Tire for an aeroplane and, in particular, the crown thereof which comprises a tread (1), a working reinforcement (2), a carcass reinforcement (3) and a hoop reinforcement (4). The radially internal working layer (21) of the working reinforcement (2) comprises a concave portion. The hoop reinforcement (41) comprises at least one hooping layer (41) radially on the inside of the working layer (21) and made up of mutually parallel reinforcing elements, having a mean diameter D, that are inclined, with respect to the circumferential direction (XX′), at an angle of between +10° and −10°. The hooping layer (41) comprises at least one axial discontinuity (411) having an axial width (L411) at least equal to three times the mean diameter D of the reinforcing elements of the hooping layer (41).
ARMATURE DE SOMMET DE PNEUMATIQUE POUR AVION
CROWN REINFORCEMENT FOR AN AIRCRAFT TYRE
GÜRTELVERSTÄRKUNG FÜR EINEN FLUGZEUGREIFEN
2018-09-12
Patent
Electronic Resource
French
IPC: | B60C VEHICLE TYRES , Fahrzeugreifen |