Patent Application
20170182845
The present invention relates to a tire having a radial carcass reinforcement, and more particularly a tire intended to equip vehicles that carry heavy loads and run at sustained speed, such as lorries, tractors, trailers or buses, for example.
In the tires of heavy duty type, the carcass reinforcement is generally anchored on either side in the area of the bead and is surmounted radially by a crown reinforcement made up of at least two layers that are superimposed and formed of threads or cords which are parallel in each layer and crossed from one layer to the next, forming angles of between 10° and 45° with the circumferential direction. The said working layers that form the working reinforcement may furthermore be covered with at least one layer, referred to as a protective layer, formed of reinforcing elements which are advantageously metallic and extensible and referred to as elastic reinforcing elements. It may also comprise a layer of metal threads or cords having low extensibility, forming an angle of between 45° and 90° with the circumferential direction, this ply, referred to as the triangulation ply, being located radially between the carcass reinforcement and the first crown ply, referred to as the working ply, formed of parallel threads or cords lying at angles not exceeding 45° in terms of absolute value. The triangulation ply forms a triangulated reinforcement with at least the said working ply, this reinforcement having low deformation under the various stresses which it undergoes, the triangulation ply essentially serving to absorb the transverse compressive forces that act on all the reinforcing elements in the crown area of the tire.
Cords are said to be inextensible when the said cords exhibit, under a tensile force equal to 10% of the breaking force, a relative elongation at most equal to 0.2%.
Cords are said to be elastic when the said cords exhibit, under a tensile force equal to the breaking load, a relative elongation at least equal to 3% with a maximum tangent modulus of less than 150 GPa.
Circumferential reinforcing elements are reinforcing elements which form angles with the circumferential direction in the range +2.5°, −2.5° around 0°.
The circumferential direction of the tire, or longitudinal direction, is the direction that corresponds to the periphery of the tire and is defined by the direction in which the tire runs.
The transverse or axial direction of the tire is parallel to the axis of rotation of the tire.
The radial direction is a direction that intersects the axis of rotation of the tire and is perpendicular thereto.
The axis of rotation of the tire is the axis about which it turns in normal use.
A radial or meridian plane is a plane which contains the axis of rotation of the tire.
The circumferential median 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 “elastic modulus” of a rubber compound is to be understood as meaning a secant extension modulus at 10% deformation and at ambient temperature.
As far as rubber compositions are concerned, modulus measurements are taken under tension in accordance with standard AFNOR-NFT-46002 of September 1988: the nominal secant modulus (or apparent stress, in MPa) at 10% elongation (normal temperature and relative humidity conditions in accordance with standard AFNOR-NFT-40101 of December 1979) is measured in second elongation (i.e. after an accommodation cycle).
Some current tires, referred to as “road” tires, are intended to run at high speed and over increasingly long journeys, as a result of the improvement in the road network and of the growth of the motorway network throughout the world. The combined conditions under which such a tire is called upon to run without any doubt makes possible an increase in the distance travelled, the wear on the tire being reduced, but on the other hand, the endurance of the tire and in particular of the crown reinforcement is detrimentally affected.
This is because there are stresses in the crown reinforcement and, more particularly, shear stresses between the crown layers, combined with a not-insignificant rise in the operating temperature at the ends of the axially shortest crown layer which have the effect of causing cracks in the rubber to appear and spread at the said ends.
In order to improve the endurance of the crown reinforcement of the type of tire under consideration, solutions relating to the structure and quality of the layers and/or the profiled elements of rubber compounds which are placed between and/or around the ends of the plies and, more particularly, the ends of the axially shortest ply have already been applied.
It is notably known practice to introduce a layer of rubber compound between the ends of the working layers in order to create an uncoupling between the said ends in order to limit shear stresses. Such decoupling layers must, however, exhibit a very good cohesion. Such layers of rubber compounds are, for example, described in Patent Application WO 2004/076204.
Patent FR 1 389 428, in order to improve the resistance to degradation of the rubber compounds situated near the crown reinforcement edges, recommends the use, in combination with a low-hysteresis tread, of a rubber profiled element covering at least the sides and the marginal edges of the crown reinforcement and made up of a low-hysteresis rubber compound.
Patent FR 2 222 232, in order to avoid separations between crown reinforcement plies, teaches the coating of the reinforcement ends in a cushion of rubber of Shore A hardness different from that of the tread surmounting the said reinforcement, and higher than the Shore A hardness of the profiled element of rubber compound placed between the edges of crown reinforcement and carcass reinforcement plies.
Tires produced in this way do effectively allow an improvement in performance notably in terms of endurance.
Moreover, it is known practice, in order to produce tires with a very wide tread or in order to confer greater load bearing capacity on tires of a given dimension, to introduce a layer of circumferential reinforcing elements. Patent application WO 99/24269 describes, for example, the presence of such a layer of circumferential reinforcing elements.
The layer of circumferential reinforcing elements is usually made up of at least one metal cord wound to form a turn of which the angle of layering with respect to the circumferential direction is less than 2.5°.
During testing, the inventors demonstrated that, when certain designs of this type of tire, comprising a layer of circumferential reinforcing elements, were loaded heavily and frequently in a manner such as may be encountered when driving along twisty roads, the said tires could exhibit properties in terms of cornering stiffness that are such that cleavage occurs in the rubber compounds of which the crown reinforcement found between the working layers are made. Such cleavage is, of course, penalizing in terms of the endurance properties of the tire. Such cleavage is further accentuated when running with overload and at high speed, again on twisty roads.
It is an object of the invention to provide tires the endurance properties of which are maintained whatever the degree of wear, and the rolling resistance performance of which is improved in order to contribute to a lowering of the fuel consumption of the vehicles fitted with such tires. The invention notably seeks to improve the dynamic properties of the tires, notably the cornering stiffness, such that the endurance properties are maintained whatever the degree of wear and notably under conditions of running with an overload and at high speed.
This object is achieved according to the invention using a tire with a radial carcass reinforcement comprising a crown reinforcement formed of at least two working crown layers of reinforcing elements, crossed from one layer to the other making with the circumferential direction angles comprised between 10° and 45°, the said at least two working crown layers each being formed of reinforcing elements inserted between two skim layers of rubber compound, a first layer S of polymer compound being in contact with at least one working crown layer and in contact with the carcass reinforcement, the said first layer of polymer compound extending axially as far as at least the axial end of the tread, the said tread capping the crown reinforcement and being connected to two beads by two sidewalls, the crown reinforcement comprising at least one layer of circumferential reinforcing elements, the elastic modulus under tension at 10% elongation of at least one skim layer of at least one working crown layer is greater than 9 MPa, the maximum value of tan(δ), denoted tan(δ)max, of the said at least one skim layer of at least one working crown layer is less than 0.100 and the complex dynamic shear modulus G*, measured at 10% and 60° C. on the return cycle, of the said first layer S of polymer compound being greater than 1.35 MPa.
The loss factor tan(δ) is a dynamic property of the layer of rubber compound. It is measured on a viscosity analyser (Metravib VA4000) according to Standard ASTM D 5992-96. The response of a sample of vulcanized composition (cylindrical test specimen 4 mm thick and 400 mm2 in cross section), subjected to sinusoidal loading in simple alternating shear stress at a frequency of 10 Hz, at a temperature of 60° C. is recorded. The sweep is carried out in deformation amplitude from 0.1 to 50% (outward cycle), then from 50% to 1% (return cycle). The results exploited are the complex dynamic shear modulus (G*) and the loss factor tan(δ). For the return cycle, the maximum observed value for tan(δ) is indicated, denoted tan(δ)max.
The rolling resistance is the resistance that occurs when the tire is rolling. It is represented by the hysteresis losses related to the deformation of the tire during a revolution. The frequency values associated with the revolving of the tire correspond to tan(δ) values measured between 30 and 100° C. The value for tan(δ) at 100° C. thus corresponds to an indication of the rolling resistance of the tire when running
It is also possible to estimate the rolling resistance by measuring rebound energy losses for test specimens with energy imposed at temperatures of 60° C. and expressed as percentages.
Advantageously according to the invention, the loss at 60° C., denoted P60, for the said at least one skim layer of at least one working crown layer is less than 20%.
The use of such compounds with elastic modulus values less than or equal to 9 MPa and with tan(δ)max values of less than 0.100 will make it possible to improve the properties of the tire in terms of rolling resistance while at the same time maintaining satisfactory endurance properties.
According to a preferred embodiment of the invention, the said at least one skim layer of at least one working crown layer is an elastomeric compound based on natural rubber or on synthetic polyisoprene with a predominance of cis-1,4 chains and possibly at least one other diene elastomer, the natural rubber or the synthetic polyisoprene in the case of a blend being present at a content that predominates over the content of the other diene elastomer or elastomers used and of a reinforcing filler made up of:
The BET specific surface area measurement is performed in accordance with the BRUNAUER, EMMET and TELLER method described in “The Journal of the American Chemical Society”, Vol. 60, page 309, February 1938, corresponding to standard NFT 45007, November 1987.
If a clear filler or a white filler is being used, it is necessary to use a coupling and/or covering agent selected from the agents known to those skilled in the art. Mention may be made, as examples of preferred coupling agents, of alkoxysilane sulphides of the bis(3-trialkoxysilylpropyl) polysulphide type and among these in particular of bis(3-triethoxysilylpropyl) tetrasulphide, sold by Degussa under the name Si69 for the pure liquid product and the name X50S for the solid product (50/50 by weight blend with N330 black). Mention may be made, as examples of covering agents, of a fatty alcohol, an alkylalkoxysilane, such as a hexadecyltrimethoxysilane or hexadecyltriethoxysilane respectively sold by Degussa under the names Si116 and Si216, diphenylguanidine, a polyethylene glycol or a silicone oil, optionally modified by means of OH or alkoxy functional groups. The coating and/or coupling agent is used in a proportion of 1/100 and 20/100 by weight to the filler, and preferably in the range from 2/100 to 15/100 if the clear filler forms the whole of the reinforcing filler and in the range from 1/100 to 20/100 if the reinforcing filler is formed by a blend of carbon black and clear filler.
Other examples of reinforcing fillers that have the morphology and surface SiOH and/or AlOH functions of materials of the silica and/or alumina type described hereinabove and that can be used according to the invention as a partial or complete replacement for these include carbon blacks modified either during synthesis by addition to the oil fed to the oven of a silicon and/or aluminium compound or after synthesis by addition, to an aqueous suspension of carbon black in a solution of sodium silicate and/or aluminate of an acid so as to at least partially cover the surface of the carbon black with SiOH and/or AlOH functions. Mention may be made, as nonlimiting examples of carbon-based fillers of this type with SiOH and/or AlOH functional groups at the surface, of the fillers of CSDP type described in Conference No. 24 of the ACS Meeting, Rubber Division, Anaheim, Calif., 6-9 May 1997, and also those of Patent Application EP-A-0 799 854.
When a clear filler is used as the only reinforcing filler, the hysteresis and cohesion properties are obtained by using a precipitated or pyrogenated silica or alternatively a precipitated alumina or even an aluminosilicate with a BET specific surface area comprised between 30 and 260 m2/g. Mention may be made, as nonlimiting examples of filler of this type, of the silicas KS404 from Akzo, Ultrasil VN2 or VN3 and BV3370GR from Degussa, Zeopol 8745 from Huber, Zeosil 175MP or Zeosil 1165MP from Rhodia, HI-SIL 2000 from PPG, and the like.
Included among the diene elastomers that can be used as a blend with natural rubber or a synthetic polyisoprene with a predominance of cis-1,4 chains, mention may be made of a polybutadiene (BR) preferably with a predominance of cis-1,4 chains, a stirene-butadiene copolymer (SBR) solution or emulsion, a butadiene-isoprene copolymer (BIR) or alternatively still, a stirene-butadiene-isoprene terpolymer (SBIR). These elastomers can be elastomers modified during polymerization or after polymerization by means of branching agents, such as a divinylbenzene, or star-branching agents, such as carbonates, halotins or halosilicons, or alternatively by means of functionalization agents resulting in a grafting, to the chain or at the chain end, of oxygen-comprising carbonyl or carboxyl functional groups or else of an amine functional group, such as, for example, by the action of dimethylaminobenzophenone or diethylaminobenzophenone. In the case of blends of natural rubber or synthetic polyisoprene predominantly comprising cis-1,4 chains with one or more of the diene elastomers mentioned above, the natural rubber or the synthetic polyisoprene is preferably used at a predominant content and more preferably at a content of greater than 70 phr.
The choice of reinforcing filler used in the rubber compound of which the at least one skim layer of the at least one working crown layer is made contributes both to obtaining values for the elastic modulus under tension at 10% elongation and to obtaining values for tan(δ)max. However, within the aforementioned ranges of values regarding the said reinforcing fillers, a person skilled in the art will know how to further adapt the quantities of the other conventional ingredients, such as the vulcanizing agents or alternatively derivatives of cobalt, or how to adapt the blending processes in order to obtain the above-mentioned elastic modules and tan(δ)max values.
The most conventional tire designs provide skim layers of the working crown layers with elastic modulus values under tension at 10% elongation substantially equivalent to those of the said at least one skim layer of at least one working crown layer according to the invention but maximum values of tan(δ), denoted tan(δ)max, of the skim layers of the working crown layers greater than 0.120. Such compounds which are more conventional for this type of layer lead to better cohesion.
Within the meaning of the invention, a cohesive rubber compound is a rubber compound that is notably robust in relation to cracking. The cohesion of the compound is thus evaluated by a fatigue cracking test performed on a “PS” (pure shear) test specimen. It consists in determining, once the test specimen has been notched, the crack propagation rate “PR” (nm/cycle) as a function of the energy release rate “E” (J/m2). The experimental range covered by the measurement is comprised in the range −20° C. and +150° C. in terms of temperature, in an atmosphere of air or of nitrogen. The stressing of the test specimen is an imposed dynamic movement with an amplitude of between 0.1 mm and 10 mm in the form of an impulsive stress loading (“haversine” tangent signal) with a rest time equal to the duration of the impulse; the frequency of the signal is of the order of 10 Hz on average.
The measurement comprises 3 parts:
The inventors have been able to demonstrate that the cohesion of the said at least one skim layer of at least one working crown layer in accordance with the invention remains satisfactory.
The inventors have notably demonstrated that the presence of at least one layer of circumferential reinforcing elements contributes to less of a change in cohesion of the skim layers of the working crown layers. Specifically, since the more conventional tire designs notably comprise skim layers of the working crown layers with values of tan(δ)max greater than 0.120, this leads to a change in the cohesion of the said skim layers of the working crown layers, this change having a tendency to be for the worse. The inventors note that the presence of at least one layer of circumferential reinforcing elements that limits the shear stresses between the ends of the working crown layers and also limits the increases in temperature leads to a small change in the cohesion of the said skim layers of the working crown layers. The inventors thus consider that the cohesion of the said at least one skim layer of at least one working crown layer, which is lower than that which exists in more conventional tire designs, is satisfactory in the tire design according to the invention.
The inventors have thus been able to demonstrate that the presence of at least one layer of circumferential reinforcing elements makes it possible to maintain performance notably in terms of endurance but also in terms of satisfactory wear with the combination of an elastic modulus under tension at 10% elongation of the said at least one skim layer of at least one working crown layer greater than 9 MPa and a value of tan(δ)max of the said at least one skim layer of at least one working crown layer less than 0.100.
The inventors have also been able to demonstrate that choosing a first layer S having a complex shear modulus G*, measured at 10% and 60° C. on the return cycle of more than 1.35 MPa, improves the dynamic properties and notably cornering stiffness properties of the tire, especially when the tire is subjected to running conditions that are particularly penalizing in terms of cleavage of the rubber compounds. Indeed the inventors have been able to demonstrate that despite the presence of a layer of circumferential reinforcing elements which does, however, give significant stiffness to the tire, more particularly to the crown reinforcement thereof, the features listed hereinabove for the first layer S make a notable contribution to this cornering stiffness property.
Specifically, and in a way that is entirely unexpected to a person skilled in the art, the properties of the first layer S of polymer compound, the said layer S being positioned in contact with the carcass reinforcement and with at least one layer of the crown reinforcement, have an appreciable influence on the cornering stiffness properties. The presence of the layer of circumferential reinforcing elements would appear to be able to influence the cornering stiffness properties sufficiently and, in theory, optimally, on account of the stiffness it confers upon the tire. Tests carried out have demonstrated that the properties of the first layer S have an appreciable effect on the cornering stiffness properties of the tire and allow these to be improved even when a layer of circumferential reinforcing elements is present. The inventors have further demonstrated that the choice of this first layer S of polymer compound does not impair the performance in terms of the stresses experienced by the tire when driving in a straight line.
Advantageously according to the invention, the complex shear modulus G*, measured at 10% and 60° C. on the return cycle, of the first layer S is less than 2 MPa, so that the thermal properties of the tire are not excessively modified in case that impairs the endurance properties of the tire and the rolling resistance properties thereof.
Advantageously too, the maximum value of tan(δ), denoted tan(δ)max, of the first layer S is less than 0.100.
According to one preferred embodiment of the invention, the first layer S of polymer compound comprises a reinforcing filler made up of:
The inventors have further demonstrated that the first layer S has enough cohesion to limit the spread of cracks that begin when an object pierces the tread of the tire. The inventors also demonstrate the reaching of a tire performance compromise combining the dynamic properties, notably the cornering stiffness, the rolling resistance and the endurance properties even in the abovementioned case when an object pierces the tread of the tire.
According to an advantageous alternative form of the invention, the tire comprises a second layer G of polymer compound radially between the carcass reinforcement and the radially innermost layer of reinforcing elements of the crown reinforcement of axial width at least equal to 70% of the width of the radially innermost layer of reinforcing elements of the crown reinforcement and having a complex shear modulus G*, measured at 10% and 60° C. on the return cycle, of greater than 1.35 MPa.
According to a preferred embodiment of this alternative form of the invention, the axial width of the said second layer G is at most equal to the width of the radially innermost layer of reinforcing elements of the crown reinforcement and, for preference, at least equal to 90% of the width of the radially innermost layer of reinforcing elements of the crown reinforcement.
Preferably also according to this alternative form of the invention, the thickness, measured in the radial direction, of the said second layer G is greater than φ and preferably less than 3φ, φ being the diameter of the reinforcing elements of the radially innermost layer of crown reinforcement.
The inventors have also been able to demonstrate that the second layer G of polymer compound thus defined further contributes to improving the cornering stiffness properties of the tire by supplementing the layer of circumferential reinforcing elements and the first layer S of polymer compound.
Advantageously according to the invention, the complex shear modulus G*, measured at 10% and at 60° C. on the return cycle, of the second layer G is less than 2 MPa, such that the thermal properties of the tire are not excessively modified in case that impairs the endurance properties of the tire and the rolling resistance properties thereof.
Advantageously too, the maximum value of tan(δ), denoted tan(δ)max, of the second layer G is less than 0.100.
According to one preferred embodiment of this alternative form of the invention, the second layer G of polymer compound comprises a reinforcing filler made up of:
Advantageously, the polymer compound that makes up the second layer G is identical to the polymer compound that makes up the second layer S.
According to a preferred embodiment of the invention, with the tire comprising a layer C of rubber compound positioned between at least the ends of the said at least two working crown layers and with the said at least two working crown layers having unequal axial widths, the distance d between the end of the axially narrowest working layer and the working layer separated from the axially narrowest working layer by the layer C of rubber compound is such that 1.1φ<d<2.2φ, φ being the diameter of the reinforcing elements of the said at least one layer of circumferential reinforcing elements and, in a meridian plane, the thickness of the layer C of rubber compound being substantially constant over the axial width comprised between the axially interior end of the layer C and the end of the axially narrowest working layer.
Within the meaning of the invention, the distance d is measured in a meridian plane from cord to cord, namely between the cord of a first working layer and the cord of a second working layer, in a direction substantially perpendicular to the surfaces of the layer C. In other words, this distance d encompasses the thickness of the first layer C and the respective thicknesses of the skim rubber compounds radially on the outside of the cords of the radially inner working layer and radially on the inside of the cords of the radially outer working layer.
Within the meaning of the invention, the thickness of the layer C of rubber compound is measured between the two surfaces of the said layer C on the orthogonal projection of a point on one surface onto the other surface.
Within the meaning of the invention, the thickness of the layer C of rubber compound is substantially constant means that it does not vary by more than 0.3 mm These variations in thickness are due only to phenomena of creep during the manufacture and curing of the tire. The layer C in semi-finished form, which means to say by way of elements ready to be used to create a tire, thus advantageously exhibits a constant thickness.
The various thickness measurements are taken on a cross section of a tire, the tire therefore being in an uninflated state.
The layer C of rubber compound makes it possible to obtain decoupling of the said working crown layers so as to spread the shear stresses over a greater thickness.
Within the meaning of the invention, layers that are coupled are layers in which the respective reinforcing elements are separated radially by at most 1.5 mm, the said thickness of rubber being measured radially between the respectively upper and lower generatices of the said reinforcement elements.
More conventional tire designs provide layers of rubber compound positioned between the ends of the working crown layers with greater thicknesses notably at the region of the end of the narrowest working layer and with a profile of non-uniform thickness when viewed in meridian cross section of the tire so as to allow for such a thickness and so as to avoid excessive disruption to the environment of the end of the narrowest working layer. As explained above, the presence of this layer of rubber compound makes it possible in particular to limit the shear stresses between the ends of the working crown layers, the said working crown layers having no circumferential stiffness at their ends. The distance between the end of the axially narrowest working layer and the working layer separated from the axially narrowest working layer by the layer of rubber compound, measured in accordance with the definition of d given hereinabove, is usually greater than 3.3 mm That corresponds to a thickness of the layer of rubber compound of at least 2.5 mm whereas, in general, its thickness at each of its ends tends toward a value of less than 0.5 mm.
The inventors have been able to demonstrate that the presence of at least one layer of circumferential reinforcing elements makes it possible to maintain performance notably in terms of endurance with a layer C of rubber compound of substantially constant thickness across the axial width comprised between the axially inner end of the layer C and the end of the axially narrowest working layer and such that the distance d is comprised between 1.1φ and 2.2φ. Indeed it would appear that the presence of the layer of circumferential reinforcing elements makes enough of a contribution to reacting at least some of the circumferential tension notably in the contact patch that shear stresses between the ends of the crown working layers can be reduced.
In addition, the combination of the layer of circumferential reinforcing elements and of the first layer S, or even of the second layer G, having a complex shear modulus G*, measured at 10% and 60° C. on the return cycle, greater than 1.35 MPa also makes it possible to maintain the satisfactory tire cornering stiffness properties when the layer C has a substantially constant thickness over the axial width comprised between the axially inner end of the layer C and the end of the axially narrowest working layer and such that the distance d is between 1.1φ and 2.2φ, such a feature relative to the thickness of the layer C being penalizing with regard to the cornering stiffness properties of the tire.
Moreover, the layer C of rubber compound is thus advantageously in the semi-finished state in the form of a layer of constant thickness which is simple to manufacture and can also be stored easily. Specifically, the layers usually employed as described hereinabove and which in cross section have a shape exhibiting variations in thickness are, on the one hand, more difficult to produce and, on the other hand, more difficult to store. Specifically, the variations in thickness create storage problems as these semi-finished products are usually stored coiled on reels. The layer C according to the invention is in the semi-finished product state with a cross section having a profile which is substantially flat compared to the layers conventionally used which are in the semi-finished product state with a cross section having a substantially rounded profile.
Because the manufacture and storage of the layer of rubber compound according to the invention in the form of a semi-finished product is thus simplified to such an extent, this may lead to lower costs of manufacture of the tire although the latter may comprise a layer of circumferential reinforcing elements in addition in comparison with a conventional tire.
According to one advantageous embodiment of the invention, the axially widest working crown layer is radially on the inside of the other working crown layers.
For preference also, the axial width D of the layer of rubber compound C comprised between the axially innermost end of the said layer of rubber compound C and the end of the axially least-wide working crown layer is such that:
3.φ2≦D≦25.φ2
where φ2 is the diameter of the reinforcing elements of the axially least-wide working crown layer. Such a relationship defines a zone of engagement between the layer of rubber compound C and the axially least-wide working crown layer. Such an engagement below a value equal to three times the diameter of the reinforcing elements of the axially least-wide working layer may prove insufficient for obtaining decoupling of the working crown layers in order notably to obtain a reduction in the stresses at the end of the axially least-wide working crown layer. A value for this engagement that is greater than twenty times the diameter of the reinforcing elements of the axially least-wide working layer may lead to too great a reduction in the cornering stiffness of the crown reinforcement of the tire.
For preference, the axial width D of the layer of rubber compound C comprised between the axially innermost end of the said layer of rubber compound C and the end of the axially least-wide working crown layer is greater than 5 mm
According to one advantageous embodiment of the invention, the said reinforcing elements of at least one working crown layer are cords with saturated layers, at least one internal layer being sheathed by a layer made up of a polymer composition such as a non-crosslinkable, crosslinkable or crosslinked rubber composition preferably based on at least one diene elastomer.
Cords referred to as “layered” cords or “multilayered” cords are cords made up of a central nucleus and of one or more practically concentric layers of strands or threads arranged around this central nucleus.
Within the meaning of the invention, a saturated layer of a layered cord is a cord made up of threads in which there is not enough space to add at least one additional thread.
The inventors have been able to demonstrate that the presence of the cords as just described by way of reinforcing elements for the working crown layers are able to contribute to better performance in terms of endurance.
Specifically, it would appear, as explained hereinabove, that the rubber compounds of the skims of the working layers make it possible to reduce the rolling resistance of the tire. That results in a lowering of the temperatures of these rubber compounds, when the tire is being used, which may lead to lower protection of the reinforcing elements with regard to the phenomenon of oxidation under certain conditions of use of the tire. Specifically, the properties of the rubber compounds relating to their ability to block oxygen decrease with temperature and the presence of oxygen may lead to progressive degeneration of the mechanical properties of the cords, for the most harsh running conditions, and may adversely affect the life of these cords.
The presence of the rubber sheath within the cords described hereinabove compensates for this potential risk of oxidation of the reinforcing elements, as the sheath contributes to blocking the oxygen.
The expression “composition based on at least one diene elastomer” means, in the known way, that the composition contains a predomination (i.e. a fraction by mass in excess of 50%) of this or these diene elastomer or elastomers.
It will be noted that the sheath according to the invention extends continuously around the layer that it covers (which means to say that this sheath is continuous in the “orthoradial” direction of the cord, which direction is perpendicular to its radius) so as to form a continuous sleeve the cross section of which is advantageously practically circular.
It will also be noted that the rubber composition of this sheath may be crosslinkable or crosslinked, which means to say that by definition it comprises a crosslinking system suited to allowing the composition to crosslink when it is cured (i.e. to harden rather than to melt); thus, this rubber composition may be qualified as unmeltable, because it cannot be melted whatever the temperature to which it is heated.
The term “diene” elastomer or rubber is understood to mean, in a known way, an elastomer which is based, at least partially (i.e. a homopolymer or a copolymer), on diene monomers (monomers bearing two conjugated or non-conjugated carbon-carbon double bonds).
For preference, the crosslinking system for the rubber sheath is a system referred to as a vulcanization system, namely one based on sulphur (or a sulphur donor agent) and a primary vulcanization accelerator. Various known secondary accelerators or vulcanization activators may be added to this basic vulcanization system.
The rubber composition of the sheath according to the invention may comprise, in addition to the said crosslinking system, all the customary ingredients that can be used in rubber compositions for tires, such as reinforcing fillers based on carbon black and/or on an inorganic reinforcing filler such as silica, antiageing agents, for example antioxidants, extension oils, plasticizers or agents that improve the workability of the compositions in the raw state, methylene acceptors and donors, resins, bismaleimides, known adhesion promoting systems of the “RFS” (resorcinol-formaldehyde-silica) type or metal salts, notably cobalt salts.
By way of preference, the composition of this sheath is chosen to be identical to the composition used for the skim layer of the working crown layer that the cords are intended to reinforce. Thus, there is no problem of potential incompatibility between the respective materials of the sheath and of the rubber matrix.
According to an alternative form of the invention, the said cords of at least one working crown layer are cords of ┌L+M┐ layer construction, comprising a first layer C1 of L threads of diameter di wound together in a helix at a pitch p1 with L ranging from 1 to 4, surrounded by at least one intermediate layer C2 of M threads of diameter d2 wound together in a helix at a pitch p2 with M ranging from 3 to 12, a sheath made of a noncrosslinkable, crosslinkable or crosslinked rubber composition based on at least one diene elastomer covering, in the construction, the said first layer C1.
For preference, the diameter of the threads of the first layer of the internal layer (C1) is comprised between 0.10 and 0.5 mm and the diameter of the threads of the external layer (C2) is comprised between 0.10 and 0.5 mm.
For preference also, the pitch of the helix at which the said threads of the external layer (C2) are wound is comprised between 8 and 25 mm.
Within the meaning of the invention, the helix pitch represents the length, measured parallel to the axis of the cord, after which a thread of this pitch has effected a complete turn about the axis of the cord; thus, if the axis is sectioned on two planes perpendicular to the said axis and separated by a length equal to the pitch of a thread of a layer of which the cord is made, the axis of this thread in these two planes occupies the same position on the two circles corresponding to the layer of the thread considered.
Advantageously, the cord is ascertained to have one, or even more preferably, all, of the following characteristics:
Preferably, the rubber sheath has a mean thickness ranging from 0.010 mm to 0.040 mm.
In general, the said cords according to the invention can be produced using any type of metal thread, notably made of steel, for example threads made of carbon steel and/or threads of stainless steel. Use is preferably made of carbon steel but it is, of course, possible to use other steels or other alloys.
Where a carbon steel is used, its carbon content (% by weight of steel) is preferably comprised between 0.1% and 1.2%, more preferably from 0.4% to 1.0%; these contents represent a good compromise between the mechanical properties required for the tire and the workability of the thread. It should be noted that a carbon content of between 0.5% and 0.6% ultimately makes such steels less expensive because they become easier to draw. Another advantageous embodiment of the invention can also consist, depending on the applications targeted, in using steels having a low carbon content, for example of between 0.2% and 0.5%, due in particular to a lower cost and to a greater ease of drawing.
The said cords according to the invention may be obtained using various techniques known to those skilled in the art, for example in two steps, first of all by sheathing the core or layer C1 using an extrusion head, which step is followed in a second stage by a final operation of cabling or twisting the remaining M threads (layer C2) around the layer C1 thus sheathed. The problem of bonding in the raw state posed by the rubber sheath during the optional intermediate winding and unwinding operations can be solved in a way known to a person skilled in the art, for example by the use of an interposed plastic film.
Such cords of at least one working crown layer are, for example, selected from the cords described in patent applications WO 2006/013077 and WO 2009/083212.
According to an advantageous alternative form of the invention, the layer of circumferential reinforcing elements has an axial width greater than 0.5 xS.
S 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 layers of reinforcing elements are measured on a cross section of a tire, the tire therefore being in an uninflated state.
According to a preferred embodiment of the invention, at least two working crown layers having different axial widths, the difference between the axial width of the axially widest working crown layer and the axial width of the axially least-wide working crown layer is comprised between 10 and 30 mm
According to a preferred embodiment of the invention, the layer of circumferential reinforcing elements is placed radially between two working crown layers.
According to this embodiment of the invention, the layer of circumferential reinforcing elements makes it possible to limit more significantly the extent to which the reinforcing elements of the carcass reinforcement are placed under compression than a similar layer placed radially on the outside of the working layers is able to achieve. It is preferably separated radially from the carcass reinforcement by at least one working layer so as to limit the stress loadings on the said reinforcing elements and avoid excessively fatiguing them.
Advantageously too according to the invention, the axial widths of the working crown layers radially adjacent to the layer of circumferential reinforcing elements are greater than the axial width of the said layer of circumferential reinforcing elements and, for preference, the said working crown layers adjacent to the layer of circumferential reinforcing elements are, on either side of the equatorial plane and in the immediate axial continuation of the layer of circumferential reinforcing elements, coupled over an axial width and then decoupled by the said layer of rubber compound C at least over the remainder of the width that the said two working layers have in common.
The presence of such couplings between the working crown layers adjacent to the layer of circumferential reinforcing elements allow a reduction in the tensile stresses acting on the axially outermost circumferential elements situated closest to the coupling.
According to one advantageous embodiment of the invention, the reinforcing elements of at least one layer of circumferential reinforcing elements are metallic reinforcing elements having a secant modulus at 0.7% elongation comprised between 10 and 120 GPa and a maximum tangent modulus of less than 150 GPa.
According to a preferred embodiment, the secant modulus of the reinforcing elements of 0.7% elongation is less than 100 GPa and greater than 20 GPa, preferably comprised between 30 and 90 GPa and more preferably still, less than 80 GPa.
Also preferably, the maximum tangent modulus of the reinforcing elements is less than 130 GPa and more preferably less than 120 GPa.
The modulus values expressed hereinabove are measured on a curve of tensile stress as a function of elongation determined with a preload of 20 MPa, divided by the cross section of metal of the reinforcing element, the tensile stress corresponding to a measured tension divided by the cross section of metal of the reinforcing element.
The modulus values for the same reinforcing elements may be measured from a curve of tensile stress as a function of elongation which is determined with a preload of 10 MPa divided by the overall cross section of the reinforcing element, the tensile stress corresponding to a measured tension divided by the overall cross section of the reinforcing element. The overall cross section of the reinforcing element is the cross section of a composite element made up of metal and of rubber, the latter notably having penetrated the reinforcing element during the tire curing phase.
According to this formulation relating to the overall cross section of the reinforcing element, the reinforcing elements of the axially outer parts and of the central part of at least one layer of circumferential reinforcing elements are metallic reinforcing elements having a secant modulus of 0.7% elongation comprised between 5 and 60 GPa and a maximum tangent modulus of less than 75 GPa.
According to one preferred embodiment, the secant modulus of the reinforcing elements at 0.7% elongation is less than 50 GPa and greater than 10 GPa, preferably comprised between 15 and 45 GPa, and more preferably still, less than 40 GPa.
Also preferably, the maximum tangent modulus of the reinforcing elements is less than 65 GPa and more preferably less than 60 GPa.
According to one preferred embodiment, the reinforcing elements of at least one layer of circumferential reinforcing elements are metallic reinforcing elements having a curve of tensile stress as a function of relative elongation that has shallow gradients for small elongations and a substantially constant and steep gradient for greater elongations. Such reinforcing elements of the additional ply are normally known as “bimodulus” elements.
According to a preferred embodiment of the invention, the substantially constant and steep gradient appears upwards of a relative elongation of between 0.1% and 0.5%.
The various characteristics of the reinforcing elements mentioned above are measured on reinforcing elements taken from tires.
Reinforcing elements more particularly suited to the creation of at least one layer of circumferential reinforcing elements according to the invention are, for example, assemblies of formula 21.23, the makeup of which is 3×(0.26+6×0.23) 4.4/6.6 SS; this stranded cord being made up of 21 elementary threads of formula 3×(1+6), with 3 strands twisted together, each one made up of 7 threads, one thread forming a central core of a diameter equal to 26/100 mm, and 6 wound threads of a diameter equal to 23/100 mm Such a cord has a secant modulus of 0.7% equal to 45 GPa and a maximum tangent modulus equal to 98 GPa, these being measured on a curve of tensile stress as a function of elongation determined with a preload of 20 MPa divided by the cross section of metal of the reinforcing element, the tensile stress corresponding to a measured tension divided by the cross section of metal of the reinforcing element. On a curve of tensile stress as a function of elongation determined with a preload of 10 MPa divided by the overall cross section of the reinforcing element, the tensile stress corresponding to a measured tension divided by the overall cross section of the reinforcing element, this cord of formula 21.23 has a secant modulus of 0.7% equal to 23 GPa and a maximum tangent modulus equal to 49 GPa.
In the same way, another example of reinforcing elements is an assembly of formula 21.28, the construction of which is 3×(0.32+6×0.28) 6.2/9.3 SS. This cord has a secant modulus at 0.7% equal to 56 GPa and a maximum tangent modulus equal to 102 GPa, these measured on a curve of tensile stress as a function of elongation determined with a preload of 20 MPa divided by the cross section of metal of the reinforcing element, the tensile stress corresponding to a measured tension divided by the cross section of metal of the reinforcing element. On a curve of tensile stress as a function of elongation determined with a preload of 10 MPa divided by the overall cross section of the reinforcing element, the tensile stress corresponding to a measured tension divided by the overall cross section of the reinforcing element, this cord of formula 21.28 has a secant modulus of 0.7% equal to 27 GPa and a maximum tangent modulus equal to 49 GPa.
The use of such reinforcing elements in at least one layer of circumferential reinforcing elements notably makes it possible to maintain satisfactory stiffnesses of the layer even after the shaping and curing stages in conventional manufacturing methods.
According to a second embodiment of the invention, the circumferential reinforcing elements may be formed of metallic elements that are inextensible and cut in such a way as to form portions of a length very much less than the circumference of the least-long layer, but preferably greater than 0.1 times the said circumference, the cuts between portions being axially offset from one another. Preferably again, the tensile modulus of elasticity per unit of 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, in a simple way, to confer upon the layer of circumferential reinforcing elements a modulus that can easily be adjusted (by means of the choice of spacings between portions of the same row) but that is in all cases lower than the modulus of the layer made up of the same metallic elements but continuous, the modulus of the additional layer being measured on a vulcanized layer of cut elements, taken from the tire.
According to a third embodiment of the invention, the circumferential reinforcing elements are wavy metallic elements the ratio a/λ of the amplitude of the waves to the wavelength being at most equal to 0.09. 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.
The metallic elements are preferably steel cords.
According to a preferred embodiment of the invention, the reinforcing elements of the working crown layers are inextensible metal cords.
The invention also advantageously, in order to reduce the tensile stresses acting on the axially outermost circumferential elements, plans for the angle formed with the circumferential direction by the reinforcing elements of the working crown layers to be less than 30° and preferably less than 25°.
One preferred embodiment of the invention also provides for the crown reinforcement to be supplemented radially on the outside by at least one additional layer, referred to as a protective layer, of reinforcing elements, referred to as elastic reinforcing elements, that are oriented with respect to the circumferential direction at an angle of between 10° and 45° and in the same direction as the angle formed by the elements of the working layer radially adjacent to it.
The protective layer may have an axial width less than the axial width of the least-wide working layer. The said protective layer can also have an axial width greater than the axial width of the narrowest working layer, such that it overlaps the edges of the narrowest working layer and, when it is the layer radially above which is narrowest, such that it is coupled, in the axial extension of the additional reinforcement, with the widest working crown layer over an axial width in order thereafter, axially on the outside, to be decoupled from the said widest working layer by profiled elements having a thickness at least equal to 2 mm The protective layer formed of elastic reinforcing elements can, in the abovementioned case, on the one hand be optionally decoupled from the edges of the said narrowest working layer by profiled elements having a thickness substantially less than the thickness of the profiled elements separating the edges of the two working layers and, on the other hand, have an axial width less than or greater than the axial width of the widest crown layer.
According to any one of the embodiments of the invention mentioned above, the crown reinforcement may furthermore be supplemented, radially on the inside between the carcass reinforcement and the radially internal working layer closest to said carcass reinforcement, by a triangulation layer made of metal inextensible reinforcing elements that are made of steel and form, with the circumferential direction, an angle of more than 60° and in the same direction as the angle formed by the reinforcing elements of the radially closest layer of the carcass reinforcement.
The tire according to the invention as has just been described therefore has a rolling resistance that is an improvement on conventional tires and improved cornering stiffness properties and therefore heightened performance in terms of endurance irrespective of the running conditions.
Further details and advantageous features of the invention will become apparent hereinafter from the description of exemplary embodiments of the invention, with reference to
In order to make them easier to understand, the figures are not shown to scale. The figures depict only half a view of a tire which extends symmetrically with respect to the axis XX' that represents the circumferential meridian plane, or equatorial plane, of a tire.
In
The crown reinforcement is itself capped by a tread 5.
The maximum axial width S of the tire is equal to 317 mm.
The axial width L41 of the first working layer 41 is equal to 252 mm.
The axial width L43 of the second working layer 43 is equal to 232 mm The difference between the widths L41 and L43 is equal to 15 mm.
As for the axial width L42 of the layer of circumferential reinforcing elements 42, this is equal to 194 mm.
The last crown ply 44, referred to as the protective ply, has a width L44 equal to 124 mm.
A layer of rubber compound C is also present for decoupling the ends of the working crown layers 41 and 43.
The zone of engagement of the layer C between the two working crown layers 41 and 43 is defined by its thickness or, more precisely, the radial distance d between the end of the layer 43 and the layer 41 and by the axial width D of the layer C comprised between the axially inner end of the said layer C and the end of the radially outer working crown layer 43.
According to the invention, a first layer S of rubber compound is placed between the carcass reinforcement 2 and the first working layer 41.
In
In
The diameter of the circumferential reinforcing elements of the layer 42 is equal to 1.35 mm The distance d is therefore equal to 1.48 times the diameter φ of these elements.
Tests have been conducted with various tires produced according to the invention as depicted in
Tests have notably been performed by varying the characteristics of the skim compounds of the working layers 41 and 43, notably their elastic modulus values under tension at 10% elongation and the tan(δ)max value and the characteristics of the compounds of the layer S, notably the complex dynamic shear modulus G*, measured at 10% and 60° C. on the return cycle.
Still further tests have been performed by varying the shape and dimensions of the layer C.
The various compounds used are listed below.
The values for the constituent ingredients are expressed in phr (parts by weight per hundred parts of elastomer).
Various reference tires were tested.
First reference tires T1 have working layers of which the skims are made of the compound R1, a layer C as depicted in
Second reference tires T2 have working layers of which the skims are made of the compound 1, a layer C as depicted in
Third reference tires T3 have working layers of which the skims are made of the compound 1, a layer C as depicted in
Various tires according to the invention were tested.
First tires Si according to the invention have working layers of which the skims are made of the compound 1, a layer C as depicted in
Second tires S2 according to the invention have working layers of which the skims are made of the compound 1, a layer C as depicted in
First endurance tests were run on a test machine that forced each of the tires to run in a straight line at a speed equal to the maximum speed rating prescribed for the said tire (the speed index) under an initial load of 4000 kg progressively increased in order to reduce the duration of the test.
It was found that all the tires tested exhibited substantially comparable results.
Other endurance tests were conducted on a test machine that cyclically imposed a transverse loading and a dynamic overload on the tires. The tests were carried out for the tires according to the invention under conditions identical to those applied to the reference tires.
The distances covered varied from one type of tire to another, failures occurring as a result of degradation of the rubber compounds at the ends of the working layers. The results are set out in the table which follows with reference to a base 100 fixed for the reference tire T1.
Moreover, rolling resistance measurements were taken. These measurements applied to all of the tires described hereinabove.
The results of the measurements are given in the table below: they are expressed in kg/t, a value of 100 being assigned to the tire T1.
| Number | Date | Country | Kind |
|---|---|---|---|
| 1455965 | Jun 2014 | FR | national |
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/EP2015/061713 | 5/27/2015 | WO | 00 |
