self-Lubricated Bearings

    Cooper,J.H. / Garlock Bearings,US | Kraftfahrwesen | 1983


    The Application of Self-Lubricated and Pre-Lubricated Bearings to Off-Highway Equipment

    Cooper, James H. / Perlberg, Richard C. | SAE Technical Papers | 1982


    The Application of Self-Lubricated and Pre-Lubricated Bearings to Off-Highway Equipment

    Perlberg,R.C. / Cooper,J.H. / Garlock Bearings,US | Kraftfahrwesen | 1982