An aircraft wheel (1) comprising a hub connected to a rim (3) provided with a tire (100), the hub having an outer surface that extends facing an inner surface (4) of the rim (3) and that co-operates therewith to define an annular space for receiving a stack of brake disks including rotor disks having axial peripheral notches, each notch receiving a segment of an axial bar (10) extending projecting from the inner surface (4) of the rim (3), and respective heat shields (20), each in the form of an annular segment, being mounted between the two bars (10) of respective pairs of adjacent bars. Each heat shield (20) includes at least one holder portion bearing against at least one first abutment (19, 119) secured to the rim (3) in order to hold the heat shield (20) in position on the rim (3) elastically.
ROUE D'AÉRONEF POURVUE D'ÉCRANS THERMIQUES
AIRCRAFT WHEEL PROVIDED WITH THERMAL SCREENS
RAD EINES LUFTFAHRZEUGS, DAS MIT THERMISCHEN ABSCHIRMUNGEN AUSGESTATTET IST
14.02.2024
Patent
Elektronische Ressource
Französisch
IPC: | B64C AEROPLANES , Flugzeuge |