BEAD CORE FOR AGRICULTURAL TIRE

Abstract

A bead core for a tire, which is substantially rotationally symmetrical about an axis, comprises a plurality of windings of at least one metallic wire with diameter d arranged next to one another in a direction P forming an angle α with the axial direction in a radial sectional half-plane R, on N layers superposed on one another in the radial direction, wherein: α ranges from 0° to 10°; in the sectional half-plane R, the windings form a structure consisting of a base structure and a cap structure, wherein the radially inner base structure in the shape of a parallelogram is directly in contact in the radial direction with the radially outer cap structure in the shape of a trapezium. The product of the diameter d times the number of windings L ranges from 13.0 mm to 25.0 mm, and N is less than or equal to 16.

Claims

1.-14. (canceled)

15. A bead core for a tire which is substantially rotationally symmetrical about an axis, the bead core comprising a plurality of windings of at least one metallic wire with diameter d arranged next to one another in a direction P forming an angle α with an axial direction in a radial sectional half-plane R, on N layers superposed on one another in a radial direction, wherein α ranges from 0° to 10°, wherein, in the sectional half-plane R, the windings of the bead core form a structure consisting of a base structure and a cap structure, where a radially inner base structure in the shape of a parallelogram is directly in contact in the radial direction with a radially outer cap structure in the shape of a trapezium, wherein the base structure of I layers Ci superposed on one another in the radial direction, wherein I is odd and I≥3, comprises: the radially innermost layer C.sub.1 and the radially outermost layer C.sub.I comprising L windings, wherein i is an integral number ranging from 1 to I−2, L.sub.i=L.sub.i+2 and |L.sub.i−L.sub.i+1=1, wherein L.sub.i is the number of windings of the layer Ci and Max(L.sub.i)=L with: when i is odd, each axially outermost winding of the layers Ci is arranged in contact with a first outer side, which is a straight line parallel to the radial direction and tangent to the axially outermost winding of the layer C.sub.1 in the radial sectional half-plane R, and when i is even, the axially outermost winding of the layers Ci is arranged in contact with the two axially outermost windings of the immediately lower layer, wherein the cap structure of J layers Cj superposed on one another in the radial direction comprises: the layer C.sub.I+1 of L−1 windings superposed on layer C.sub.I of the base structure in the radial direction and the axially outermost winding being in contact with the two axially outermost windings of the immediately lower layer, and or when j is an integral number between 1 and J, the layer C.sub.I+j is such that: when j is even, L.sub.I+j=L.sub.I+(j−1), when j is odd, L.sub.I+j=L−(j+1)/2, such that when j is odd, the layer C.sub.I+j is formed from L.sub.I+j windings and the axially outermost winding is arranged in contact with the two axially outermost windings of the immediately lower layer, and when j is even, the layer C.sub.I+j comprises L.sub.I+j windings arranged next to one another in the direction P from the first outer side, or when j ranges from 1 to J, the layer C.sub.I+j is such that: L.sub.I+j=L−j so as to form an isosceles trapezium, wherein a product of the diameter d times L ranges from 13.0 mm to 25.0 mm, and wherein N, I and J are integral numbers not equal to zero, such that N=I+J is less than or equal to 16.

16. The bead core according to claim 15, wherein the product of the diameter d times L is less than or equal to 24.5 mm.

17. The bead core according to claim 15, wherein the product of the diameter d times L is greater than or equal to 14.5 mm.

18. The bead core according to claim 15, wherein the angle α is less than or equal to 8°.

19. The bead core according to claim 15, wherein the angle α is greater than or equal to 30.

20. The bead core according to claim 15, wherein the diameter d ranges from 0.95 mm to 3.00 mm.

21. The bead core according to claim 15, wherein max(L.sub.k)=max(L.sub.i)=L is strictly greater than N, with C.sub.k being a layer of the bead core selected from N layers, and L.sub.k is the number of windings of each layer C.sub.k, k being an integral number between 1 and N.

22. The bead core according to claim 15, wherein N ranges from 7 to 16.

23. The bead core according to claim 15, wherein 1 ranges from 5 to 13.

24. The bead core according to claim 15, wherein J ranges from 2 to 3.

25. A method for manufacture of a bead core for a tire which is substantially rotationally symmetrical about an axis, the bead core comprising a plurality of windings of at least one wire with diameter d arranged next to one another in a direction P forming an angle α with an axial direction in a radial sectional half-plane R, on N layers superposed on one another in a radial direction, the method comprising: placing a winding in contact with a laying surface of a channel at a radially inner end and unwinding the winding toward a first outer side, which is a straight line parallel to the radial direction and tangent to an outermost winding of the layer, in order to form the layer C.sub.1 such that a product of the diameter d times L is strictly less than 25.0 mm; superposing I layers Ci on one another in the radial direction, wherein I is odd and I≥3, so as to form a base structure in the form of a parallelogram in the sectional half-plane R such that the radially innermost layer C.sub.1 and the radially outermost layer C.sub.I comprise L windings, wherein i is an integral number ranging from 1 to I−2, L.sub.i=L.sub.i+2 and |L.sub.i−L.sub.i+1|=1, wherein L.sub.i is the number of windings of the layer Ci and Max(L.sub.i)=L with: when i is odd, each axially outermost winding of the layers Ci is arranged in contact with the first outer side, which is a straight line parallel to the radial direction and tangent to the axially outermost winding of the layer C.sub.1 in the radial sectional half-plane R, and when i is even, the axially outermost winding of the layers Ci is arranged in contact with the two axially outermost windings of the immediately lower layer; and superposing J layers Cj on one another in the radial direction so as to form a cap structure in the sectional half-plane R such that: the layer C.sub.I+1 of L−1 windings superposed on layer C.sub.I of the base structure in the radial direction, and or when j is an integral number between 1 and J, the layer C.sub.I+j is such that: when j is even, L.sub.I+j=L.sub.1+(j−1), when j is odd, L.sub.I+j=L−(j+1)/2, such that when j is odd, the layer C.sub.I+j is formed from L.sub.I+j windings and the axially outermost winding is arranged in contact with the two axially outermost windings of the immediately lower layer, and when j is even, the layer C.sub.I+j comprises L.sub.I+j windings arranged next to one another in the direction P from the first outer side, or when j ranges from 1 to J, the layer C.sub.I+j is such that: L.sub.I+j=L−j so as to form an isosceles trapezium, wherein N, I and J are integral numbers not equal to zero, such that N=I+J is less than or equal to 16.

26. The method according to claim 25, wherein the bead core is covered with at least one fabric comprising filamentary elements comprising at least one multifilament strand comprising several monofilaments, each made up of a material selected from the group consisting of a polyester, a polyamide, a polyketone, a polyurethane, a natural fiber, a mineral fiber, and an assembly of these materials.

27. A tire for an agricultural or forestry vehicle comprising: at least one bead comprising a bead core according to claim 15; and a carcass reinforcement comprising at least one carcass ply anchored in each bead by a return around the bead core.

28. The tire according to claim 27, wherein the carcass reinforcement consists of a single carcass ply anchored in each bead by a return around the bead core.

Description

[0091] The invention will be understood better on reading the following description of the figures, which is given purely by way of non-limiting example and with reference to the drawings, in which:

[0092] FIG. 1 is a radial sectional view of a tyre according to the invention;

[0093] FIG. 2 is a detailed sectional view of the zone T of the tyre of FIG. 1;

[0094] FIG. 3 is an illustration of the rotation of the bead core of the prior art around the carcass ply after the step of curing of the tyre;

[0095] FIG. 4 is an illustration of the phenomenon of soft bead;

[0096] FIGS. 5 and 6 are two schematic illustrations of the conventional packing rubber and the packing rubber with extended range;

[0097] FIG. 7 is a sectional view of a bead core 52_A according to a first variant of the first embodiment of the invention;

[0098] FIG. 8 is a sectional view of a bead core 52_S according to a second variant of the first embodiment of the invention;

[0099] FIG. 9 is a view similar to that of FIG. 7 of a bead core 52-5_A according to a first variant of the sixth embodiment of the invention;

[0100] FIGS. 10 to 14 are views similar to that of FIG. 8 of bead cores 52-1_S, 52-2_S, 52-3_S, 52-4_S and 52-5_S respectively according to a second variant of the second, third, fourth, fifth and sixth embodiments;

[0101] FIGS. 15 to 18 are sectional views illustrating various steps in the method of manufacturing the tyre according to the invention; and

[0102] FIG. 19 is an illustration of the channel used during the method of manufacturing the bead core according to the invention.

[0103] The tyre according to the invention has a generally toroidal form about an axis of rotation. This axis of rotation defines the axial direction.

[0104] When using the term “radial”, a distinction should be made between several different uses of the word by the person skilled in the art when speaking of a tyre.

[0105] Firstly, the expression refers to a radius of the tyre. It is in that sense that an element A is said to be “radially inside” an element B (or “radially on the inside of” the element B) if it is closer to the axis of rotation of the tyre than is the element B. Conversely, an element C is said to be “radially outside” an element D (or “radially on the outside of” the element D) if it is further from the axis of rotation of the tyre than is the element D. Progress “radially inwards (or outwards)” will mean progress towards smaller (or larger) radii.

[0106] Secondly, a reinforcing element or a reinforcement is said to be “radial” when the reinforcing element or the reinforcing elements of the reinforcement make an angle greater than or equal to 65° and less than or equal to 90° with the circumferential direction.

[0107] Thirdly, a “radial cross-section” or “radial section” here means a cross-section or a section in a plane which contains the axis of rotation of the tyre.

[0108] An “axial” direction is a direction parallel to the axis of rotation of the tyre. An element E is said to be “axially inside” an element F (or “axially on the inside of” the element F) if it is closer to the median plane of the tyre than is the element F. Conversely, an element G is said to be “axially outside” an element H (or “axially on the outside of” the element H) if it is further from the median plane of the tyre than is the element H.

[0109] The “median plane” of the tyre is the plane which is perpendicular to the axis of rotation of the tyre and which lies at equal distances from the annular reinforcing structures of each bead.

[0110] A “circumferential” direction is a direction that is perpendicular both to a radius of the tyre and to the axial direction.

[0111] Example of a Tyre and Bead Core According to the Invention

[0112] Tyre 10 According to the Invention

[0113] FIGS. 1 and 2 show directions X, Y, Z corresponding to the usual axial (X), radial (Y) and circumferential (Z) directions of a tyre.

[0114] FIGS. 1 and 2 show an exemplary tyre according to the invention and denoted by the general reference 10. The tyre 10 is preferably intended for an industrial vehicle selected from agricultural or forestry vehicles. In this case, the tyre 10 is intended for an agricultural vehicle, for example a tractor.

[0115] The tyre 10 has a nominal rim diameter as defined by ETRTO (European Tyre and Rim Technical Organisation) ranging from 24 to 54 inches (60.96 cm to 137.16 cm). The tyre 10 has a nominal aspect ratio is defined by ETRTO ranging from 0.7 to 0.9.

[0116] The tyre 10 has a crown 12 comprising a crown reinforcement 14 comprising one or more crown plies 16 of reinforcing elements. The crown reinforcement 14 is surmounted by a tread 18. The crown reinforcement 14 is arranged radially inside the tread 18. Two sidewalls 20 extend the crown 12 radially inwards. The tyre 10 has two beads 22 radially inside the sidewalls 20, each comprising an annular reinforcing structure 24.

[0117] The tyre 10 also has a radial carcass reinforcement 26. The carcass reinforcement 26 extends from the beads 22 through the sidewalls 20 towards the crown 12. The carcass reinforcement 26 comprises one or more carcass plies 28, wherein at least one of these carcass plies 28 is anchored in each of the beads 22 by a return 30 around the annular reinforcing structure 24, so as to form, in each bead 22, an outgoing strand 32 extending radially between each bead 22 through the sidewalls 20 and the crown 12, and an incoming strand 34 extending radially from each bead 22 through each sidewall 20, the radially outer end 36 of the return strand 34 being situated radially outside the annular reinforcement structure 24 and axially outside the outgoing strand 32.

[0118] The tyre 10 also comprises an inner sealing liner 38 arranged radially and axially inside the carcass reinforcement 26. The inner liner 38 extends between each bead 22, passing through the sidewalls 20 and the crown 12.

[0119] Each bead 22 comprises, in addition to the annular reinforcing structure 24, a mass 40 of packing rubber arranged in a space delimited by the outgoing strand 32 and incoming strand 34. Each bead 22 also comprises a first mass 42 of rubber protecting the bead 22 following the return 30 of the carcass reinforcement 26.

[0120] Furthermore, each bead 22 also comprises a mass 44 of packing rubber arranged axially outside the carcass reinforcement 26, in particular axially outside the incoming strand 34. Each sidewall 20 comprises an axially outer mass 46 of rubber delimiting an axially outer surface 48 of the sidewall 20 and arranged axially outside the mass 44 of packing rubber. Finally, each bead 22 comprises a second mass 50 for protection of the bead 22, arranged axially between the packing rubber 44 and the axially outer mass 46 of rubber of the sidewall 20.

[0121] Each annular reinforcing structure 24 comprises an annular bead core 52_A coated with a coating mass 54, for example comprising rubber. The bead core 52_A is arranged radially inside the packing rubber 40. The bead core 52_A complies with the first variant of the first embodiment of the invention.

[0122] Bead Core 52_A According to a First Variant of the First Embodiment of the Invention

[0123] FIG. 7 shows the bead core 52_A according to a first variant of the first embodiment of the invention.

[0124] The bead core 52_A has a generally symmetrical form in rotation about the axis of revolution of the tyre 10 which is substantially parallel to the axial direction X.

[0125] The bead core 52_A comprises n windings of at least one wire of diameter d arranged in a radial sectional half-plane R in a direction P forming an angle α with the axial direction, next to one another over N layers C.sub.k superposed on the layer C.sub.i+1 in the radial sectional half-plane R. The bead core 52_A is obtained by successive superpositions of N layers C.sub.k, with k varying from 1 to N inclusive, each layer C.sub.k being obtained by successive axial windings of at least one wire. The total number of windings n of the bead core 52_A is greater than or equal to 30, preferably to 50 and more preferably to 70, here n=74.

[0126] In a first variant of the first embodiment shown in FIG. 6, the bead core 52_A comprises n windings of a single wire. Preferably, the wire is metallic, has a substantially circular cross-section, and advantageously a diameter between 0.95 mm and 3.00 mm, preferably between 1.20 mm and 2.20 mm, and more preferably between 1.25 mm and 2.05 mm, here a diameter equal to 1.55 mm. The wire is made of a carbon steel comprising 0.7% carbon by mass. The metallic wire is first coated with a polymer compound with thickness ranging from 0.05 mm to 0.3 mm, advantageously between 0.1 and 0.2 mm. Here, the thickness is 0.15 mm.

[0127] Table 1 below shows the number of windings L.sub.k of each layer C.sub.k. The maximum number of windings max(L.sub.k) of the N layers C.sub.k is such that max(L.sub.k)=max(L.sub.i)=L is strictly greater than N. Here max (L.sub.k)=N+2.

TABLE-US-00001 TABLE 1 Layer number Number of windings L.sub.k C1 10 C2 9 C3 10 C4 9 C5 10 C6 9 C7 9 C8 8

[0128] The bead core 52_A comprises at least one layer C.sub.k with kϵ]1, N [such that L.sub.k+1>L.sub.k and L.sub.k<L.sub.k−1, here L.sub.3>L.sub.2 and L.sub.2<L.sub.1

[0129] The bead core in the sectional half-plane R is composed of a radially inner base structure in the form of a parallelogram, here represented by layers C1 to C5, which is in direct contact in the radial direction with a radially outer cap structure in the form of a trapezium, here represented by layers C6, C7 and C8.

[0130] For the cap structure, the number of windings of layer C.sub.6 is L.sub.6=L−1=10−1=9 which are arranged one next to the other in the direction P from the first outer side, and the layer C.sub.7 has the same number of windings as the layer C.sub.6, or L.sub.7=9 windings, which are arranged one next to the other in the direction P from the first inner side. Finally, the last layer C.sub.8 is such that L.sub.8=L−(3+1)/2=10−2=8 so as to form a trapezium.

[0131] N is an integral number not equal to zero, less than or equal to 16, and ranges from 7 to 16. Here N=I+J=8.

[0132] I ranges from 5 to 13. Here I=5.

[0133] J ranges from 2 to 3. Here J=3.

[0134] L=10.

[0135] The product of the diameter d times L is firstly strictly greater than 14.0 mm, preferably greater than or equal to 14.5 mm, and more preferably greater than or equal to 15.0 mm, and secondly less than or equal to 25.0 mm, preferably less than or equal to 24.5 mm, and more preferably less than or equal to 24.4 mm. Here d×L=1.55×10=15.50 mm.

[0136] The angle α ranges from 0° to 10°, is preferably less than or equal to 6°, and greater than or equal to 4°. Here, α is equal to 5°.

[0137] The angle α+90°=95°.

[0138] The bead core comprises a layer C.sub.1 and C.sub.1=C.sub.5 of L=10 windings.

[0139] Example of a Method for Manufacturing a Tyre and Bead Core According to the Invention

[0140] Method for Manufacturing the Tyre 10

[0141] We will now describe a method for manufacturing a tyre 10 according to the invention with reference to FIGS. 15 to 18.

[0142] Firstly, in a first assembly phase, the various plies, rubber masses and other elements described above are assembled in order to form an initial preform on an assembly drum, as known to the person skilled in the art.

[0143] Then, successively and in this order, the first mass 42 of protection rubber is laid, followed by the inner sealing layer 38, one or more carcass plies 28 intended to be anchored in the beads 22, the packing rubber 40, and the annular reinforcing structure 24 comprising the bead core 52_A and the coating mass 54. The bead core 52_A has thus been laid on the carcass ply or plies 28. This gives the intermediate preform shown in FIG. 15.

[0144] Then the first mass 42 of protection rubber, and a part of the carcass ply or plies 28, here the incoming strand 34, are folded around the annular reinforcing structure 24. This gives the intermediate preform shown in FIG. 16.

[0145] Then, successively and in this order, the packing rubber 44 is applied, followed by the second protection mass 50 and finally the axially outer mass 46 of rubber delimiting the axially outer surface 48 of the sidewall 20. This gives the intermediate preform shown in FIG. 17.

[0146] Then the carcass ply or plies 28 and the bead core 52_A are turned relative to one another. In this case, the assembly of the intermediate preform, with the exception of the annular reinforcing structure 24, is turned around the latter which remains substantially fixed during the rotation. This gives the intermediate preform shown in FIG. 18. It will be noted that after the rotation, the bead core 52_A has the same orientation as before the rotation, and that the various plies and rubber masses have not been deformed under the effect of the rotation.

[0147] In a second, subsequent finishing phase, the crown 12 and the tread 18 are added to the intermediate preform previously obtained.

[0148] In a third curing phase, the finished preform is cured so as to produce the cured tyre.

[0149] Process for the Manufacture of the Bead Core 52_A

[0150] We will now describe a method for manufacturing a bead core 52_A according to the invention with reference to FIG. 19.

[0151] The wire of diameter d=1.55 mm, previously coated with an elastomer compound, is brought into contact with a laying surface of a channel in the radial section plane in the direction P forming an angle α with the axial direction, α=5°, and the wire is wound from a channel at the radially inner end, and the wire is wound by L=10 windings towards the first outer side in order to form a radially inner layer C.sub.1, such that the product of the diameter d times L is strictly less than 25.0 mm, here d×L=15.5 mm, and strictly greater than 14.0 mm, and N, I and J are integral numbers not equal to zero, such that N=I+J is less and or equal to 16, N=8=5+3.

[0152] I layers Ci are superposed on one another in the radial direction, wherein I is odd and I≥3, here I=5, so as to form the base structure in the form of the parallelogram in the sectional half-plane R such that: [0153] the radially innermost layer C.sub.1 and the radially outermost layer C.sub.5 comprise L windings; [0154] wherein i is an integral number ranging from 1 to I−2=3, L.sub.i=L.sub.i+2 and |L.sub.i−L.sub.i+1|=1, wherein Li is the number of windings of the layer C.sub.i and Max(L.sub.i)=L with: [0155] when i is odd, each axially innermost winding of the layers Ci is arranged in contact with the first inner side which is the straight line parallel to the radial direction and tangent to the axially innermost winding of the layer C.sub.1 in the radial sectional half-plane R. Here, I=5 and the layers C.sub.i are layers C.sub.1 to C.sub.5, L.sub.1=L.sub.3=L.sub.5=10 windings and L.sub.2=L.sub.4=9 windings.

[0156] J=3 layers Ci are superposed on one another in the radial direction so as to form a cap structure in the sectional half-plane R.

[0157] Layer C.sub.I+j is such that: when j is even, L.sub.I+j=L.sub.I+(j−1) and when j is odd, L.sub.I+j=L−(j+1)/2 such that when j is odd, the layer C.sub.I+j is formed from L.sub.I+j windings and the axially outermost winding is arranged in contact with the two axially outermost windings of the immediately lower layer; and when j is even, the layer C.sub.I+j is formed from L.sub.I+j windings arranged next to one another in the direction P from the first outer side. Here, the layer in contact with the layer C.sub.6 is the layer C.sub.7 which has L.sub.6=L.sub.7=9 windings, and the layer C.sub.8 has L.sub.8=10−(3+1)/2=8 windings.

[0158] The bead core 52_A is covered with at least one fabric comprising filamentary elements comprising at least one multifilament strand comprising several monofilaments, each made up of a material selected from a polyester, a polyamide, a polyketone, a polyurethane, a natural fibre, a mineral fibre, preferably selected from a polyester, an aromatic or aliphatic polyamide, a polyketone, a polyurethane, a natural fibre and an assembly of these materials, more preferably selected from an aliphatic polyamide and an assembly of these materials, here the bead core 52_A is coated with a crossed fabric comprising an assembly of 2 multifilamentary strands comprising several monofilaments, each composed of an aliphatic polyamide material, nylon N94/1.

[0159] The fabric is first bonded with a polymer compound, thus allowing it to be well supported while being laid around the bead core.

[0160] Bead Core 52_S According to a Second Variant of the First Embodiment of the Invention

[0161] FIG. 8 shows a bead core 52_S according to a second variant of the first embodiment of the invention.

[0162] In contrast to the bead core according to the first variant of the first embodiment, the bead core 52_S of the second variant of the first embodiment comprises n=72 windings.

[0163] Table 2 below shows the number of windings L.sub.i of each layer C.sub.k. Here max(L.sub.k)=L=10.

TABLE-US-00002 TABLE 2 Layer number Number of windings L.sub.k C1 10 C2 9 C3 10 C4 9 C5 10 C6 9 C7 8 C8 7

[0164] Here, the bead core according to the sectional half-plane R is composed of a radially inner base structure in the shape of a parallelogram, here represented by layers C1 to C5, which is in direct contact in the radial direction with a radially outer cap structure in the shape of a trapezium, here represented by layers C6, C7 and C8.

[0165] For the cap structure, the number of windings L.sub.I+j of the layer C.sub.I+j is such that L.sub.I+j=L−j so as to form an isosceles trapezium. Here L.sub.6=L−1 and L.sub.7=L−2 and L.sub.8=L−3.

[0166] Other Example of a Bead Core According to a First Variant of the Invention

[0167] FIG. 9 shows a bead core 52-5_A according to a first variant of the sixth embodiment of the invention.

[0168] In contrast to the bead core according to the first variant of the first embodiment, the bead core 52-5_A of the first variant of the sixth embodiment comprises N=12 layers and n=148 windings.

[0169] Table 3 below shows the number of windings L.sub.k of each layer C.sub.k. Here max(L.sub.k)=L=13.

TABLE-US-00003 TABLE 3 Layer number Number of windings L.sub.k C1 13 C2 12 C3 13 C4 12 C5 13 C6 12 C7 13 C8 12 C9 13 C10 12 C11 12 C12 11

[0170] Other Examples of Bead Cores According to the Second Variant of the Invention

[0171] FIGS. 10, 11, 12, 13 and 14 show bead cores according to other embodiments of the invention. In these figures, elements similar to those of FIG. 7 are denoted by identical references.

[0172] FIG. 10 depicts a bead core according to a second embodiment of the invention.

[0173] In contrast to the bead core according to the second variant of the first embodiment, the bead core 52-1_S of the second embodiment comprises N=7 layers and n=51 windings.

[0174] Table 4 below shows the number of windings L.sub.k of each layer C.sub.k. Here max(L.sub.k)=L=8.

TABLE-US-00004 TABLE 4 Layer number Number of windings L.sub.k C1 8 C2 7 C3 8 C4 7 C5 8 C6 7 C7 6

[0175] FIG. 11 depicts a bead core according to a third embodiment of the invention.

[0176] The bead core 52-2_S according to the third embodiment comprises N=7 layers and n=58 windings.

[0177] Table 5 below shows the number of windings L.sub.k of each layer C.sub.k. Here max(L.sub.k)=L=9.

TABLE-US-00005 TABLE 5 Layer number Number of windings L.sub.k C1 9 C2 8 C3 9 C4 8 C5 9 C6 8 C7 7

[0178] FIG. 12 depicts a bead core according to a fourth embodiment of the invention.

[0179] The bead core 52-3_S according to the fourth embodiment comprises N=8 layers and n=88 windings.

[0180] Table 6 below shows the number of windings L.sub.k of each layer C.sub.k. Here max(L.sub.k)=L=12.

TABLE-US-00006 TABLE 6 Layer number Number of windings L.sub.k C1 12 C2 11 C3 12 C4 11 C5 12 C6 11 C7 10 C8 9

[0181] FIG. 13 depicts a bead core according to a fifth embodiment of the invention.

[0182] The bead core 52-4_S according to the fifth embodiment comprises N=12 layers and n=182 windings.

[0183] Table 7 below shows the number of windings L.sub.k of each layer C.sub.k. Here max(L.sub.k)=L=16.

TABLE-US-00007 TABLE 7 Layer number Number of windings L.sub.k C1 16 C2 15 C3 16 C4 15 C5 16 C6 15 C7 16 C8 15 C9 16 C10 15 C11 14 C12 13

[0184] FIG. 14 shows a bead core according to a second variant of the sixth embodiment of the invention.

[0185] The bead core 52-5_S according to the second variant of the sixth embodiment comprises N=12 layers and n=146 windings.

[0186] Table 8 below shows the number of windings L.sub.k of each layer C.sub.k. Here max(L.sub.k)=L=13.

TABLE-US-00008 TABLE 8 Layer number Number of windings L.sub.k C1 13 C2 12 C3 13 C4 12 C5 13 C6 12 C7 13 C8 12 C9 13 C10 12 C11 11 C12 10

[0187] The comparative bead core TPFR-C is a bead core with a square base which is narrower than the bead cores of the first to fifth embodiments. Table 9 below shows the number of windings of each layer of the TPFR-C.

TABLE-US-00009 TABLE 9 Layer number Number of windings L.sub.k C1 9 C2 8 C3 9 C4 8 C5 9 C6 8 C7 7

[0188] Tables 10 and 11 below show the characteristics of the various bead cores of the prior art, TPC and TPFR-H, a comparative bead core TPFR-C, and the bead cores of the first variants of the first and sixth embodiment, and the bead cores the second variants of the first to sixth embodiments. The width La is the projection of the direction perpendicular to the plane P over the axial direction of the bead core, and the height Ha is the distance between the projection of the straight line passing through the radially outermost layer of the bead core parallel to direction P over the first inner side, and the projection of the direction P over the first inner side.

TABLE-US-00010 TABLE 10 Bead core TPC TPFR_H TPFR_C 52_A 52-5_A n (number of 72 44 58 74 148 wires) Diameter of 1.30 1.55 1.55 1.55 1.55 wires (mm) L 9 5 9 10 13 d × L (mm) 11.70 7.75 13.95 15.50 20.15 La (mm) 14.4 9.3 16.7 18.5 24.1 Ha (mm) 12.8 11.5 11.5 13.1 19.5 max L.sub.k 9 8 9 10 13 Number of 8 7 7 8 12 layers N

TABLE-US-00011 TABLE 11 Bead core 52_S 52-1_S 52-2_S 52-3_S 52-4_S 52-5_S n (number 72 51 58 88 182 146 of wires) Diameter 1.55 2.00 1.75 1.30 0.96 1.55 of wires (mm) L 10 8 9 12 16 13 d × L (mm) 15.50 16.00 15.75 15.60 15.36 20.15 La (mm) 18.5 18.2 18.5 19.2 20.2 24.1 Ha (mm) 13.1 14.1 12.7 11.3 13.3 19.5 max L.sub.k 10 8 9 12 16 13 Number of 8 7 7 8 12 12 layers N

[0189] Tests and Comparative Tests

[0190] Performance in Rotation on the Rim

[0191] The performance of each tyre in rotation on the rim was tested. In fact in order for the tyre to be able to transfer all the forces exerted by the engine of the vehicle to the ground, and for the endurance performance of the bottom region of the tyre to be guaranteed, it is preferable that the rotation of the tyre on the rim is as low as possible.

[0192] Therefore the equivalent coefficient of friction for the road is measured, which corresponds to the coefficient of friction from which we begin to see a rotation on the rim of the tyre at low load and at high load.

[0193] At low load, a vehicle is used with two tyres to be tested at a pressure of 0.5 bar. Then on tarmac, a weight of equal mass is then towed, here 2.6 tonnes per tyre.

[0194] At high load, a vehicle is used with two tyres to be tested at a pressure of 1.6 bar. Then on tarmac, a weight of equal mass is then towed, here 6 tonnes per tyre.

[0195] A load cell is placed between the weight to be towed and the vehicle, allowing measurement of the force F expressed in kg exerted by the vehicle on the weight to be towed when the tyre begins to turn relative to the rim. Thus for a force F=500 kg exerted to cause the tyre to turn relative to the rim, the maximum force towed (Fmax) before an unacceptable extent of tyre rotation on the rim is measured. As a function of the force measured, tyres are classed from 1 to 5, wherein 5 indicates a tyre with a high rotation on the rim and 1 indicates a tyre with the lowest rotation on the rim.

[0196] The results of these tests are summarised in table 12 below for a bead core of the prior art TPC, a comparative bead core TPFR=C, and the bead cores of the first variant of the first embodiment with an angle α equal to 0° designated 52_A0 and an angle α equal to 5°, designated 52_A5.

TABLE-US-00012 TABLE 12 Bead core TPC TPFR_C 52_A0 52_A5 angle α 0 0 0 5 Rotation on the rim Low load, P = 0.5 bar 1 2 1 1 High load, P = 1.6 bar 2 2 1 1

[0197] It is considered that classifications 1 and 2 reflect a low rotation on the rim, and hence the corresponding tyres fulfil the required criterion of performance of rotation on the rim. It is noted that the tyres comprising bead cores 52_A0 and 52_A5 according to the invention have a classification of 1 at low load and a classification at 1 at high load, compared with the tyre of the prior art comprising the bead core TPC and the tyre comprising the comparative bead core TPFR_C.

[0198] Thus the tyres according to the invention have a low rotation on the rim, thus proving their response to the problem of disorganisation of the geometry of the bead court during curing.

[0199] Gain in Clamping Pressure and Rotation on the Rim as a Function of Angle α

[0200] The mean clamping pressure of each bead on the seat is measured by sensors which measure pressure from the interior of the rim seat towards the outside in the direction P forming an angle α with the axial direction, i.e. on the rim flange.

[0201] The results of these tests are collated in table 13 below.

TABLE-US-00013 TABLE 13 Bead core TPC TPFR_C 52_A0 52_A5 Gain in clamping pressure −− − + ++

[0202] It is found that tyres comprising the bead cores 52_A0 and 52_A5 according to the invention show an improvement in their performance in clamping pressure relative to the tyre of the prior art comprising the bead core TPC, which has a much smaller contact area with the seat (14.4 mm vs 18.5 mm for bead core 52), and also relative to the tyre comprising the comparative bead core TPFR_C with a much greater contact area with the seat (16.7 mm). Thus the distribution of area of clamping pressure on the rim seat and hence the performance in rotation on the rim under the effect of high torque levels are improved. Also, a good positioning of the pressure maximum in the centre of the rim seat is ensured, and hence the performance in resistance to detachment of the tyre from the rim flange, caused by the lifting of the bead core on the axially outer side of the tyre.

[0203] The invention is not limited to the above-described embodiments.

[0204] The characteristics of the various embodiments described above may be combined insofar as they are mutually compatible.