The invention relates to a braking device (1) of an aircraft wheel, comprising a ring (15) which has a plurality of cavities (17) in which actuators (18) are fitted in order to apply a braking force to a stack of discs (11) which extend opposite the ring. The ring is provided with a heat shield (25) which extends opposite a face of the ring directed towards the stack of discs in order to protect the ring from thermal radiation which is generated by the stack of discs.According to the disclosure, the heat shield is provided with holes (26) through which the actuators extend and which have a sectional profile which is formed to reflect the thermal radiation away from the device.
ECRAN THERMIQUE POUR DISPOSITIF DE FREINAGE D'UNE ROUE D'AERONEF
HEAT SHIELD FOR A BRAKING DEVICE OF AN AIRCRAFT WHEEL
HITZESCHILD FÜR EINE BREMSVORRICHTUNG EINES FLUGZEUGRADS
2024-10-30
Patent
Electronic Resource
French
ECRAN THERMIQUE POUR DISPOSITIF DE FREINAGE D'UNE ROUE D'AERONEF
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