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.


    Access

    Download


    Export, share and cite



    Title :

    SELF-LUBRICATED BEARINGS


    Contributors:

    Publication date :

    2018-05-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F16C SHAFTS , Wellen / B64C AEROPLANES , Flugzeuge



    Self-lubricated bearings

    BASKIN BRYAN K | European Patent Office | 2018

    Free access

    The Influence of Misalignment on Self-Lubricated Bearings

    Cooper,J.H. / Garlock Bearings,US | Automotive engineering | 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 | Automotive engineering | 1982