A torque bar assembly for use in an aircraft wheel is disclosed. In various embodiments, the assembly includes a torque bar (224); and a spacer (240) configured for positioning between the torque bar (224) and a wheel well (207) of the aircraft wheel and to thermally insulate the wheel well (207) from the torque bar (224), wherein the spacer (240) includes a first anodized metal oxide layer (250) on a first surface of the spacer configured to contact the torque bar (224). In various embodiments, the spacer (240) includes a second anodized metal oxide layer (252) on a second surface of the spacer configured to contact the wheel well (207).


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    Titel :

    AIRCRAFT WHEEL TORQUE BAR SPACER


    Weitere Titelangaben:

    ABSTANDSHALTER EINES FLUGZEUGRADDREHMOMENTSTABS
    ENTRETOISE DE BARRE DE TORSION DE ROUE D'AÉRONEF


    Beteiligte:
    WHITTLE SCOTT (Autor:in)

    Erscheinungsdatum :

    12.04.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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