An aircraft braked wheel comprising a rim integral with a hub for rotationally mounting thereof on an axle of the aircraft along an axis of rotation, the wheel being equipped with a heat shield (11) extending opposite an inner face of the rim to protect the rim from the thermal radiation generated by a stack of discs extending inside the rim, characterized in that the heat shield has a face facing the discs (15) which has longitudinal ribs (16) extending in operation parallel to the axis of rotation of the wheel.
ECRAN THERMIQUE POUR ROUE FREINEE D'AERONEF
HEAT SHIELD FOR A BRAKED AIRCRAFT WHEEL
HITZESCHILD FÜR GEBREMSTES RAD EINES LUFTFAHRZEUGS
2021-09-01
Patent
Electronic Resource
French