WO2018172691A1 - Tyre crown reinforcement consisting of a working crown layer and a layer of circumferential elements - Google Patents

Tyre crown reinforcement consisting of a working crown layer and a layer of circumferential elements Download PDF

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Publication number
WO2018172691A1
WO2018172691A1 PCT/FR2018/050673 FR2018050673W WO2018172691A1 WO 2018172691 A1 WO2018172691 A1 WO 2018172691A1 FR 2018050673 W FR2018050673 W FR 2018050673W WO 2018172691 A1 WO2018172691 A1 WO 2018172691A1
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WO
WIPO (PCT)
Prior art keywords
layer
reinforcing elements
tire
working
circumferential
Prior art date
Application number
PCT/FR2018/050673
Other languages
French (fr)
Inventor
Luc Bestgen
Orel FOURNIER
Patrick DAYET
Original Assignee
Compagnie Generale Des Etablissements Michelin
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Compagnie Generale Des Etablissements Michelin filed Critical Compagnie Generale Des Etablissements Michelin
Publication of WO2018172691A1 publication Critical patent/WO2018172691A1/en

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60CVEHICLE TYRES; TYRE INFLATION; TYRE CHANGING; CONNECTING VALVES TO INFLATABLE ELASTIC BODIES IN GENERAL; DEVICES OR ARRANGEMENTS RELATED TO TYRES
    • B60C9/00Reinforcements or ply arrangement of pneumatic tyres
    • B60C9/18Structure or arrangement of belts or breakers, crown-reinforcing or cushioning layers
    • B60C9/20Structure or arrangement of belts or breakers, crown-reinforcing or cushioning layers built-up from rubberised plies each having all cords arranged substantially parallel
    • B60C9/22Structure or arrangement of belts or breakers, crown-reinforcing or cushioning layers built-up from rubberised plies each having all cords arranged substantially parallel the plies being arranged with all cords disposed along the circumference of the tyre
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60CVEHICLE TYRES; TYRE INFLATION; TYRE CHANGING; CONNECTING VALVES TO INFLATABLE ELASTIC BODIES IN GENERAL; DEVICES OR ARRANGEMENTS RELATED TO TYRES
    • B60C9/00Reinforcements or ply arrangement of pneumatic tyres
    • B60C9/02Carcasses
    • B60C9/04Carcasses the reinforcing cords of each carcass ply arranged in a substantially parallel relationship
    • B60C9/06Carcasses the reinforcing cords of each carcass ply arranged in a substantially parallel relationship the cords extend diagonally from bead to bead and run in opposite directions in each successive carcass ply, i.e. bias angle ply
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60CVEHICLE TYRES; TYRE INFLATION; TYRE CHANGING; CONNECTING VALVES TO INFLATABLE ELASTIC BODIES IN GENERAL; DEVICES OR ARRANGEMENTS RELATED TO TYRES
    • B60C9/00Reinforcements or ply arrangement of pneumatic tyres
    • B60C9/02Carcasses
    • B60C9/04Carcasses the reinforcing cords of each carcass ply arranged in a substantially parallel relationship
    • B60C9/07Carcasses the reinforcing cords of each carcass ply arranged in a substantially parallel relationship the cords curve from bead to bead in plural planes, e.g. S-shaped cords
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60CVEHICLE TYRES; TYRE INFLATION; TYRE CHANGING; CONNECTING VALVES TO INFLATABLE ELASTIC BODIES IN GENERAL; DEVICES OR ARRANGEMENTS RELATED TO TYRES
    • B60C9/00Reinforcements or ply arrangement of pneumatic tyres
    • B60C9/02Carcasses
    • B60C9/04Carcasses the reinforcing cords of each carcass ply arranged in a substantially parallel relationship
    • B60C2009/0491Carcasses the reinforcing cords of each carcass ply arranged in a substantially parallel relationship with special path of the carcass cords, e.g. sinusoidal
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60CVEHICLE TYRES; TYRE INFLATION; TYRE CHANGING; CONNECTING VALVES TO INFLATABLE ELASTIC BODIES IN GENERAL; DEVICES OR ARRANGEMENTS RELATED TO TYRES
    • B60C9/00Reinforcements or ply arrangement of pneumatic tyres
    • B60C9/18Structure or arrangement of belts or breakers, crown-reinforcing or cushioning layers
    • B60C9/20Structure or arrangement of belts or breakers, crown-reinforcing or cushioning layers built-up from rubberised plies each having all cords arranged substantially parallel
    • B60C2009/2012Structure or arrangement of belts or breakers, crown-reinforcing or cushioning layers built-up from rubberised plies each having all cords arranged substantially parallel with particular configuration of the belt cords in the respective belt layers
    • B60C2009/2019Structure or arrangement of belts or breakers, crown-reinforcing or cushioning layers built-up from rubberised plies each having all cords arranged substantially parallel with particular configuration of the belt cords in the respective belt layers comprising cords at an angle of 30 to 60 degrees to the circumferential direction
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60CVEHICLE TYRES; TYRE INFLATION; TYRE CHANGING; CONNECTING VALVES TO INFLATABLE ELASTIC BODIES IN GENERAL; DEVICES OR ARRANGEMENTS RELATED TO TYRES
    • B60C9/00Reinforcements or ply arrangement of pneumatic tyres
    • B60C9/18Structure or arrangement of belts or breakers, crown-reinforcing or cushioning layers
    • B60C9/20Structure or arrangement of belts or breakers, crown-reinforcing or cushioning layers built-up from rubberised plies each having all cords arranged substantially parallel
    • B60C2009/2048Structure or arrangement of belts or breakers, crown-reinforcing or cushioning layers built-up from rubberised plies each having all cords arranged substantially parallel characterised by special physical properties of the belt plies
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60CVEHICLE TYRES; TYRE INFLATION; TYRE CHANGING; CONNECTING VALVES TO INFLATABLE ELASTIC BODIES IN GENERAL; DEVICES OR ARRANGEMENTS RELATED TO TYRES
    • B60C9/00Reinforcements or ply arrangement of pneumatic tyres
    • B60C9/18Structure or arrangement of belts or breakers, crown-reinforcing or cushioning layers
    • B60C9/20Structure or arrangement of belts or breakers, crown-reinforcing or cushioning layers built-up from rubberised plies each having all cords arranged substantially parallel
    • B60C9/22Structure or arrangement of belts or breakers, crown-reinforcing or cushioning layers built-up from rubberised plies each having all cords arranged substantially parallel the plies being arranged with all cords disposed along the circumference of the tyre
    • B60C2009/2214Structure or arrangement of belts or breakers, crown-reinforcing or cushioning layers built-up from rubberised plies each having all cords arranged substantially parallel the plies being arranged with all cords disposed along the circumference of the tyre characterised by the materials of the zero degree ply cords

Definitions

  • the present invention relates to a tire, radial carcass reinforcement and more particularly a tire for fitting vehicles carrying heavy loads, such as, for example trucks, tractors, trailers or road buses.
  • the carcass reinforcement is anchored on both sides in the bead zone and is radially surmounted by a crown reinforcement consisting of at least two layers, superimposed and formed of son or parallel cables in each layer and crossed from one layer to the next in making with the circumferential direction angles between 10 ° and 45 °.
  • Said working layers, forming the working armature can still be covered with at least one so-called protective layer and formed of advantageously metallic and extensible reinforcing elements, called elastic elements.
  • the triangulation ply may also comprise a layer of metal wires or cables forming with the circumferential direction an angle of between 45 ° and 90 °, this so-called triangulation ply being radially located between the carcass reinforcement and the first crown ply of work, formed of parallel wires or cables having angles at most equal to 45 ° in absolute value.
  • the triangulation ply forms with at least said working ply a triangulated reinforcement, which presents, under the different stresses it undergoes, few deformations, the triangulation ply having the essential role of taking up the transverse compression forces of which the object all the reinforcing elements in the area of the crown of the tire.
  • Cables are said to be inextensible when said cables have under a tensile force equal to 10% of the breaking force a relative elongation at most equal to 0.2%.
  • Circumferential reinforcing elements are reinforcing elements which make angles with the circumferential direction in the range + 2.5 °, -2.5 ° around 0 °.
  • the circumferential direction of the tire is the direction corresponding to the periphery of the tire and defined by the rolling direction of the tire.
  • the transverse or axial direction of the tire is parallel to the axis of rotation of the tire.
  • the radial direction is a direction intersecting the axis of rotation of the tire and perpendicular thereto.
  • the axis of rotation of the tire is the axis around which it rotates in normal use.
  • a radial or meridian plane is a plane which contains the axis of rotation of the tire.
  • the circumferential mid-plane, or equatorial plane is a plane perpendicular to the axis of rotation of the tire and which divides the tire into two halves.
  • the measurements of force at break (maximum load in N), tensile strength (in MPa), elongation at break (total elongation in%) and of module (in GPa) are made in traction according to the ISO 6892 standard of 1984.
  • an axially continuous sheet formed of non-extensible metal cables forming an angle of at least 60 ° with the circumferential direction, and whose axial width is at least equal to the axial width the shortest working crown ply, and secondly between the two working crown plies an additional ply formed of metal elements, oriented substantially parallel to the circumferential direction.
  • the French application WO 99/24269 proposes, on either side of the equatorial plane and in the immediate axial extension of the additional ply of reinforcing elements substantially parallel to the circumferential direction, to couple, over a certain axial distance, the two working crown plies formed of reinforcing elements crossed from one ply to the next ply and then decoupling them by rubber mixing profiles at least over the remainder of the width common to the two tablecloths.
  • the use of tires on vehicles for trucks "type site” leads the tires to suffer shocks when driving on stony ground. These shocks are of course harmful in terms of endurance performance. It is still known to those skilled in the art to increase the number of webs constituting the crown reinforcement to improve the endurance of the tire with respect to such shocks.
  • An object of the invention is to provide tires for vehicles "Heavy-Duty", for example of the type "building site”, whose endurance performance is preserved or improved especially in view of shocks suffered on the tape and whose overall mass is reduced.
  • a vehicle tire of heavy weight type carcass reinforcement consisting of a layer of metal reinforcing elements oriented in a radial direction in the sidewalls of the tire, comprising a frame apex comprising a working crown layer of metal reinforcing elements forming with the circumferential direction an angle (a2) of between 25 ° and 55 °, said working crown layer being centered on the circumferential mid-plane, the reinforcement the crown being radially capped with a tread, said tread being joined to two beads by means of the two sidewalls, the crown reinforcement being completed by at least one layer of circumferential metal reinforcing elements, and on a portion centered on the circumferential median plane of axial width less than the width of said working crown layer, the reinforcing elements of said layer of the carcass reinforcement making with the circumferential direction an angle (a1) such that the average angle (a) defined by the Arctan relation ((tan (
  • RL average of the radii of the axially outermost points on each side of the tire, that is to say the average of the radii, measured in the radial direction, of the axially outermost points on each of the tire sidewalls.
  • the thickness Es and the pitch p 2 are measured on a section of the tire and are expressed in millimeters.
  • angles ⁇ 1 and ⁇ 2, expressed in degrees, are also measured on a section of the tire.
  • the angle measurements are according to the invention made at the circumferential mid-plane.
  • the measurements of the Re and RL spokes are performed on a tire mounted on its nominal rim and inflated to the nominal pressure.
  • the working crown layer is radially external to said at least one layer of circumferential reinforcing elements.
  • the tires according to the invention can be reduced by reducing the number of constituent layers of the crown reinforcement while maintaining or even improving the endurance properties of the crown of the tire. in particular against shocks appearing on the tread for example when driving on stony ground. It is known to those skilled in the art that in order to improve the endurance performance of the crown reinforcement of a tire with respect to this type of impact, it is customary to increase the number of layers of reinforcing elements.
  • the inventors still find that it is possible to do without a protective layer.
  • a protective layer is usually present to be sacrificed in the event of an attack of the tire-type cuts that can alter the integrity of metal reinforcing elements by corrosion phenomena associated with the fatigue of said reinforcing elements.
  • the inventors actually observe that the reinforcing elements of the working crown layer, which is in a radially outermost position of a tire according to the invention, are less stressed when the tire is inflated or when it is use in normal rolling that the reinforcing elements of a radially outermost working crown layer of a tire more usual on the one hand because of the presence of the layer of circumferential reinforcing elements and secondly because of the relatively low utilization ratio of the F2 / FR2 rupture potential in comparison with a conventional tire.
  • the elements reinforcing the working crown layer of a tire according to the invention thus have endurance properties much greater than those of a more usual tire; the inventors thus realize that the removal of the protective layer is made possible and contributes to the lightening of the tire.
  • the inventors propose, for example, the use of a finishing drum having a membrane reinforced by reinforcing elements.
  • the reinforcing elements are only present on a portion of the membrane centered on a plane coming to merge with the equatorial plane position of the tire being made.
  • the presence of these reinforcing elements thus allows the reorientation of the reinforcing elements of the carcass reinforcement layer in the area of the crown of the tire.
  • the reinforcing elements of the carcass reinforcement layer which are initially oriented to form an angle of between 80 ° and 90 ° with the circumferential direction will have their advanced orientation due to the presence of reinforcing elements reinforcing the membrane of the finishing drum.
  • the tire blank thus formed is shaped to pass from a cylindrical structure to a toric structure.
  • the inventors have shown that the presence of reinforcing elements allows the local reorientation of the reinforcing elements of the carcass reinforcement layer during this conformation phase.
  • the reinforcing elements of the layer of reinforcing elements are distributed with not between 1.4 and 3.0 mm.
  • the utilization ratio of the fracture potential F2 / FR2 of the radially outermost working layer is less than 1/15. Such a ratio of utilization of the breaking potential F2 / FR2 further contributes to improving the endurance performance of the reinforcing elements of the radially outermost working layer during the use of the tire.
  • the average angle ⁇ formed by the reinforcing elements of the carcass reinforcement layer is greater than 75 ° on either side of the circumferential mid-plane on two sides. parts axially inside the ends of the working layer and each of said two parts having an axial width of between 10 mm and 35 mm. More preferably, the average angle ⁇ 1 is greater than 82 ° on these two parts.
  • the usual inflation pressures of the truck tires impose an orientation in the radial direction to the reinforcing elements of the carcass reinforcement layer at the level of the tire shoulders and especially since the working layer is no longer radially superposed on the tire. the carcass reinforcement layer. It is therefore preferable to provide these two parts, which are assimilated to transition zones between the portion of the carcass reinforcement layer centered on the equatorial plane and the parts of the carcass reinforcement layer present in the flanks. of the tire.
  • the reinforcing elements are thus advantageously present on the membrane of the finishing drum over an axial width narrower than the axial width of the working layer, a axial width between 14 and 80 mm.
  • the reinforcing elements are present on a narrower width than the layer of circumferential reinforcing elements.
  • said at least one layer of circumferential reinforcing elements has an axial width greater than 0.5xL.
  • L is the maximum axial width of the tire, when the latter is mounted on its service rim and inflated to its recommended pressure.
  • the axial widths of the reinforcing element layers are measured on a cross section of a tire, the tire is therefore in a non-inflated state.
  • the reinforcing elements of said at least one layer of circumferential reinforcing elements are metal reinforcing elements having a secant modulus at 0.7% elongation between 10 and 120 GPa and a maximum tangent modulus less than 150 GPa.
  • the secant modulus of the reinforcing elements at 0.7% elongation is less than 100 GPa and greater than 20 GPa, preferably between 30 and 90 GPa and more preferably less than 80 GPa. .
  • the maximum tangent modulus of the reinforcing elements is less than 130 GPa and more preferably less than 120 GPa.
  • the modules expressed above are measured on a tensile stress curve as a function of the elongation determined with a preload of 20 MPa reduced to the metal section of the reinforcing element, the tensile stress corresponding to a measured voltage brought back to the metal section of the reinforcing element.
  • the modules of the same reinforcing elements can be measured on a tensile stress curve as a function of the elongation determined with a prestress of 10 MPa reduced to the overall section of the reinforcing element, the tensile stress corresponding to a measured voltage brought back to the overall section of the reinforcing element.
  • the overall section of the reinforcing element is the section of a composite element made of metal and rubber, the latter having in particular penetrated the reinforcing element during the baking phase of the tire.
  • the reinforcing elements of the axially outer portions and the central portion of at least one layer of circumferential reinforcing elements are metal reinforcing elements having secant modulus at 0.7% elongation between 5 and 60 GPa and a maximum tangent modulus of less than 75 GPa.
  • the secant modulus of the reinforcing elements at 0.7% elongation is less than 50 Gpa and greater than 10 GPa, preferably between 15 and 45 GPa and more preferably less than 40 GPa. .
  • the maximum tangent modulus of the reinforcing elements is less than 65 GPa and more preferably less than 60 GPa.
  • the reinforcing elements of said at least one layer of circumferential reinforcing elements are metal reinforcing elements having a tensile stress curve as a function of the relative elongation having slight slopes for the low elongations and a substantially constant and strong slope for the higher elongations.
  • Such reinforcing elements of the additional ply are usually referred to as "bi-module" elements.
  • the substantially constant and strong slope appears from a relative elongation of between 0.1% and 0.5%.
  • Reinforcement elements more particularly adapted to the production of at least one layer of circumferential reinforcing elements according to the invention are, for example, assemblies of formula 21.23, the construction of which is 3x (0.26 + 6x0.23). 4.4 / 6.6 SS; this strand cable consists of 21 elementary wires of formula 3 x (1 + 6), with 3 twisted strands each consisting of 7 wires, a wire forming a central core of diameter equal to 26/100 mm and 6 coiled wires of diameter equal to 23/100 mm.
  • Such a cable has a secant module at 0.7% equal to 45 GPa and a maximum tangent modulus equal to 98 GPa, measured on a tensile stress curve as a function of the elongation determined with a preload of 20 MPa brought back to the section. of the reinforcing element, the tensile stress corresponding to a measured voltage brought back to the metal section of the reinforcing element.
  • this cable of formula 21.23 On a tensile stress curve in according to the elongation determined with a preload of 10 MPa brought back to the overall section of the reinforcement element, the tensile stress corresponding to a measured tension brought back to the overall section of the reinforcing element, this cable of formula 21.23 has a secant modulus at 0.7% equal to 23 GPa and a maximum tangent modulus equal to 49 GPa.
  • reinforcement elements is an assembly of formula 21.28, whose construction is 3x (0.32 + 6x0.28) 6.2 / 9.3 SS.
  • This cable has a secant module at 0.7% equal to 56 GPa and a maximum tangent modulus equal to 102 GPa, measured on a tensile stress curve as a function of the elongation determined with a preload of 20 MPa brought to the cross section.
  • metal of the reinforcing element the tensile stress corresponding to a measured voltage brought back to the metal section of the reinforcing element.
  • this cable of formula 21.28 On a tensile stress curve as a function of the elongation determined with a preload of 10 MPa brought back to the overall section of the reinforcing element, the tensile stress corresponding to a measured tension brought back to the overall section of the element of reinforcement, this cable of formula 21.28 has a secant module at 0.7% equal to 27 GPa and a maximum tangent modulus equal to 49 GPa.
  • reinforcing elements in at least one layer of circumferential reinforcing elements makes it possible in particular to maintain rigidities of the satisfactory layer including after the shaping and baking steps in conventional manufacturing processes.
  • the circumferential reinforcing elements may be formed of inextensible metal elements and cut so as to form sections of length much shorter than the circumference of the least long layer, but preferably greater than 0.1 times said circumference, the cuts between sections being axially offset with respect to each other. More preferably, the tensile modulus of elasticity per unit width of the additional layer is less than the tensile modulus of elasticity, measured under the same conditions, of the most extensible working crown layer.
  • Such an embodiment makes it possible to confer, in a simple manner, on the layer of reinforcing elements circumferential a module that can easily be adjusted (by the choice of intervals between sections of the same row), but in all cases lower than the module of the layer consisting of the same metallic elements but continuous, the module of the additional layer being measured on a vulcanized layer of cut elements, taken from the tire.
  • the circumferential reinforcing elements are corrugated metal elements, the ratio a / ⁇ of the amplitude of waviness over the wavelength being at most equal to 0, 09.
  • the tensile modulus of elasticity per unit width of the additional layer is smaller than the tensile modulus of elasticity, measured under the same conditions, of the most extensible working crown layer.
  • the reinforcing elements of the working crown layers are inextensible metal cables.
  • the working crown layer and said layer of circumferential reinforcing elements are the only layers present to constitute the crown reinforcement over at least 80% of the axial width. of the crown frame.
  • This advantageous embodiment of the invention goes in the direction of an even greater relief of the tire.
  • the crown reinforcement comprises an additional layer, called protective, radially external to the working crown layers, preferably centered on the circumferential mid-plane.
  • the reinforcing elements of such a protective layer are preferably so-called elastic reinforcing elements, oriented with respect to the circumferential direction with an angle of between 25 ° and 55 ° and in the same direction as the angle formed by the elements. reinforcement of the working layer. More preferably, the reinforcing elements of such a protective layer are parallel to the reinforcing elements of the working layer.
  • the crown reinforcement can be completed between the carcass reinforcement and the radially inner working layer closest to said carcass reinforcement, by a triangulation layer of elements of the carcass reinforcement.
  • Inextensible steel metal reinforcement making, with the circumferential direction, an angle greater than 45 ° and in the same direction as that of the angle formed by the elements of the carcass reinforcement at the equatorial plane.
  • the angle formed by the reinforcing elements of the triangulation layer with the circumferential direction the angle is greater than that formed by the reinforcing elements of the the carcass reinforcement layer with the circumferential direction.
  • said triangulation layer consists of two half-layers positioned axially on either side of the circumferential mid-plane.
  • the tire according to the invention may also comprise one or more layers of additional circumferential reinforcing elements, advantageously consisting of two half-layers positioned axially on either side of the circumferential mid-plane.
  • the figure is not shown in scale to simplify understanding.
  • the figure represents only a half-view of a tire which extends symmetrically with respect to the axis XX 'which represents the circumferential median plane, or equatorial plane, of a tire.
  • the tire 1, of size 12 R 22.5 has a form ratio H / L equal to 0.90, H being the height of the tire 1 on its mounting rim and L its maximum axial width.
  • Said tire 1 comprises a radial carcass reinforcement 2 anchored in two beads, not shown in the figure.
  • the carcass reinforcement 2 is formed of a single layer of metal cables. They still include a tread 5.
  • the carcass reinforcement 2 is shrunk according to the invention by a crown reinforcement 4, formed radially from the inside to the outside: of a layer of circumferential reinforcing elements 41 formed 21x28 steel wire ropes, of "bi-module" type, a working layer 42 formed of metal cables oriented at an angle equal to 45 °.
  • the metal cables constituting the reinforcing elements of the layer of circumferential reinforcing elements are spaced from each other by 2 mm, depending on the normal direction of the average line of the cables.
  • the metal cables constituting the reinforcing elements of the working layer are cables of formula 9.35. They are distributed in the working layer with a distance between the reinforcing elements, measured according to the normal to the direction of the average line of the cable equal to 2 mm and form an angle a2 with the circumferential direction equal to 45 °.
  • the tire is inflated to a pressure of 9 bar.
  • the axial width L of the layer of circumferential reinforcing elements 41 is equal to 158 mm.
  • the axial width L 42 of the working layer 42 is equal to 202 mm.
  • the axial width of the tread L 5 is equal to 215 mm.
  • the axial width L is equal to 302 mm.
  • the angle ⁇ 1 formed by the reinforcing elements of the carcass reinforcement layer with the circumferential direction at the equatorial plane is equal to 70 °.
  • the reinforcing elements of the carcass reinforcement layer 2 form this angle ⁇ 1 on a width D, substantially equal to 138 mm, defined by the axial width on which are present the reinforcing elements on the finishing drum, after shaping.
  • the average angle a is equal to 58.9 ° and is well between 30 ° and 67 °.
  • the mean angle ⁇ 1 formed by the reinforcing elements of the carcass reinforcement layer 2 with the circumferential direction has a value equal to 83 °.
  • the average angle ⁇ formed by the reinforcement elements of the carcass reinforcement layer 2 with the circumferential direction has a value greater than 88 °.
  • the measured value of Re is equal to 541.7 mm.
  • the measured value of Es is equal to 22.3 mm.
  • the average value RL of the measured rays is equal to 410 mm.
  • the calculated value of Qs is equal to 97.9 mm.
  • F2 is equal to 94 N.
  • the breaking force of the reinforcing elements of the working crown layer FR2 is equal to 2600 N.
  • the utilization ratio of the rupture potential F2 / FR2 is equal to 3.6%.
  • the tire according to the invention is compared to a reference tire of the same size which differs from the tire according to the invention by its crown reinforcement formed radially from the inside to the outside: of a triangulation layer, consisting of two half-plies, formed of non-stranded inextensible metal cables 9.28, oriented at an angle equal to 65 °, a first working layer formed of metal cables oriented at an angle equal to 26 °, a second working layer formed of metal cables oriented at an angle of 18 ° and crossed to the metal cables of the first layer working, the cables of each of the working layers being oriented on either side of the circumferential direction, a protective layer formed of elastic metal cables 6.35.
  • the metal cables of the two working layers are cables of formula 9.35. They are distributed in each of the working layers with a distance between the reinforcing elements, measured according to the normal to the direction of the average line of the cable equal to 2.5 mm.
  • the reference tire is inflated to a pressure of 9 bar.
  • the overall axial width of the triangulation layer is equal to 180 mm, each of the half-plies having a width equal to 60 mm.
  • the axial width of the first working layer is equal to 220 mm.
  • the axial width of the second working layer is equal to 200 mm.
  • the axial width of the protective layer is equal to 136 mm.
  • the cumulative mass of the working layers of the reference tire, the protective layer and the triangulation layer, comprising the mass of the metal cables and calendering mixtures, amounts to 10.0 Kg.
  • First endurance tests were performed on a test machine imposing on each tire a straight line running at a speed equal to the maximum speed index prescribed for said tire (speed index) under an initial load of 3550 Kg gradually increased to reduce the duration of the test.
  • Other endurance tests were performed on a test machine imposing cyclically a transverse force and a dynamic overload to the tires. The tests were carried out for the tires according to the invention with conditions identical to those applied to the reference tires.
  • Tests to characterize the breaking strength of a tire crown reinforcement subjected to shocks were also carried out. These tests consist in rolling a tire, inflated to a recommended pressure and subjected to a recommended load, on an obstacle or cylindrical indenter of diameter equal to 1.5 inches, that is to say 38.1 mm, and of a determined height.
  • the breaking strength is characterized by the critical height of the indenter, that is to say the maximum height of the indenter resulting in a total rupture of the crown reinforcement, that is to say of the breaking of all vertex layers.
  • the values express the energy necessary to obtain the break of the vertex block. The values are expressed from a base 100 corresponding to the value measured for the reference tire.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Tires In General (AREA)

Abstract

The invention relates to a tyre (1), of which the reinforcing elements of the carcass reinforcement (2) are oriented in a radial direction in the sidewalls of the tyre, comprising a crown reinforcement (4) consisting of a working crown layer (42) of reinforcing elements forming, together with the circumferential direction, an angle (α2) of between 25° and 55° and a layer of circumferential reinforcing elements (41). According to the invention, in the crown region, the reinforcing elements of said carcass reinforcement layer (2) form, together with the circumferential direction, an angle (α1) such that the average angle a defined by the formula arctan((tan (|α1|)*tan (|α2|))1/2) is between 30° and 67°, and the utilisation ratio of the breaking potential F2/FR2 of the working layer is less than 1/10.

Description

ARMATURE DE SOMMET DE PNEUMATIQUE CONSTITUEE  REINFORCED PNEUMATIC TOP REINFORCEMENT
D'UNE COUCHE DE SOMMET DE TRAVAIL ET D'UNE  OF A WORK SUMMIT LAYER AND A
COUCHE D'ELEMENTS CIRCONFERENTIELS  LAYER OF CIRCUMFERENTIAL ELEMENTS
[0001] La présente invention concerne un pneumatique, à armature de carcasse radiale et plus particulièrement un pneumatique destiné à équiper des véhicules portant de lourdes charges, tels que, par exemple les camions, tracteurs, remorques ou bus routiers. The present invention relates to a tire, radial carcass reinforcement and more particularly a tire for fitting vehicles carrying heavy loads, such as, for example trucks, tractors, trailers or road buses.
[0002] D'une manière générale dans les pneumatiques de type poids-lourds, l'armature de carcasse est ancrée de part et d'autre dans la zone du bourrelet et est surmontée radialement par une armature de sommet constituée d'au moins deux couches, superposées et formées de fils ou câbles parallèles dans chaque couche et croisés d'une couche à la suivante en faisant avec la direction circonférentielle des angles compris entre 10° et 45°. Lesdites couches de travail, formant l'armature de travail, peuvent encore être recouvertes d'au moins une couche dite de protection et formée d'éléments de renforcement avantageusement métalliques et extensibles, dits élastiques. Elle peut également comprendre une couche de fils ou câbles métalliques faisant avec la direction circonférentielle un angle compris entre 45° et 90°, cette nappe, dite de triangulation, étant radialement située entre l'armature de carcasse et la première nappe de sommet dite de travail, formée de fils ou câbles parallèles présentant des angles au plus égaux à 45° en valeur absolue. La nappe de triangulation forme avec au moins ladite nappe de travail une armature triangulée, qui présente, sous les différentes contraintes qu'elle subit, peu de déformations, la nappe de triangulation ayant pour rôle essentiel de reprendre les efforts de compression transversale dont est l'objet l'ensemble des éléments de renforcement dans la zone du sommet du pneumatique. [0002] In general, in heavy-vehicle tires, the carcass reinforcement is anchored on both sides in the bead zone and is radially surmounted by a crown reinforcement consisting of at least two layers, superimposed and formed of son or parallel cables in each layer and crossed from one layer to the next in making with the circumferential direction angles between 10 ° and 45 °. Said working layers, forming the working armature, can still be covered with at least one so-called protective layer and formed of advantageously metallic and extensible reinforcing elements, called elastic elements. It may also comprise a layer of metal wires or cables forming with the circumferential direction an angle of between 45 ° and 90 °, this so-called triangulation ply being radially located between the carcass reinforcement and the first crown ply of work, formed of parallel wires or cables having angles at most equal to 45 ° in absolute value. The triangulation ply forms with at least said working ply a triangulated reinforcement, which presents, under the different stresses it undergoes, few deformations, the triangulation ply having the essential role of taking up the transverse compression forces of which the object all the reinforcing elements in the area of the crown of the tire.
[0003] Des câbles sont dits inextensibles lorsque lesdits câbles présentent sous une force de traction égale à 10% de la force de rupture un allongement relatif au plus égal à 0,2%. Cables are said to be inextensible when said cables have under a tensile force equal to 10% of the breaking force a relative elongation at most equal to 0.2%.
[0004] Des câbles sont dits élastiques lorsque lesdits câbles présentent sous une force de traction égale à la charge de rupture un allongement relatif au moins égal à 3% avec un module tangent maximum inférieur à 150 GPa. [0005] Des éléments de renforcement circonférentiels sont des éléments de renforcement qui font avec la direction circonférentielle des angles compris dans l'intervalle + 2,5°, - 2,5° autour de 0°. Cables are said elastic when said cables have under tensile force equal to the breaking load a relative elongation of at least 3% with a maximum tangent modulus of less than 150 GPa. [0005] Circumferential reinforcing elements are reinforcing elements which make angles with the circumferential direction in the range + 2.5 °, -2.5 ° around 0 °.
[0006] La direction circonférentielle du pneumatique, ou direction longitudinale, est la direction correspondant à la périphérie du pneumatique et définie par la direction de roulement du pneumatique. The circumferential direction of the tire, or longitudinal direction, is the direction corresponding to the periphery of the tire and defined by the rolling direction of the tire.
[0007] La direction transversale ou axiale du pneumatique est parallèle à l'axe de rotation du pneumatique. [0007] The transverse or axial direction of the tire is parallel to the axis of rotation of the tire.
[0008] La direction radiale est une direction coupant l'axe de rotation du pneumatique et perpendiculaire à celui-ci. The radial direction is a direction intersecting the axis of rotation of the tire and perpendicular thereto.
[0009] L'axe de rotation du pneumatique est l'axe autour duquel il tourne en utilisation normale. The axis of rotation of the tire is the axis around which it rotates in normal use.
[0010] Un plan radial ou méridien est un plan qui contient l'axe de rotation du pneumatique. [0011] Le plan médian circonférentiel, ou plan équatorial, est un plan perpendiculaire à l'axe de rotation du pneu et qui divise le pneumatique en deux moitiés. A radial or meridian plane is a plane which contains the axis of rotation of the tire. The circumferential mid-plane, or equatorial plane, is a plane perpendicular to the axis of rotation of the tire and which divides the tire into two halves.
[0012] En ce qui concerne les fils ou câbles métalliques, les mesures de force à la rupture (charge maximale en N), de résistance à la rupture (en MPa), d'allongement à la rupture (allongement total en %) et de module (en GPa) sont effectuées en traction selon la norme ISO 6892 de 1984. As regards the metal wires or cables, the measurements of force at break (maximum load in N), tensile strength (in MPa), elongation at break (total elongation in%) and of module (in GPa) are made in traction according to the ISO 6892 standard of 1984.
[0013] Certains pneumatiques actuels, dits "routiers", sont destinés à rouler à des vitesses moyennes élevées et sur des trajets de plus en plus longs, du fait de l'amélioration du réseau routier et de la croissance du réseau autoroutier dans le monde. L'ensemble des conditions, sous lesquelles un tel pneumatique est appelé à rouler, permet sans aucun doute un accroissement du nombre de kilomètres parcourus, l'usure du pneumatique étant moindre. Cette augmentation de la durée de vie en termes kilométriques, conjuguée au fait que de telles conditions d'usage sont susceptibles de se traduire, sous forte charge, par des températures sommet relativement élevées, nécessite une augmentation au moins proportionnelle du potentiel d'endurance de l'armature sommet des pneumatiques. Some current tires, called "road", are intended to run at high average speeds and on longer and longer journeys, because of the improvement of the road network and the growth of the motorway network in the world. . The set of conditions under which such a tire is called to roll, undoubtedly allows an increase in the number of kilometers traveled, the wear of the tire being less. This increase in service life in terms of kilometers, combined with the fact that such conditions of use are likely to result, under heavy load, relatively high top temperatures, requires an at least proportional increase in the endurance potential of the crown reinforcement of the tires.
[0014] Il existe en effet des contraintes au niveau de l'armature de sommet et plus particulièrement des contraintes de cisaillement entre les couches de sommet qui, dans le cas d'une trop forte élévation de la température de fonctionnement au niveau des extrémités de la couche de sommet axialement la plus courte, ont pour conséquence l'apparition et la propagation de fissures dans la gomme au niveau desdites extrémités. Le même problème existe dans le cas de bords de deux couches d'éléments de renforcement, ladite autre couche n'étant pas obligatoirement radialement adjacente à la première. [0015] Dans le but d'améliorer l'endurance de l'armature sommet des pneumatiques, la demande française FR 2 728 510 propose de disposer, d'une part entre l'armature de carcasse et la nappe de travail d'armature de sommet, radialement la plus proche de l'axe de rotation, une nappe axialement continue, formée de câbles métalliques inextensibles faisant avec la direction circonférentielle un angle au moins égal à 60°, et dont la largeur axiale est au moins égale à la largeur axiale de la nappe de sommet de travail la plus courte, et d'autre part entre les deux nappes de sommet de travail une nappe additionnelle formée d'éléments métalliques, orientés sensiblement parallèlement à la direction circonférentielle. There are indeed constraints at the crown reinforcement and more particularly shear stresses between the crown layers which, in the case of too high a rise in the operating temperature at the ends of the crown. the axially shorter crown layer, result in the appearance and propagation of cracks in the rubber at said ends. The same problem exists in the case of edges of two layers of reinforcement elements, said other layer not necessarily being radially adjacent to the first. In order to improve the endurance of the tire crown reinforcement, the French application FR 2 728 510 proposes to have, on the one hand, between the carcass reinforcement and the reinforcing steel working ply. radially closest to the axis of rotation, an axially continuous sheet formed of non-extensible metal cables forming an angle of at least 60 ° with the circumferential direction, and whose axial width is at least equal to the axial width the shortest working crown ply, and secondly between the two working crown plies an additional ply formed of metal elements, oriented substantially parallel to the circumferential direction.
[0016] En complément, la demande française WO 99/24269 propose notamment, de part et d'autre du plan équatorial et dans le prolongement axial immédiat de la nappe additionnelle d'éléments de renforcement sensiblement parallèles à la direction circonférentielle, de coupler, sur une certaine distance axiale, les deux nappes de sommet de travail formées d'éléments de renforcement croisés d'une nappe à la suivante pour ensuite les découpler par des profilés de mélange de caoutchouc au moins sur le restant de la largeur commune aux dites deux nappes de travail. [0017] Par ailleurs, l'usage de pneumatiques sur des véhicules pour poids-lourds de type « approche chantier » conduit les pneumatiques à subir des chocs lors de roulages sur des sols caillouteux. Ces chocs sont bien entendu néfastes quant aux performances en termes d ' endurance . [0018] Il est encore connu de l'homme du métier d'augmenter le nombre de nappes constituant l'armature sommet pour améliorer l'endurance du pneumatique à l'égard de tels chocs. In addition, the French application WO 99/24269 proposes, on either side of the equatorial plane and in the immediate axial extension of the additional ply of reinforcing elements substantially parallel to the circumferential direction, to couple, over a certain axial distance, the two working crown plies formed of reinforcing elements crossed from one ply to the next ply and then decoupling them by rubber mixing profiles at least over the remainder of the width common to the two tablecloths. Furthermore, the use of tires on vehicles for trucks "type site" leads the tires to suffer shocks when driving on stony ground. These shocks are of course harmful in terms of endurance performance. It is still known to those skilled in the art to increase the number of webs constituting the crown reinforcement to improve the endurance of the tire with respect to such shocks.
[0019] Quelles que soient l'une de ces solutions telles que présentées précédemment, la présence d'une ou plusieurs couches d'éléments de renforcement supplémentaire conduit à une masse plus importante du pneumatique et à des coûts de fabrication des pneumatiques plus importants. Whatever one of these solutions as presented above, the presence of one or more layers of additional reinforcing elements leads to a larger mass of the tire and higher tire manufacturing costs.
[0020] Un but de l'invention est de fournir des pneumatiques pour véhicules "Poids- Lourds", par exemple de type « approche chantier », dont les performances d'endurance sont conservées voire améliorées notamment au regard des chocs subis sur la bande de roulement et dont la masse globale est diminuée. An object of the invention is to provide tires for vehicles "Heavy-Duty", for example of the type "building site", whose endurance performance is preserved or improved especially in view of shocks suffered on the tape and whose overall mass is reduced.
[0021] Ce but est atteint selon l'invention par un pneumatique pour véhicule de type poids lourd, à armature de carcasse constituée d'une couche d'éléments de renforcement métalliques orientés selon une direction radiale dans les flancs du pneumatique, comprenant une armature de sommet comprenant une couche de sommet de travail d'éléments de renforcement métalliques faisant avec la direction circonférentielle un angle (a2) compris entre 25° et 55°, ladite couche de sommet de travail étant centrée sur le plan médian circonférentiel, l'armature de sommet étant coiffée radialement d'une bande de roulement, ladite bande de roulement étant réunie à deux bourrelets par l'intermédiaire des deux flancs, l'armature de sommet étant complétée par au moins une couche d'éléments de renforcement circonférentiels métalliques, et sur une partie centrée sur le plan médian circonférentiel de largeur axiale inférieure à la largeur de ladite couche de sommet de travail, les éléments de renforcement de ladite couche de l'armature de carcasse faisant avec la direction circonférentielle un angle (al) tel que l'angle moyen (a) défini par la relation Arctan((tan(|al |)*tan(|a2|))1/2) est compris entre 30 et 67°, lesdits angles al et a2 étant orientés de part et d'autre de la direction circonférentielle, le ratio d'utilisation du potentiel de rupture F2/FR2 de la couche de travail étant inférieur à 1/10, dans lequel : This object is achieved according to the invention by a vehicle tire of heavy weight type, carcass reinforcement consisting of a layer of metal reinforcing elements oriented in a radial direction in the sidewalls of the tire, comprising a frame apex comprising a working crown layer of metal reinforcing elements forming with the circumferential direction an angle (a2) of between 25 ° and 55 °, said working crown layer being centered on the circumferential mid-plane, the reinforcement the crown being radially capped with a tread, said tread being joined to two beads by means of the two sidewalls, the crown reinforcement being completed by at least one layer of circumferential metal reinforcing elements, and on a portion centered on the circumferential median plane of axial width less than the width of said working crown layer, the reinforcing elements of said layer of the carcass reinforcement making with the circumferential direction an angle (a1) such that the average angle (a) defined by the Arctan relation ((tan (| al |) * tan (| a2 |)) 1/2 ) is between 30 and 67 °, said angles a1 and a2 being oriented on either side of the circumferential direction, the utilization ratio of the fracture potential F 2 / FR 2 of the working layer being less than 1/10, wherein:
FR2 est la force rupture en extension uniaxiale des éléments de renforcement de la couche de travail, exprimée en N, F2 = 0.1 * P *Qs*p2/ [(sin(|a2|)+tan(|al |)*cos(|a2|))* sin(|a2|)], avec P : pression de gonflage, exprimée en bar, FR2 is the breaking force in uniaxial extension of the reinforcing elements of the working layer, expressed in N, F2 = 0.1 * P * Qs * p 2 / [(sin (| a2 |) + tan (| al |) * cos (| a2 |)) * sin (| a2 |)], with P: inflation pressure, expressed in bar,
Qs = (Rs2-RL2)/(2*Rs), Qs = (Rs 2 -RL 2 ) / (2 * Rs),
p2 : le pas de pose des éléments de renforcement de la couche de sommet de travail, mesuré perpendiculairement aux éléments de renforcement au niveau du plan médian circonférentiel, p 2 : the laying pitch of the reinforcing elements of the working crown layer, measured perpendicular to the reinforcing elements at the circumferential mid-plane,
Rs = Re - Es, Rs = Re - Es,
Re : rayon extérieur du pneumatique mesuré au point radialement le plus extérieur sur la surface de la bande de roulement du pneumatique, ladite surface étant extrapolée pour combler les éventuels creux,  Re: outer radius of the tire measured at the radially outermost point on the surface of the tread of the tire, said surface being extrapolated to fill any cavities,
Es : distance radiale entre le point radialement le plus à l'extérieur du pneumatique et sa projection orthogonale sur la face radialement extérieure d'un élément de renforcement de la couche de sommet de travail, Es: radial distance between the radially outermost point of the tire and its orthogonal projection on the radially outer face of a reinforcing element of the working crown layer,
RL : moyenne des rayons des points axialement les plus à l'extérieur de chaque côté du pneumatique, c'est-à-dire la moyenne des rayons, mesurés selon la direction radiale, des points axialement les plus à l'extérieur sur chacun des flancs du pneumatique.  RL: average of the radii of the axially outermost points on each side of the tire, that is to say the average of the radii, measured in the radial direction, of the axially outermost points on each of the tire sidewalls.
[0022] L'épaisseur Es et le pas p2 sont mesurés sur une coupe du pneumatique et sont exprimés en millimètres. The thickness Es and the pitch p 2 are measured on a section of the tire and are expressed in millimeters.
[0023] Les angles al et a2, exprimés en degré, sont également mesurés sur une coupe du pneumatique. Les mesures d'angles sont selon l'invention réalisées au niveau du plan médian circonférentiel. The angles α1 and α2, expressed in degrees, are also measured on a section of the tire. The angle measurements are according to the invention made at the circumferential mid-plane.
[0024] Les mesures des rayons Re et RL sont réalisées sur un pneumatique monté sur sa jante nominale et gonflé à la pression nominale. The measurements of the Re and RL spokes are performed on a tire mounted on its nominal rim and inflated to the nominal pressure.
[0025] Avantageusement selon l'invention, la couche de sommet de travail est radialement extérieure à ladite au moins une couche d'éléments de renforcement circonférentiels. Advantageously according to the invention, the working crown layer is radially external to said at least one layer of circumferential reinforcing elements.
[0026] Les résultats obtenus avec des pneumatiques conformes à l'invention ont effectivement mis en évidence que les performances en termes d'endurance peuvent être améliorées notamment lors de roulage sur sol caillouteux, l'armature sommet du pneumatique étant allégée. L'allégement de l'armature sommet du pneumatique s'accompagne d'une simplification de fabrication et d'une diminution des coûts de fabrication. The results obtained with tires according to the invention have indeed demonstrated that the performance in terms of endurance can be improved especially when driving on stony ground, the crown reinforcement of the tire being lightened. The lightening of the crown of the tire is accompanied by a simplification of manufacturing and a reduction in manufacturing costs.
[0027] Contre toute attente, les résultats ont effectivement mis en évidence que les pneumatiques selon l'invention peuvent être allégés en diminuant le nombre de couches constitutives de l'armature sommet tout en conservant voire améliorant les propriétés d'endurance du sommet du pneumatique notamment à l'égard de chocs apparaissant sur la bande de roulement par exemple lors de roulage sur sol caillouteux. Il est en effet connu de l'homme du métier que pour améliorer les performances d'endurance de l'armature sommet d'un pneumatique à l'égard de ce type de chocs, il est usuel d'augmenter le nombre de couches d'éléments de renforcement. Against all expectations, the results have indeed demonstrated that the tires according to the invention can be reduced by reducing the number of constituent layers of the crown reinforcement while maintaining or even improving the endurance properties of the crown of the tire. in particular against shocks appearing on the tread for example when driving on stony ground. It is known to those skilled in the art that in order to improve the endurance performance of the crown reinforcement of a tire with respect to this type of impact, it is customary to increase the number of layers of reinforcing elements.
[0028] Les inventeurs pensent interpréter ces résultats du fait de l'angle formé avec la direction circonférentielle par les éléments de renforcement de la couche d'armature de carcasse dans la zone du sommet du pneumatique, ceux-ci se substituant fonctionnellement à des éléments d'une couche de sommet de travail. Il semble selon les inventeurs qu'il est ainsi possible que la couche d'armature de carcasse joue le rôle d'une couche de travail dont les éléments de renforcement seraient croisés avec les éléments de la couche de sommet de travail dans la zone du sommet du pneumatique telle que la prévoit le pneumatique selon l'invention. The inventors think to interpret these results because of the angle formed with the circumferential direction by the reinforcing elements of the carcass reinforcement layer in the area of the crown of the tire, the latter functionally substituting elements a working top layer. It seems according to the inventors that it is thus possible for the carcass reinforcement layer to act as a working layer whose reinforcing elements would be crossed with the elements of the working crown layer in the zone of the crown. of the tire as provided by the tire according to the invention.
[0029] Les inventeurs font encore le constat qu'il est possible de se passer d'une couche de protection. Une telle couche est habituellement présente pour être sacrifiée en cas d'agressions du pneumatique de type coupures pouvant venir altérer l'intégrité d'éléments de renforcement métalliques par des phénomènes de corrosion associés à la fatigue desdits éléments de renforcement. Les inventeurs font effectivement le constat que les éléments de renforcement de la couche de sommet de travail, qui est dans une position radialement la plus extérieure d'un pneumatique selon l'invention, sont moins sollicités lors du gonflage du pneumatique ou bien lors de son utilisation en roulage normal que les éléments de renforcement d'une couche de sommet de travail radialement la plus extérieure d'un pneumatique plus usuel d'une part du fait de la présence de la couche d'éléments de renforcement circonférentiels et d'autre part du fait du ratio d'utilisation du potentiel de rupture F2/FR2 relativement faible en comparaison d'un pneumatique usuel. Les éléments de renforcement de la couche de sommet de travail d'un pneumatique selon l'invention présentent ainsi des propriétés d'endurance bien supérieures à ceux d'un pneumatique plus usuel ; les inventeurs font ainsi le constat que la suppression de la couche de protection est rendue possible et permet de contribuer à l'allégement du pneumatique. The inventors still find that it is possible to do without a protective layer. Such a layer is usually present to be sacrificed in the event of an attack of the tire-type cuts that can alter the integrity of metal reinforcing elements by corrosion phenomena associated with the fatigue of said reinforcing elements. The inventors actually observe that the reinforcing elements of the working crown layer, which is in a radially outermost position of a tire according to the invention, are less stressed when the tire is inflated or when it is use in normal rolling that the reinforcing elements of a radially outermost working crown layer of a tire more usual on the one hand because of the presence of the layer of circumferential reinforcing elements and secondly because of the relatively low utilization ratio of the F2 / FR2 rupture potential in comparison with a conventional tire. The elements reinforcing the working crown layer of a tire according to the invention thus have endurance properties much greater than those of a more usual tire; the inventors thus realize that the removal of the protective layer is made possible and contributes to the lightening of the tire.
[0030] Afin d'obtenir une couche d'armature de carcasse dont les éléments de renforcement forment un angle avec la direction circonférentielle compris entre 80 et 90° dans les flancs et dont les éléments de renforcement forment un angle l avec la direction circonférentielle sur une partie centrée sur le plan médian circonférentiel, tel que l'angle moyen a soit compris entre 30 et 67°, les inventeurs proposent, par exemple, l'utilisation d'un tambour de finition comportant une membrane renforcée par des éléments de renforcement. Afin d'obtenir le pneumatique selon l'invention, les éléments de renforcements sont seulement présents sur une partie de la membrane centrée sur un plan venant se confondre avec la position du plan équatorial du pneumatique en cours de confection. In order to obtain a carcass reinforcement layer whose reinforcing elements form an angle with the circumferential direction between 80 and 90 ° in the sidewalls and whose reinforcing elements form an angle 1 with the circumferential direction on a part centered on the circumferential median plane, such that the average angle a is between 30 and 67 °, the inventors propose, for example, the use of a finishing drum having a membrane reinforced by reinforcing elements. In order to obtain the tire according to the invention, the reinforcing elements are only present on a portion of the membrane centered on a plane coming to merge with the equatorial plane position of the tire being made.
[0031] La présence de ces éléments de renforcement autorise ainsi la réorientation des éléments de renforcement de la couche d'armature de carcasse dans la zone du sommet du pneumatique. En effet, les inventeurs ont mis en évidence que lors de la fabrication du pneumatique, les éléments de renforcement de la couche d'armature de carcasse qui sont initialement orientés pour former angle compris entre 80° et 90° avec la direction circonférentielle vont voir leur orientation évoluée du fait de la présence des éléments de renforcement renforçant la membrane du tambour de finition. Après la pose de la couche d'armature de carcasse et avant la mise en place de l'armature sommet, l'ébauche de pneumatique ainsi constituée est conformée pour passer d'une structure cylindrique à une structure torique. Les inventeurs ont montré que la présence des éléments de renforcement autorise la réorientation locale des éléments de renforcement de la couche d'armature de carcasse durant cette phase de conformation. The presence of these reinforcing elements thus allows the reorientation of the reinforcing elements of the carcass reinforcement layer in the area of the crown of the tire. Indeed, the inventors have demonstrated that during the manufacture of the tire, the reinforcing elements of the carcass reinforcement layer which are initially oriented to form an angle of between 80 ° and 90 ° with the circumferential direction will have their advanced orientation due to the presence of reinforcing elements reinforcing the membrane of the finishing drum. After the laying of the carcass reinforcement layer and before the setting of the crown reinforcement, the tire blank thus formed is shaped to pass from a cylindrical structure to a toric structure. The inventors have shown that the presence of reinforcing elements allows the local reorientation of the reinforcing elements of the carcass reinforcement layer during this conformation phase.
[0032] Selon un mode de réalisation préféré de l'invention, les éléments de renforcement de la couche d'éléments de renforcement sont répartis avec pas compris entre 1.4 et 3.0 mm. [0033] Avantageusement selon l'invention, le ratio d'utilisation du potentiel de rupture F2/FR2 de la couche de travail radialement la plus extérieure est inférieur à 1/15. Un tel ratio d'utilisation du potentiel de rupture F2/FR2 contribue encore à améliorer les performances d'endurance des éléments de renforcement de la couche de travail radialement la plus extérieure lors de l'utilisation du pneumatique. According to a preferred embodiment of the invention, the reinforcing elements of the layer of reinforcing elements are distributed with not between 1.4 and 3.0 mm. Advantageously according to the invention, the utilization ratio of the fracture potential F2 / FR2 of the radially outermost working layer is less than 1/15. Such a ratio of utilization of the breaking potential F2 / FR2 further contributes to improving the endurance performance of the reinforcing elements of the radially outermost working layer during the use of the tire.
[0034] Selon un mode de réalisation préféré de l'invention, l'angle moyen al formé par les éléments de renforcement de la couche d'armature de carcasse est supérieur à 75° de part et d'autre du plan médian circonférentiel sur deux parties axialement à l'intérieur des extrémités de la couche de travail et chacune desdites deux parties présentant une largeur axiale comprise entre 10 mm et 35 mm. De préférence encore, l'angle moyen al est supérieur à 82° sur ces deux parties. Les pressions usuelles de gonflage des pneumatiques poids lourds imposent une orientation selon la direction radiale aux éléments de renforcement de la couche d'armature de carcasse au niveau des épaules du pneumatique et notamment dès lors que la couche de travail n'est plus radialement superposée à la couche d'armature de carcasse. Il est donc préférable de prévoir ces deux parties, qui s'assimilent à des zones de transition entre la partie de la couche d'armature de carcasse centrée sur le plan équatorial et les parties de la couche d'armature de carcasse présentent dans les flancs du pneumatique. According to a preferred embodiment of the invention, the average angle α formed by the reinforcing elements of the carcass reinforcement layer is greater than 75 ° on either side of the circumferential mid-plane on two sides. parts axially inside the ends of the working layer and each of said two parts having an axial width of between 10 mm and 35 mm. More preferably, the average angle α1 is greater than 82 ° on these two parts. The usual inflation pressures of the truck tires impose an orientation in the radial direction to the reinforcing elements of the carcass reinforcement layer at the level of the tire shoulders and especially since the working layer is no longer radially superposed on the tire. the carcass reinforcement layer. It is therefore preferable to provide these two parts, which are assimilated to transition zones between the portion of the carcass reinforcement layer centered on the equatorial plane and the parts of the carcass reinforcement layer present in the flanks. of the tire.
[0035] Après conformation, lorsque la couche de travail est mise en place, les éléments de renforcement sont ainsi avantageusement présents sur la membrane du tambour de finition sur une largeur axiale plus étroite que la largeur axiale de la couche de travail, d'une largeur axiale comprise entre 14 et 80 mm. Avantageusement encore, les éléments de renforcement sont présents sur une largeur plus étroite que la couche d'éléments de renforcement circonférentiels. [0036] Selon une variante avantageuse de réalisation de l'invention, ladite au moins une couche d'éléments de renforcement circonférentiels présente une largeur axiale supérieure à 0.5xL. After shaping, when the working layer is put in place, the reinforcing elements are thus advantageously present on the membrane of the finishing drum over an axial width narrower than the axial width of the working layer, a axial width between 14 and 80 mm. Advantageously, the reinforcing elements are present on a narrower width than the layer of circumferential reinforcing elements. According to an advantageous embodiment of the invention, said at least one layer of circumferential reinforcing elements has an axial width greater than 0.5xL.
[0037] L est la largeur maximale axiale du pneumatique, lorsque ce dernier est monté sur sa jante de service et gonflé à sa pression recommandée. [0038] Les largeurs axiales des couches d'éléments de renforcement sont mesurées sur une coupe transversale d'un pneumatique, le pneumatique étant donc dans un état non gonflé. L is the maximum axial width of the tire, when the latter is mounted on its service rim and inflated to its recommended pressure. The axial widths of the reinforcing element layers are measured on a cross section of a tire, the tire is therefore in a non-inflated state.
[0039] Selon un mode de réalisation avantageux de l'invention, les éléments de renforcement de ladite au moins une couche d'éléments de renforcement circonférentiels sont des éléments de renforcement métalliques présentant un module sécant à 0,7 % d'allongement compris entre 10 et 120 GPa et un module tangent maximum inférieur à 150 GPa. According to an advantageous embodiment of the invention, the reinforcing elements of said at least one layer of circumferential reinforcing elements are metal reinforcing elements having a secant modulus at 0.7% elongation between 10 and 120 GPa and a maximum tangent modulus less than 150 GPa.
[0040] Selon une réalisation préférée, le module sécant des éléments de renforcement à 0,7 % d'allongement est inférieur à 100 GPa et supérieur à 20 GPa, de préférence compris entre 30 et 90 GPa et de préférence encore inférieur à 80 GPa. According to a preferred embodiment, the secant modulus of the reinforcing elements at 0.7% elongation is less than 100 GPa and greater than 20 GPa, preferably between 30 and 90 GPa and more preferably less than 80 GPa. .
[0041] De préférence également, le module tangent maximum des éléments de renforcement est inférieur à 130 GPa et de préférence encore inférieur à 120 GPa. Also preferably, the maximum tangent modulus of the reinforcing elements is less than 130 GPa and more preferably less than 120 GPa.
[0042] Les modules exprimés ci-dessus sont mesurés sur une courbe contrainte de traction en fonction de l'allongement déterminée avec une précontrainte de 20 MPa ramenée à la section de métal de l'élément de renforcement, la contrainte de traction correspondant à une tension mesurée ramenée à la section de métal de l'élément de renforcement. The modules expressed above are measured on a tensile stress curve as a function of the elongation determined with a preload of 20 MPa reduced to the metal section of the reinforcing element, the tensile stress corresponding to a measured voltage brought back to the metal section of the reinforcing element.
[0043] Les modules des mêmes éléments de renforcement peuvent être mesurés sur une courbe contrainte de traction en fonction de l'allongement déterminée avec une précontrainte de 10 MPa ramenée à la section globale de l'élément de renforcement, la contrainte de traction correspondant à une tension mesurée ramenée à la section globale de l'élément de renforcement. La section globale de l'élément de renforcement est la section d'un élément composite constitué de métal et de caoutchouc, ce dernier ayant notamment pénétré l'élément de renforcement pendant la phase de cuisson du pneumatique. The modules of the same reinforcing elements can be measured on a tensile stress curve as a function of the elongation determined with a prestress of 10 MPa reduced to the overall section of the reinforcing element, the tensile stress corresponding to a measured voltage brought back to the overall section of the reinforcing element. The overall section of the reinforcing element is the section of a composite element made of metal and rubber, the latter having in particular penetrated the reinforcing element during the baking phase of the tire.
[0044] Selon cette formulation relative à la section globale de l'élément de renforcement, les éléments de renforcement des parties axialement extérieures et de la partie centrale d'au moins une couche d'éléments de renforcement circonférentiels sont des éléments de renforcement métalliques présentant un module sécant à 0,7 % d'allongement compris entre 5 et 60 GPa et un module tangent maximum inférieur à 75 GPa. According to this formulation relating to the overall section of the reinforcing element, the reinforcing elements of the axially outer portions and the central portion of at least one layer of circumferential reinforcing elements are metal reinforcing elements having secant modulus at 0.7% elongation between 5 and 60 GPa and a maximum tangent modulus of less than 75 GPa.
[0045] Selon une réalisation préférée, le module sécant des éléments de renforcement à 0,7 % d'allongement est inférieur à 50 Gpa et supérieur à 10 GPa, de préférence compris entre 15 et 45 GPa et de préférence encore inférieure à 40 GPa. According to a preferred embodiment, the secant modulus of the reinforcing elements at 0.7% elongation is less than 50 Gpa and greater than 10 GPa, preferably between 15 and 45 GPa and more preferably less than 40 GPa. .
[0046] De préférence également, le module tangent maximum des éléments de renforcement est inférieur à 65 GPa et de préférence encore inférieur à 60 GPa. Also preferably, the maximum tangent modulus of the reinforcing elements is less than 65 GPa and more preferably less than 60 GPa.
[0047] Selon un mode de réalisation préféré, les éléments de renforcements de ladite au moins une couche d'éléments de renforcement circonférentiels sont des éléments de renforcement métalliques présentant une courbe contrainte de traction en fonction de l'allongement relatif ayant des faibles pentes pour les faibles allongements et une pente sensiblement constante et forte pour les allongements supérieurs. De tels éléments de renforcement de la nappe additionnelle sont habituellement dénommés éléments "bi- module". According to a preferred embodiment, the reinforcing elements of said at least one layer of circumferential reinforcing elements are metal reinforcing elements having a tensile stress curve as a function of the relative elongation having slight slopes for the low elongations and a substantially constant and strong slope for the higher elongations. Such reinforcing elements of the additional ply are usually referred to as "bi-module" elements.
[0048] Selon une réalisation préférée de l'invention, la pente sensiblement constante et forte apparaît à partir d'un allongement relatif compris entre 0,1% et 0,5%. According to a preferred embodiment of the invention, the substantially constant and strong slope appears from a relative elongation of between 0.1% and 0.5%.
[0049] Les différentes caractéristiques des éléments de renforcement énoncées ci- dessus sont mesurées sur des éléments de renforcement prélevés sur des pneumatiques. The various characteristics of the reinforcement elements mentioned above are measured on reinforcing elements taken from tires.
[0050] Des éléments de renforcement plus particulièrement adaptés à la réalisation d'au moins une couche d'éléments de renforcement circonférentiels selon l'invention sont par exemple des assemblages de formule 21.23, dont la construction est 3x(0.26+6x0.23) 4.4/6.6 S S ; ce câble à torons est constitué de 21 fils élémentaires de formule 3 x (1+6), avec 3 torons tordus ensembles chacun constitué de 7 fils, un fil formant une âme centrale de diamètre égal à 26/100 mm et 6 fils enroulés de diamètre égal à 23/100 mm. Un tel câble présente un module sécant à 0,7% égal à 45 GPa et un module tangent maximum égal à 98 GPa, mesurés sur une courbe contrainte de traction en fonction de l'allongement déterminée avec une précontrainte de 20 MPa ramenée à la section de métal de l'élément de renforcement, la contrainte de traction correspondant à une tension mesurée ramenée à la section de métal de l'élément de renforcement. Sur une courbe contrainte de traction en fonction de l'allongement déterminée avec une précontrainte de 10 MPa ramenée à la section globale de l'élément de renforcement, la contrainte de traction correspondant à une tension mesurée ramenée à la section globale de l'élément de renforcement, ce câble de formule 21.23 présente un module sécant à 0,7% égal à 23 GPa et un module tangent maximum égal à 49 GPa. Reinforcement elements more particularly adapted to the production of at least one layer of circumferential reinforcing elements according to the invention are, for example, assemblies of formula 21.23, the construction of which is 3x (0.26 + 6x0.23). 4.4 / 6.6 SS; this strand cable consists of 21 elementary wires of formula 3 x (1 + 6), with 3 twisted strands each consisting of 7 wires, a wire forming a central core of diameter equal to 26/100 mm and 6 coiled wires of diameter equal to 23/100 mm. Such a cable has a secant module at 0.7% equal to 45 GPa and a maximum tangent modulus equal to 98 GPa, measured on a tensile stress curve as a function of the elongation determined with a preload of 20 MPa brought back to the section. of the reinforcing element, the tensile stress corresponding to a measured voltage brought back to the metal section of the reinforcing element. On a tensile stress curve in according to the elongation determined with a preload of 10 MPa brought back to the overall section of the reinforcement element, the tensile stress corresponding to a measured tension brought back to the overall section of the reinforcing element, this cable of formula 21.23 has a secant modulus at 0.7% equal to 23 GPa and a maximum tangent modulus equal to 49 GPa.
[0051] De la même façon, un autre exemple d'éléments de renforcement est un assemblage de formule 21.28, dont la construction est 3x(0.32+6x0.28) 6.2/9.3 SS. Ce câble présente un module sécant à 0,7% égal à 56 GPa et un module tangent maximum égal à 102 GPa, mesurés sur une courbe contrainte de traction en fonction de l'allongement déterminée avec une précontrainte de 20 MPa ramenée à la section de métal de l'élément de renforcement, la contrainte de traction correspondant à une tension mesurée ramenée à la section de métal de l'élément de renforcement. Sur une courbe contrainte de traction en fonction de l'allongement déterminée avec une précontrainte de 10 MPa ramenée à la section globale de l'élément de renforcement, la contrainte de traction correspondant à une tension mesurée ramenée à la section globale de l'élément de renforcement, ce câble de formule 21.28 présente un module sécant à 0,7% égal à 27 GPa et un module tangent maximum égal à 49 GPa. In the same way, another example of reinforcement elements is an assembly of formula 21.28, whose construction is 3x (0.32 + 6x0.28) 6.2 / 9.3 SS. This cable has a secant module at 0.7% equal to 56 GPa and a maximum tangent modulus equal to 102 GPa, measured on a tensile stress curve as a function of the elongation determined with a preload of 20 MPa brought to the cross section. metal of the reinforcing element, the tensile stress corresponding to a measured voltage brought back to the metal section of the reinforcing element. On a tensile stress curve as a function of the elongation determined with a preload of 10 MPa brought back to the overall section of the reinforcing element, the tensile stress corresponding to a measured tension brought back to the overall section of the element of reinforcement, this cable of formula 21.28 has a secant module at 0.7% equal to 27 GPa and a maximum tangent modulus equal to 49 GPa.
[0052] L'utilisation de tels éléments de renforcement dans au moins une couche d'éléments de renforcement circonférentiels permet notamment de conserver des rigidités de la couche satisfaisante y compris après les étapes de conformation et de cuisson dans des procédés de fabrication usuels. The use of such reinforcing elements in at least one layer of circumferential reinforcing elements makes it possible in particular to maintain rigidities of the satisfactory layer including after the shaping and baking steps in conventional manufacturing processes.
[0053] Selon un deuxième mode de réalisation de l'invention, les éléments de renforcement circonférentiels peuvent être formées d'éléments métalliques inextensibles et coupés de manière à former des tronçons de longueur très inférieure à la circonférence de la couche la moins longue, mais préférentiellement supérieure à 0,1 fois ladite circonférence, les coupures entre tronçons étant axialement décalées les unes par rapport aux autres. De préférence encore, le module d'élasticité à la traction par unité de largeur de la couche additionnelle est inférieur au module d'élasticité à la traction, mesuré dans les mêmes conditions, de la couche de sommet de travail la plus extensible. Un tel mode de réalisation permet de conférer, de manière simple, à la couche d'éléments de renforcement circonférentiels un module pouvant facilement être ajusté (par le choix des intervalles entre tronçons d'une même rangée), mais dans tous les cas plus faible que le module de la couche constituée des mêmes éléments métalliques mais continus, le module de la couche additionnelle étant mesuré sur une couche vulcanisée d'éléments coupés, prélevée sur le pneumatique. According to a second embodiment of the invention, the circumferential reinforcing elements may be formed of inextensible metal elements and cut so as to form sections of length much shorter than the circumference of the least long layer, but preferably greater than 0.1 times said circumference, the cuts between sections being axially offset with respect to each other. More preferably, the tensile modulus of elasticity per unit width of the additional layer is less than the tensile modulus of elasticity, measured under the same conditions, of the most extensible working crown layer. Such an embodiment makes it possible to confer, in a simple manner, on the layer of reinforcing elements circumferential a module that can easily be adjusted (by the choice of intervals between sections of the same row), but in all cases lower than the module of the layer consisting of the same metallic elements but continuous, the module of the additional layer being measured on a vulcanized layer of cut elements, taken from the tire.
[0054] Selon un troisième mode de réalisation de l'invention, les éléments de renforcement circonférentiels sont des éléments métalliques ondulés, le rapport a/λ de l'amplitude d'ondulation sur la longueur d'onde étant au plus égale à 0,09. De préférence, le module d'élasticité à la traction par unité de largeur de la couche additionnelle est inférieur au module d'élasticité à la traction, mesuré dans les mêmes conditions, de la couche de sommet de travail la plus extensible. According to a third embodiment of the invention, the circumferential reinforcing elements are corrugated metal elements, the ratio a / λ of the amplitude of waviness over the wavelength being at most equal to 0, 09. Preferably, the tensile modulus of elasticity per unit width of the additional layer is smaller than the tensile modulus of elasticity, measured under the same conditions, of the most extensible working crown layer.
[0055] Selon un mode de réalisation de l'invention, les éléments de renforcement des couches de sommet de travail sont des câbles métalliques inextensibles. According to one embodiment of the invention, the reinforcing elements of the working crown layers are inextensible metal cables.
[0056] Selon un mode de réalisation avantageux de l'invention, la couche de sommet de travail et ladite couche d'éléments de renforcement circonférentiels sont les seules couches présentes pour constituer l'armature de sommet sur au moins 80% de la largeur axiale de l'armature sommet. Ce mode de réalisation avantageux de l'invention va dans le sens d'un allégement encore plus important du pneumatique. According to an advantageous embodiment of the invention, the working crown layer and said layer of circumferential reinforcing elements are the only layers present to constitute the crown reinforcement over at least 80% of the axial width. of the crown frame. This advantageous embodiment of the invention goes in the direction of an even greater relief of the tire.
[0057] Selon d'autres variantes de réalisation de l'invention décalant le compromis de performance du pneumatique de façon moins favorable pour ce qui concerne l'allégement, l'armature de sommet comporte une couche supplémentaire, dite de protection, radialement extérieure aux couches de sommet de travail, de préférence centrée sur le plan médian circonférentiel. Les éléments de renforcements d'un telle couche de protection sont de préférence des éléments de renforcement dits élastiques, orientés par rapport à la direction circonférentielle avec un angle compris entre 25° et 55° et de même sens que l'angle formé par les éléments de renforcement de la couche de travail. De préférence encore, les éléments de renforcements d'une telle couche de protection sont parallèles aux éléments de renforcement de la couche de travail. [0058] D'autres variantes peuvent encore prévoir que l'armature de sommet peut être complétée entre l'armature de carcasse et la couche de travail radialement intérieure la plus proche de ladite armature de carcasse, par une couche de triangulation d'éléments de renforcement inextensibles métalliques en acier faisant, avec la direction circonférentielle, un angle supérieur à 45° et de même sens que celui de l'angle formé par les éléments de l'armature de carcasse au niveau du plan équatorial. Selon un mode de réalisation préféré selon ces variantes de réalisation, au niveau du plan équatorial, l'angle formé par les éléments de renforcement de la couche de triangulation avec la direction circonférentielle l'angle est supérieur à celui formé par les éléments de renforcement de la couche d'armature de carcasse avec la direction circonférentielle. Avantageusement, ladite couche de triangulation est constituée de deux demi-couches positionnées axialement de part et d'autre du plan médian circonférentiel. According to other embodiments of the invention offsetting the compromise of performance of the tire in a less favorable manner with regard to lightening, the crown reinforcement comprises an additional layer, called protective, radially external to the working crown layers, preferably centered on the circumferential mid-plane. The reinforcing elements of such a protective layer are preferably so-called elastic reinforcing elements, oriented with respect to the circumferential direction with an angle of between 25 ° and 55 ° and in the same direction as the angle formed by the elements. reinforcement of the working layer. More preferably, the reinforcing elements of such a protective layer are parallel to the reinforcing elements of the working layer. Other variants may also provide that the crown reinforcement can be completed between the carcass reinforcement and the radially inner working layer closest to said carcass reinforcement, by a triangulation layer of elements of the carcass reinforcement. Inextensible steel metal reinforcement making, with the circumferential direction, an angle greater than 45 ° and in the same direction as that of the angle formed by the elements of the carcass reinforcement at the equatorial plane. According to a preferred embodiment according to these embodiments, at the equatorial plane, the angle formed by the reinforcing elements of the triangulation layer with the circumferential direction the angle is greater than that formed by the reinforcing elements of the the carcass reinforcement layer with the circumferential direction. Advantageously, said triangulation layer consists of two half-layers positioned axially on either side of the circumferential mid-plane.
[0059] Le pneumatique selon l'invention peut encore comporter une ou plusieurs couches d'éléments de renforcement circonférentiels supplémentaires, avantageusement constituée de deux demi-couches positionnées axialement de part et d'autre du plan médian circonférentiel. The tire according to the invention may also comprise one or more layers of additional circumferential reinforcing elements, advantageously consisting of two half-layers positioned axially on either side of the circumferential mid-plane.
[0060] D'autres détails et caractéristiques avantageux de l'invention ressortiront ci- après de la description d'un exemple de réalisation de l'invention en référence à la figure qui représente une vue méridienne d'un schéma d'un pneumatique selon un mode de réalisation de l'invention. Other details and advantageous features of the invention will emerge below from the description of an exemplary embodiment of the invention with reference to the figure which shows a meridian view of a diagram of a tire according to an embodiment of the invention.
[0061] La figure n'est pas représentée à l'échelle pour en simplifier la compréhension. La figure ne représentent qu'une demi-vue d'un pneumatique qui se prolonge de manière symétrique par rapport à l'axe XX' qui représente le plan médian circonférentiel, ou plan équatorial, d'un pneumatique. [0062] Sur la figure, le pneumatique 1, de dimension 12 R 22.5, a un rapport de forme H/L égal à 0,90, H étant la hauteur du pneumatique 1 sur sa jante de montage et L sa largeur axiale maximale. Ledit pneumatique 1 comprend une armature de carcasse radiale 2 ancrée dans deux bourrelets, non représentés sur la figure. L'armature de carcasse 2 est formée d'une seule couche de câbles métalliques. Ils comportent encore une bande de roulement 5. [0063] Sur la figure, l'armature de carcasse 2 est frettée conformément à l'invention par une armature de sommet 4, formée radialement de l'intérieur à l'extérieur : d'une couche d'éléments de renforcement circonférentiels 41 formée de câbles métalliques en acier 21x28, de type "bi-module", d'une couche de travail 42 formée de câbles métalliques orientés d'un angle égal à 45°. The figure is not shown in scale to simplify understanding. The figure represents only a half-view of a tire which extends symmetrically with respect to the axis XX 'which represents the circumferential median plane, or equatorial plane, of a tire. In the figure, the tire 1, of size 12 R 22.5 has a form ratio H / L equal to 0.90, H being the height of the tire 1 on its mounting rim and L its maximum axial width. Said tire 1 comprises a radial carcass reinforcement 2 anchored in two beads, not shown in the figure. The carcass reinforcement 2 is formed of a single layer of metal cables. They still include a tread 5. In the figure, the carcass reinforcement 2 is shrunk according to the invention by a crown reinforcement 4, formed radially from the inside to the outside: of a layer of circumferential reinforcing elements 41 formed 21x28 steel wire ropes, of "bi-module" type, a working layer 42 formed of metal cables oriented at an angle equal to 45 °.
[0064] Les câbles métalliques constituant les éléments de renforcement de la couche d'éléments de renforcement circonférentiels sont distants les uns des autres de 2 mm, selon la normale à la direction de la ligne moyenne des câbles. The metal cables constituting the reinforcing elements of the layer of circumferential reinforcing elements are spaced from each other by 2 mm, depending on the normal direction of the average line of the cables.
[0065] Les câbles métalliques constituant les éléments de renforcement de la couche de travail sont des câbles de formule 9.35. Ils sont répartis dans la couche de travail avec une distance entre les éléments de renforcement, mesurée selon la normale à la direction de la ligne moyenne du câble égale à 2 mm et forment un angle a2 avec la direction circonférentielle égal à 45°. The metal cables constituting the reinforcing elements of the working layer are cables of formula 9.35. They are distributed in the working layer with a distance between the reinforcing elements, measured according to the normal to the direction of the average line of the cable equal to 2 mm and form an angle a2 with the circumferential direction equal to 45 °.
[0066] Le pneumatique est gonflé à une pression de 9 bars. The tire is inflated to a pressure of 9 bar.
[0067] La largeur axiale L de la couche d'éléments de renforcement circonférentiels 41 est égale à 158 mm. The axial width L of the layer of circumferential reinforcing elements 41 is equal to 158 mm.
[0068] La largeur axiale L42 de la couche de travail 42 est égale à 202 mm. The axial width L 42 of the working layer 42 is equal to 202 mm.
[0069] La largeur axiale de la bande de roulement L5 est égale à 215 mm. [0070] La largeur axiale L est égale à 302 mm. The axial width of the tread L 5 is equal to 215 mm. The axial width L is equal to 302 mm.
[0071] La masse cumulée de la couche de travail 42 et de la couche d'éléments de renforcement circonférentiels 41, comprenant la masse des câbles et des mélanges de calandrage, se monte ainsi à 6.5 Kg. The cumulative mass of the working layer 42 and the layer of circumferential reinforcing elements 41, including the mass of the cables and calendering mixtures, thus amounts to 6.5 Kg.
[0072] L'angle al formé par les éléments de renforcement de la couche d'armature de carcasse avec la direction circonférentielle au niveau du plan équatorial est égal à 70°. Les éléments de renforcement de la couche d'armature de carcasse 2 forment cet angle al sur une largeur D, sensiblement égale à 138 mm, définie par la largeur axiale sur laquelle sont présents les éléments de renforcement sur le tambour de finition, après conformation. The angle α1 formed by the reinforcing elements of the carcass reinforcement layer with the circumferential direction at the equatorial plane is equal to 70 °. The reinforcing elements of the carcass reinforcement layer 2 form this angle α1 on a width D, substantially equal to 138 mm, defined by the axial width on which are present the reinforcing elements on the finishing drum, after shaping.
[0073] L'angle moyen a est égal à 58.9° et est bien compris entre 30° et 67°. The average angle a is equal to 58.9 ° and is well between 30 ° and 67 °.
[0074] Sur une largeur 1, mesurée selon l'abscisse curviligne de la couche d'armature de carcasse égale à 29 mm, avantageusement comprise entre 10 et 35 mm, correspondant sensiblement à la distance entre l'extrémité de la couche de travail 42 et l'extrémité des éléments de renforcement sur le tambour de finition, l'angle moyen al formé par les éléments de renforcement de la couche d'armature de carcasse 2 avec la direction circonférentielle présente une valeur égale à 83°. On a width 1, measured according to the curvilinear abscissa of the carcass reinforcement layer equal to 29 mm, advantageously between 10 and 35 mm, substantially corresponding to the distance between the end of the working layer 42 and the end of the reinforcing elements on the finishing drum, the mean angle α1 formed by the reinforcing elements of the carcass reinforcement layer 2 with the circumferential direction has a value equal to 83 °.
[0075] Au-delà de l'extrémité de la couche de travail 42, l'angle moyen al formé par les éléments de renforcement de la couche d'armature de carcasse 2 avec la direction circonférentielle présente une valeur supérieure à 88°. Beyond the end of the working layer 42, the average angle α formed by the reinforcement elements of the carcass reinforcement layer 2 with the circumferential direction has a value greater than 88 °.
[0076] La valeur mesurée de Re est égale à 541.7 mm. The measured value of Re is equal to 541.7 mm.
[0077] La valeur mesurée de Es est égale à 22.3 mm. The measured value of Es is equal to 22.3 mm.
[0078] La valeur moyenne RL des rayons mesurés est égale à 410 mm. The average value RL of the measured rays is equal to 410 mm.
[0079] La valeur calculée de Qs est égale à 97.9 mm. The calculated value of Qs is equal to 97.9 mm.
[0080] La valeur de F2 est égale à 94 N. The value of F2 is equal to 94 N.
[0081] La force rupture des éléments de renforcement de la couche de sommet de travail FR2 est égale à 2600 N. The breaking force of the reinforcing elements of the working crown layer FR2 is equal to 2600 N.
[0082] Le ratio d'utilisation du potentiel de rupture F2/FR2 est égal à 3.6 %. The utilization ratio of the rupture potential F2 / FR2 is equal to 3.6%.
[0083] Le pneumatique selon l'invention est comparé à un pneumatique de référence de même dimension qui diffère du pneumatique selon l'invention par son armature de sommet formée radialement de l'intérieur à l'extérieur : d'une couche de triangulation, constituée de deux demi nappes, formée de câbles métalliques inextensibles 9.28 non frettés, orientés d'un angle égal à 65°, d'une première couche de travail formée de câbles métalliques orientés d'un angle égal à 26°, d'une seconde couche de travail formée de câbles métalliques orientés d'un angle égal à 18° et croisés aux câbles métalliques de la première couche de travail, les câbles de chacune des couches de travail étant orientés de part et d'autre de la direction circonférentielle, d'une couche de protection formées de câbles métalliques élastiques 6.35. The tire according to the invention is compared to a reference tire of the same size which differs from the tire according to the invention by its crown reinforcement formed radially from the inside to the outside: of a triangulation layer, consisting of two half-plies, formed of non-stranded inextensible metal cables 9.28, oriented at an angle equal to 65 °, a first working layer formed of metal cables oriented at an angle equal to 26 °, a second working layer formed of metal cables oriented at an angle of 18 ° and crossed to the metal cables of the first layer working, the cables of each of the working layers being oriented on either side of the circumferential direction, a protective layer formed of elastic metal cables 6.35.
[0084] Les câbles métalliques des deux couches de travail sont des câbles de formule 9.35. Ils sont répartis dans chacune des couches de travail avec une distance entre les éléments de renforcement, mesurée selon la normale à la direction de la ligne moyenne du câble égale à 2.5 mm. The metal cables of the two working layers are cables of formula 9.35. They are distributed in each of the working layers with a distance between the reinforcing elements, measured according to the normal to the direction of the average line of the cable equal to 2.5 mm.
[0085] Le pneumatique de référence est gonflé à une pression de 9 bars. The reference tire is inflated to a pressure of 9 bar.
[0086] La largeur axiale globale de la couche triangulation est égale à 180 mm, chacune des demi-nappes présentant une largeur égale à 60 mm. The overall axial width of the triangulation layer is equal to 180 mm, each of the half-plies having a width equal to 60 mm.
[0087] La largeur axiale de la première couche de travail est égale à 220 mm. The axial width of the first working layer is equal to 220 mm.
[0088] La largeur axiale de la deuxième couche de travail est égale à 200 mm. The axial width of the second working layer is equal to 200 mm.
[0089] La largeur axiale de la couche de protection est égale à 136 mm. The axial width of the protective layer is equal to 136 mm.
[0090] La masse cumulée des couches de travail du pneumatique de référence, de la couche de protection et de la couche de triangulation, comprenant la masse des câbles métalliques et des mélanges de calandrage, se monte à 10.0 Kg. The cumulative mass of the working layers of the reference tire, the protective layer and the triangulation layer, comprising the mass of the metal cables and calendering mixtures, amounts to 10.0 Kg.
[0091] Des essais ont été réalisés avec des pneumatiques réalisés selon l'invention conformément à la figure 1 et avec le pneumatique de référence. Tests were carried out with tires made according to the invention in accordance with Figure 1 and with the reference tire.
[0092] Des premiers essais d'endurance ont été réalisés sur une machine de test imposant à chacun des pneumatiques un roulage ligne droite à une vitesse égale à l'indice de vitesse maximum prescrit pour ledit pneumatique (speed index) sous une charge initiale de 3550 Kg progressivement augmentée pour réduire la durée du test. [0093] D'autres essais d'endurance ont été réalisés sur une machine de tests imposant de façon cyclique un effort transversal et une surcharge dynamique aux pneumatiques. Les essais ont été réalisés pour les pneumatiques selon l'invention avec des conditions identiques à celles appliquées aux pneumatiques de référence. First endurance tests were performed on a test machine imposing on each tire a straight line running at a speed equal to the maximum speed index prescribed for said tire (speed index) under an initial load of 3550 Kg gradually increased to reduce the duration of the test. Other endurance tests were performed on a test machine imposing cyclically a transverse force and a dynamic overload to the tires. The tests were carried out for the tires according to the invention with conditions identical to those applied to the reference tires.
[0094] Les essais ainsi réalisés ont montré que les distances parcourues lors de chacun de ces tests sont sensiblement identiques pour les pneumatiques selon l'invention et les pneumatiques de référence. Il apparaît donc que les pneumatiques selon l'invention présentent des performances sensiblement équivalentes en termes d'endurance à celles des pneumatiques de référence lors de roulage sur des sols bitumineux. The tests thus carried out showed that the distances traveled during each of these tests are substantially identical for the tires according to the invention and the reference tires. It therefore appears that the tires according to the invention have substantially equivalent performances in terms of endurance to those of the reference tires when driving on bituminous floors.
[0095] Des tests visant à caractériser la résistance à la rupture d'une armature de sommet de pneumatique soumise à des chocs ont également été réalisés. Ces tests consistent à faire rouler un pneumatique, gonflé à une pression recommandée et soumis à une charge recommandée, sur un obstacle ou indenteur cylindrique de diamètre égal à 1.5 pouce, soit 38.1 mm, et d'une hauteur déterminée. La résistance à la rupture est caractérisée par la hauteur critique de l'indenteur, c'est-à-dire la hauteur maximale de l'indenteur entraînant une rupture totale de l'armature de sommet, c'est-à-dire de la rupture de toutes les couches de sommet. Les valeurs expriment l'énergie nécessaire pour obtenir la rupture du bloc sommet. Les valeurs sont exprimées à partir d'une base 100 correspondant à la valeur mesurée pour le pneumatique de référence. Tests to characterize the breaking strength of a tire crown reinforcement subjected to shocks were also carried out. These tests consist in rolling a tire, inflated to a recommended pressure and subjected to a recommended load, on an obstacle or cylindrical indenter of diameter equal to 1.5 inches, that is to say 38.1 mm, and of a determined height. The breaking strength is characterized by the critical height of the indenter, that is to say the maximum height of the indenter resulting in a total rupture of the crown reinforcement, that is to say of the breaking of all vertex layers. The values express the energy necessary to obtain the break of the vertex block. The values are expressed from a base 100 corresponding to the value measured for the reference tire.
Ces résultats montrent que malgré un allégement du pneumatique par une diminution de la masse de son armature sommet, l'énergie à rupture lors d'un choc sur la surface de la bande de roulement est signifïcativement supérieure. These results show that despite lightening of the tire by a reduction in the mass of its crown reinforcement, the energy at rupture during an impact on the surface of the tread is significantly higher.

Claims

REVENDICATIONS
1 - Pneumatique pour véhicule de type poids lourd, à armature de carcasse constituée d'une couche d'éléments de renforcement métalliques orientés selon une direction radiale dans les flancs du pneumatique, comprenant une armature de sommet comprenant une couche de sommet de travail d'éléments de renforcement métalliques faisant avec la direction circonférentielle un angle (a2) compris entre 25° et 55°, ladite couche de sommet de travail étant centrée sur le plan médian circonférentiel, l'armature de sommet étant coiffée radialement d'une bande de roulement, ladite bande de roulement étant réunie à deux bourrelets par l'intermédiaire de deux flancs, caractérisé en ce que l'armature de sommet est complétée par une couche d'éléments de renforcement circonférentiels métalliques, en ce que, sur une partie centrée sur le plan médian circonférentiel de largeur axiale inférieure à la largeur de ladite couche de sommet de travail, les éléments de renforcement de ladite couche de l'armature de carcasse font avec la direction circonférentielle un angle (al) tel que l'angle moyen a défini par la relation Arctan((tan(|al |)*tan(|a2|))1/2) est compris entre 30 et 67°, en ce que lesdits angles al et a2 sont orientés de part et d'autre de la direction circonférentielle, en ce que le ratio d'utilisation du potentiel de rupture F2/FR2 de la couche de travail est inférieur à 1/10, dans lequel : A tire for a heavy vehicle, carcass-reinforced vehicle consisting of a layer of metal reinforcing elements oriented in a radial direction in the sidewalls of the tire, comprising a crown reinforcement comprising a working crown layer of metal reinforcing elements forming with the circumferential direction an angle (a2) of between 25 ° and 55 °, said working crown layer being centered on the circumferential mid-plane, the crown reinforcement being radially capped with a tread , said tread being joined to two beads by two sidewalls, characterized in that the crown reinforcement is completed by a layer of metal circumferential reinforcing elements, in that, on a portion centered on the median circumferential plane of axial width less than the width of said working crown layer, the reinforcing elements said layer of the carcass reinforcement makes with the circumferential direction an angle (a1) such that the average angle a defined by the Arctan relation ((tan (| al |) * tan (| a2 |)) 1 / 2 ) is between 30 ° and 67 °, in that said angles α1 and α2 are oriented on either side of the circumferential direction, in that the utilization ratio of the fracture potential F 2 / FR 2 of the work is less than 1/10, in which:
FR2 est la force rupture en extension uniaxiale des éléments de renforcement de la couche de travail, exprimée en N, F2 = 0.1 *P*Qs*p2/ [(sin(|a2|)+tan(|al |)*cos(|<x2))* sin(|a2|)], avecFR2 is the breaking force in uniaxial extension of the reinforcing elements of the working layer, expressed in N, F2 = 0.1 * P * Qs * p 2 / [(sin (| a2 |) + tan (| al |) * cos (| <x2)) * sin (| a2 |)], with
P : pression de gonflage, exprimée en bar, P: inflation pressure, expressed in bar,
Qs = (Rs2-RL2)/(2*Rs), Qs = (Rs 2 -RL 2 ) / (2 * Rs),
p2 : le pas de pose des éléments de renforcement de la couche de sommet de travail, mesuré perpendiculairement aux éléments de renforcement au niveau du plan médian circonférentiel, Rs = Re - Es, p 2 : the laying pitch of the reinforcing elements of the working crown layer, measured perpendicularly to the reinforcing elements at the circumferential mid-plane, Rs = Re-Es,
Re : rayon extérieur du pneumatique mesuré au point radialement le plus extérieur sur la surface de la bande de roulement du pneumatique, ladite surface étant extrapolée pour combler les éventuels creux,  Re: outer radius of the tire measured at the radially outermost point on the surface of the tread of the tire, said surface being extrapolated to fill any cavities,
Es : distance radiale entre le point radialement le plus à l'extérieur du pneumatique et sa projection orthogonale sur la face radialement extérieure d'un élément de renforcement de la couche de sommet de travail, RL : moyenne des rayons des points axialement les plus à l'extérieur de chaque côté du pneumatique. Es: radial distance between the radially outermost point of the tire and its orthogonal projection on the radially outer face of a reinforcing element of the working crown layer, RL: average of the radii of the axially outermost points on each side of the tire.
2 - Pneumatique selon la revendication 1, caractérisé en ce que la couche de sommet de travail est radialement extérieure à la couche d'éléments de renforcement circonférentiels. 2 - A tire according to claim 1, characterized in that the working crown layer is radially external to the layer of circumferential reinforcing elements.
3 - Pneumatique selon l'une des revendications 1 ou 2, caractérisé en ce que la couche de sommet de travail et ladite couche d'éléments de renforcement circonférentiels sont les seules couches présentes pour constituer l'armature de sommet sur au moins 80% de la largeur axiale de l'armature sommet. 3 - tire according to one of claims 1 or 2, characterized in that the working crown layer and said layer of circumferential reinforcing elements are the only layers present to form the crown reinforcement on at least 80% of the axial width of the crown reinforcement.
4 - Pneumatique selon l'une des revendications précédentes, caractérisé en ce que le ratio d'utilisation du potentiel de rupture F2/FR2 de la couche de travail est inférieur à 1/15. 4 - tire according to one of the preceding claims, characterized in that the utilization ratio of the fracture potential F2 / FR2 of the working layer is less than 1/15.
5 - Pneumatique selon l'une des revendications précédentes, caractérisé en ce que l'angle al formé par les éléments de renforcement de la couche d'armature de carcasse est supérieur à 75° de part et d'autre du plan médian circonférentiel sur deux parties axialement à l'intérieur des extrémités de la couche de travail et en ce que chacune desdites deux parties présente une largeur axiale comprise entre 10 mm et 35 mm. 5 - tire according to one of the preceding claims, characterized in that the angle α formed by the reinforcing elements of the carcass reinforcement layer is greater than 75 ° on either side of the circumferential mid-plane on two parts axially inside the ends of the working layer and in that each of said two parts has an axial width of between 10 mm and 35 mm.
6 - Pneumatique selon l'une des revendications précédentes, caractérisé en ce que les éléments de renforcement de la couche de sommet de travail sont des câbles métalliques inextensibles. 6 - tire according to one of the preceding claims, characterized in that the reinforcing elements of the working crown layer are inextensible metal cables.
7 - Pneumatique selon l'une des revendications précédentes, caractérisé en ce que les éléments de renforcement de ladite au moins une couche d'éléments de renforcement circonférentiels sont des éléments de renforcement métalliques présentant un module sécant à 0,7 % d'allongement compris entre 10 et 120 GPa et un module tangent maximum inférieur à 150 GPa. 7 - A tire according to one of the preceding claims, characterized in that the reinforcing elements of said at least one layer of circumferential reinforcing elements are metal reinforcing elements having a secant modulus at 0.7% elongation included between 10 and 120 GPa and a maximum tangent modulus less than 150 GPa.
PCT/FR2018/050673 2017-03-22 2018-03-20 Tyre crown reinforcement consisting of a working crown layer and a layer of circumferential elements WO2018172691A1 (en)

Applications Claiming Priority (2)

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FR17/52340 2017-03-22
FR1752340A FR3064213B1 (en) 2017-03-22 2017-03-22 PNEUMATIC SUMMIT REINFORCEMENT COMPRISING A TOP WORK LAYER AND A LAYER OF CIRCUMFERENTIAL ELEMENTS

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113646185A (en) * 2019-03-29 2021-11-12 米其林集团总公司 Tyre crown reinforcement consisting of two working crown layers and of a layer of circumferential reinforcing elements

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2930425A (en) * 1954-12-06 1960-03-29 Pirelli Pneumatic tire
FR2728510A1 (en) 1994-12-23 1996-06-28 Michelin & Cie T / H SHAPE TIRE LESS THAN OR EQUAL TO 0.6
WO1999024269A1 (en) 1997-11-05 1999-05-20 Compagnie Generale Des Etablissements Michelin - Michelin & Cie Crown ply reinforcement for heavy vehicle tyre
EP1052117A2 (en) * 1999-05-06 2000-11-15 Dunlop Tire Corporation Improvements to tyres
WO2016166057A1 (en) * 2015-04-17 2016-10-20 Compagnie Generale Des Etablissements Michelin Tyre reinforcing ply

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2930425A (en) * 1954-12-06 1960-03-29 Pirelli Pneumatic tire
FR2728510A1 (en) 1994-12-23 1996-06-28 Michelin & Cie T / H SHAPE TIRE LESS THAN OR EQUAL TO 0.6
WO1999024269A1 (en) 1997-11-05 1999-05-20 Compagnie Generale Des Etablissements Michelin - Michelin & Cie Crown ply reinforcement for heavy vehicle tyre
EP1052117A2 (en) * 1999-05-06 2000-11-15 Dunlop Tire Corporation Improvements to tyres
WO2016166057A1 (en) * 2015-04-17 2016-10-20 Compagnie Generale Des Etablissements Michelin Tyre reinforcing ply

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113646185A (en) * 2019-03-29 2021-11-12 米其林集团总公司 Tyre crown reinforcement consisting of two working crown layers and of a layer of circumferential reinforcing elements

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FR3064213A1 (en) 2018-09-28

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