Patent ID: 7100655
Filing Date: 2006-09-05
Classification: B60C,Y10T

Abstract:
1. A pneumatic tire for use on aircrafts having a nominal bead diameter N BD , a tread, a crown reinforcement, and a radial carcass reinforcement comprising at least one axially inner ply of textile cord wound around a pair of bead cores, the bead cores have a radial height B h ,the at least one axially inner ply being wound around the bead core in each bead from inside to the outside forming outside turn-ups and at least one axially outer ply of textile cords extending from bead to bead along the turn-ups of the inner plies, each bead having an elastomeric filler of substantially triangular shape, the apex A of the filler being located above the bead core extending a distance D as measured from a line YY′ parallel to the axis of the tire and through the location of the nominal bead diameter, and a flipper wound around the bead core to form an axially inner leg and an axially outer leg, the axially inner leg being located at a radial distance L i from the reference line YY′, and the axially outer leg being located a radial distance L E from the reference line YY′, wherein L i >B H and LE<.7D; the tire further including; a plurality of rubber components including ply rubber, elastomeric filler rubber, an elastomeric strip rubber, and a sidewall rubber, wherein the rubber modulus (M300) of the apex is greater than or equal to the ply rubber modulus, and the ply rubber modulus is greater than or equal to the strip rubber modulus, and the strip rubber modulus is greater than the sidewall rubber modulus.