The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jul. 22, 2003

Filed:

Mar. 04, 2002
Applicant:
Inventors:

Cyrille Roget, Clermont-Ferrand, FR;

Fernando Suarez, Menetrol, FR;

Assignee:

Michelin Recherche et Technique S.A., Granges-Paccot Switzerland, CH;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B60C 1/500 ;
U.S. Cl.
CPC ...
B60C 1/500 ;
Abstract

An aircraft tire, inflated to a high pressure, comprising a tread connected to two beads by way of two sidewalls each bead having at least one annular reinforcing element a crown reinforcement and a radial carcass reinforcement comprising a number of axially inner plies A to D greater than or equal to two, which radial carcass reinforcement plies have textile reinforcing elements. Among the axially inner plies A to D, at least half the total number of axially inner plies C, D are turned up in each bead about at least one annular reinforcing element at least one and at most three of the remaining axially inner plies A, B being not turned up in any of the beads and having ends situated radially below a straight line XX′ parallel to the axis of rotation of the tire and passing through the radially innermost point of the cross-section of the annular reinforcing element and axially inside a straight line YY′, perpendicular to the axis of rotation and passing through the center of gravity O of the cross section of the annular reinforcing element


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