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
12.04.2023
Patent
Elektronische Ressource
Englisch