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).
AIRCRAFT WHEEL TORQUE BAR SPACER
ABSTANDSHALTER EINES FLUGZEUGRADDREHMOMENTSTABS
ENTRETOISE DE BARRE DE TORSION DE ROUE D'AÉRONEF
2023-04-12
Patent
Electronic Resource
English