A brake stack is disclosed. In various embodiments, the brake stack includes a pressure plate; an end plate; a rotor disk disposed between the pressure plate and the end plate, the rotor disk including a rotor core comprising a carbon-carbon material and a boron-containing component; and a stator disk disposed between the pressure plate and the end plate, the stator disk including a stator core comprising the carbon-carbon material and the boron component. In various embodiments, the boron-containing component exhibits a higher heat capacity than a corresponding friction liner that comprises a ceramic matrix composite material, applied by chemical vapor infiltration, and that provides a surface optimized for aircraft brake friction and wear.


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    Titel :

    AIRCRAFT BRAKE HEATSINK WEAR LINER


    Beteiligte:
    LINCK JOHN (Autor:in)

    Erscheinungsdatum :

    2020-06-25


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen / B64C AEROPLANES , Flugzeuge / C04B Kalk , LIME



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