Granted Patent B2

US 12,583,258 · App. 18/283,527 · Granted Mar 24, 2026

Inventors: Mathieu Vandaele (Clermont-Ferrand, FR); Mathieu Girard (Clermont-Ferrand, FR); Matthieu Bonnamour (Clermont-Ferrand, FR); Stephane Callamand (Clermont-Ferrand, FR); Alexandre Laval (Clermont-Ferrand, FR); David Hernandez (Clermont-Ferrand, FR); Julien Falempin (Clermont-Ferrand, FR); Antoine Filiol (Clermont-Ferrand, FR)

Assignee: COMPAGNIE GENERALE DES ETABLISSEMENTS MICHELIN

B60C9/18B60C9/08B60C2017/0081B60C19/00B60C2200/04

Abstract

Claims (95)

1 . A tire comprising:

a crown comprising a crown reinforcement;

a first sidewall and a second sidewall, which each extend the crown radially inward and which are respectively arranged on a first side and a second side of a median plane of the tire;

a first bead and a second bead, which each extend the first sidewall and the second sidewall radially inward respectively and which are respectively arranged on the first side and the second side of the median plane;

an internal surface delimiting a toroidal cavity for inflating the tire;

a carcass reinforcement, which is anchored in each of the first and second beads and which extends in each of the first and second sidewalls and in the crown, the carcass reinforcement being radially inside the crown reinforcement in the crown; and

a stiffening structure comprising:

one or more stiffening elements, the or each stiffening element extending continuously in the toroidal cavity from the first sidewall or the first bead as far as the second sidewall or the second bead via the crown,

at least one radially outer reinforcing structure that is:

arranged in the crown,

distinct from the carcass reinforcement, from the crown reinforcement, and from the or each stiffening element, and

buried in a crown material mass of the crown, which physically separates the at least one radially outer reinforcing structure from the crown reinforcement and from the carcass reinforcement,

a first radially inner reinforcing structure that is:

arranged in the first sidewall or the first bead,

distinct from the carcass reinforcement and from the or each stiffening element, and

buried in a first material mass of the first sidewall or the first bead, which physically separates the first radially inner reinforcing structure from the carcass reinforcement, and

a second radially inner reinforcing structure that is:

arranged in the second sidewall or the second bead,

distinct from the carcass reinforcement and from the or each stiffening element, and

buried in a second material mass of the second sidewall or the second bead, which physically separates the second radially inner reinforcing structure from the carcass reinforcement,

wherein the or each stiffening element:

passes through the internal surface at a first radially inner anchor point of the first sidewall or the first bead to extend from said first radially inner anchor point deep into said first material mass so as to be anchored beneath the internal surface in or around the first radially inner reinforcing structure and to be physically separated by said first material mass from the carcass reinforcement,

passes through the internal surface at a first radially outer anchor point of the crown to extend from said first radially outer anchor point deep into said crown material mass so as to be anchored beneath the internal surface in or around the at least one radially outer reinforcing structure and to be physically separated by said crown material mass from the carcass reinforcement and the crown reinforcement,

comprises a first portion extending in the toroidal cavity between the first radially inner anchor point and the first radially outer anchor point,

passes through the internal surface at a second radially inner anchor point of the second sidewall or the second bead to extend from said second radially inner anchor point deep into said second material mass so as to be anchored beneath the internal surface in or around the second radially inner reinforcing structure and to be physically separated by said second material mass from the carcass reinforcement,

passes through the internal surface at a second radially outer anchor point of the crown to extend from said second radially outer anchor point deep into said crown material mass so as to be anchored beneath the internal surface in or around the at least one radially outer reinforcing structure and to be physically separated by said crown material mass from the carcass reinforcement and the crown reinforcement, and

comprises a second portion extending in the toroidal cavity between the second radially inner anchor point and the second radially outer anchor point,

wherein the first radially outer anchor point and the first radially inner anchor point for the or each stiffening element are arranged on the first side of the median plane,

wherein the second radially outer anchor point and the second radially inner anchor point for the or each stiffening element are arranged on the second side of the median plane, and

wherein the first portion and the second portion of the or each stiffening element do not cross over in the toroidal cavity.

2 . The tire according to claim 1 , wherein the one or more stiffening elements form a continuous stiffening element so as to trace out a boustrophedon path through the crown between the first sidewall or the first bead and the second sidewall or the second bead.

3 . The tire according to claim 1 , wherein the stiffening structure comprises a plurality of stiffening elements distributed circumferentially in the toroidal cavity.

4 . The tire according to claim 1 , wherein each of the first radially inner anchor point and the second radially inner anchor point is arranged radially at a radial distance from 0.10×H to 0.50×H from a radially innermost point of the tire, H being a section height of the tire.

5 . The tire according to claim 1 , wherein each of the first radially outer anchor point and the second radially outer anchor point is arranged axially at an axial distance at most equal to 0.45×SW from the median plane, SW being a nominal section width of the tire.

6 . The tire according to claim 1 , wherein the or each stiffening element is a filar stiffening element.

7 . The tire according to claim 1 , wherein the at least one radially outer reinforcing structure includes:

a first radially outer reinforcing structure that is:

arranged in the crown,

distinct from the carcass reinforcement, from the crown reinforcement and from the or each stiffening element, and

buried in a first crown material mass of the crown, which physically separates the first radially outer reinforcing structure from the crown reinforcement and from the carcass reinforcement, and

a second radially outer reinforcing structure that is:

arranged in the crown,

distinct from the carcass reinforcement, from the crown reinforcement, from the or each stiffening element, and from the first radially outer reinforcing structure, and

buried in a second crown material mass of the crown, which physically separates the second radially outer reinforcing structure from the crown reinforcement and from the carcass reinforcement, and

wherein the or each stiffening element:

passes through the internal surface at the first radially outer anchor point to extend from said first radially outer anchor point deep into said first crown material mass so as to be anchored beneath the internal surface in or around the first radially outer reinforcing structure, and

passes through the internal surface at the second radially outer anchor point to extend from said second radially outer anchor point deep into said second crown material mass so as to be anchored beneath the internal surface in or around the second radially outer reinforcing structure.

8 . The tire according to claim 7 , wherein the first radially outer reinforcing structure and the second radially outer reinforcing structure are respectively arranged on the first side and the second side of the median plane.

9 . The tire according to claim 1 , wherein each of the first radially inner reinforcing structure, the second radially inner reinforcing structure, and the at least one radially outer reinforcing structure comprises at least one filar reinforcing element extending in a main direction forming with a circumferential direction of the tire an angle less than or equal to 10°.

10 . The tire according to claim 9 , wherein the tire has a substantially toroidal shape around an axis of revolution, and

wherein the at least one filar reinforcing element of each of the first radially inner reinforcing structure and the second radially inner reinforcing structure is wound circumferentially over at most two complete turns around the axis of revolution.

11 . The tire according to claim 9 , wherein the tire has a substantially toroidal shape around an axis of revolution, and

wherein the at least one filar reinforcing element of the at least one radially outer reinforcing structure is wound circumferentially over at least two complete turns around the axis of revolution and at most ten complete turns around the axis of revolution.

12 . The tire according to claim 9 , wherein the or each stiffening element is wound at least in part around the at least one filar reinforcing element.

13 . A tire comprising:

a crown comprising a crown reinforcement;

a first sidewall and a second sidewall, which each extend the crown radially inward and which are respectively arranged on a first side and a second side of a median plane of the tire;

a first bead and a second bead, which each extend the first sidewall and the second sidewall radially inward respectively and which are respectively arranged on the first side and the second side of the median plane;

an internal surface delimiting a toroidal cavity for inflating the tire;

a carcass reinforcement, which is anchored in each of the first and second beads and which extends in each of the first and second sidewalls and in the crown, the carcass reinforcement being radially inside the crown reinforcement in the crown; and

a stiffening structure comprising:

one or more first stiffening elements, the or each first stiffening element extending continuously in the toroidal cavity from the first sidewall or the first bead as far as the crown, and one or more second stiffening elements, the or each second stiffening element extending continuously in the toroidal cavity from the second sidewall or the second bead as far as the crown,

at least one radially outer reinforcing structure that is:

arranged in the crown,

distinct from the carcass reinforcement, from the crown reinforcement, and from the or each first stiffening element and the or each second stiffening element, and

buried in a crown material mass of the crown, which physically separates the at least one radially outer reinforcing structure from the crown reinforcement and from the carcass reinforcement,

a first radially inner reinforcing structure that is:

arranged in the first sidewall or the first bead,

distinct from the carcass reinforcement and from the or each first stiffening element and the or each second stiffening element, and

buried in a first material mass of the first sidewall or the first bead, which physically separates the first radially inner reinforcing structure from the carcass reinforcement, and

a second radially inner reinforcing structure that is:

arranged in the second sidewall or the second bead,

distinct from the carcass reinforcement and from the or each first stiffening element and the or each second stiffening element, and

buried in a second material mass of the second sidewall or the second bead, which physically separates the second radially inner reinforcing structure from the carcass reinforcement,

wherein the or each first stiffening element:

passes through the internal surface at a first radially inner anchor point of the first sidewall or the first bead to extend from said first radially inner anchor point deep into said first material mass so as to be anchored beneath the internal surface in or around the first radially inner reinforcing structure and to be physically separated by said first material mass from the carcass reinforcement,

passes through the internal surface at a first radially outer anchor point of the crown to extend from said first radially outer anchor point deep into said crown material mass so as to be anchored beneath the internal surface in or around the at least one radially outer reinforcing structure and to be physically separated by said crown material mass from the carcass reinforcement and the crown reinforcement, and

comprises a portion extending in the toroidal cavity between the first radially inner anchor point and the first radially outer anchor point,

wherein the or each second stiffening element:

passes through the internal surface at a second radially inner anchor point of the second sidewall or the second bead to extend from said second radially inner anchor point deep into said second material mass so as to be anchored beneath the internal surface in or around the second radially inner reinforcing structure and to be physically separated by said second material mass from the carcass reinforcement,

passes through the internal surface at a second radially outer anchor point of the crown to extend from said second radially outer anchor point deep into said crown material mass so as to be anchored beneath the internal surface in or around the at least one radially outer reinforcing structure and to be physically separated by said crown material mass from the carcass reinforcement and the crown reinforcement, and

comprises a portion extending in the toroidal cavity between the second radially inner anchor point and the second radially outer anchor point,

wherein the first radially outer anchor point and the first radially inner anchor point for the or each first stiffening element are arranged on the first side of the median plane,

wherein the second radially outer anchor point and the second radially inner anchor point for the or each second stiffening element are arranged on the second side of the median plane, and

wherein said portion of the or each first stiffening element and said portion of the or each second stiffening element do not cross over in the toroidal cavity.

14 . The tire according to claim 13 , wherein the stiffening structure comprises a plurality of first stiffening elements distributed circumferentially in the toroidal cavity and a plurality of second stiffening elements distributed circumferentially in the toroidal cavity.

15 . The tire according to claim 13 , wherein each of the first radially inner anchor point and the second radially inner anchor point is arranged radially at a radial distance from 0.10×H to 0.50×H from a radially innermost point of the tire, H being a section height of the tire.

16 . The tire according to claim 13 , wherein each of the first radially outer anchor point and the second radially outer anchor point is arranged axially at an axial distance at most equal to 0.45×SW from the median plane, SW being a nominal section width of the tire.

17 . The tire according to claim 13 , wherein the or each first stiffening element is a filar stiffening element, and wherein the or each second stiffening element is a filar stiffening element.

18 . The tire according to claim 13 , wherein each of the first radially inner reinforcing structure, the second radially inner reinforcing structure, and the at least one radially outer reinforcing structure comprises at least one filar reinforcing element extending in a main direction forming with a circumferential direction of the tire an angle less than or equal to 10°.

19 . The tire according to claim 18 , wherein the tire has a substantially toroidal shape around an axis of revolution, and

wherein the at least one filar reinforcing element of each of the first radially inner reinforcing structure and the second radially inner reinforcing structure is wound circumferentially over at most two complete turns around the axis of revolution.

20 . The tire according to claim 18 , wherein the tire has a substantially toroidal shape around an axis of revolution, and

wherein the at least one filar reinforcing element of the at least one radially outer reinforcing structure is wound circumferentially over at least two complete turns around the axis of revolution and at most ten complete turns around the axis of revolution.

21 . The tire according to claim 18 , wherein the or each first stiffening element and the or each second stiffening element are wound at least in part around the at least one filar reinforcing element.

Assignments (1)

Priority Claims (1)

Continuity (1)

References Cited (35)