CA1296982C - High performance tire - Google Patents

Abstract

ABSTRACT
A pneumatic tire characterized in that: a tread is divided into a crown portion having a width corresponding to about 30% to 65% of the tread width and two shoulder portions by at least two longitudinal grooves extending in substantially zigzag or wavy line; the crown portion is provided with one or more central ribs or central block rows; each shoulder portion is provided with one or more outer ribs or outer blocks; and the rib or blocks on shoulder portions are provided with a plurality of narrow cut grooves so that the circumferential stiffness index of the pattern and a volume index of the narrow cut grooves my be set at 30 to 70 and 2.5 to 15, respectively.

Description

1~9698;Z

, HIGH PERFORMANCE TYRE
-This invention relates to a pneumatic radial ply tyre and, in particular, a radial tyre suitable for use for truck, bus, light truck and other vehicles, and is mainly intended to provide improved high speed durability of such tyres without sacrificing wear life, and at the same time, to improve the maneuverability and the ride.

The high speed durability of a tyre is mainly affected by the structure, the profile and the material used for the tyre. First of all, in the structure, a cross ply or bias tyre comprises a carcass composed of a plurality of rubberized ply layers each containing fibre cords embedded therein, the cords of one ply being crossed with respect to the next ply at an angle of 40 to 25 with respect to the equatorial line of the tyre. In one example, the carcass of a cross ply tyre for a truck or bus is composed of several ply layers of virtually unwoven fabric, each ply of which being superimposed with one another.

Secondly the structure of a radial ply tyre comprises a carcass of a substantially radial construction composed of one ply layer containing steel cords embedded therein and turned up around a pair of bead cores and a belt layer composed of 3 to 4 ply layers each containing steel cords embedded therein, said cords of which being crossed with one another at an angle of 15 to 70 with respect to the equatorial line of the tyre and superimposed about said carcass ply beneath the tread to provide a strong belt effect.

Astheresultofsuch construction~ a radial ply tyre has a tread with high stiffness and less movement of tread rubber, which leads to high resistance to wear of the tread rubber, and by the same reason as mentioned above, the heat generation and the rolling resistance are also very good.

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lZ96982 On the contrary, in the case of bias ply construction tyres with a carcass composed of several ply layers superimposed on one another and a belt layer composed of several ply layers, each ply of which has its cords crossed with respect to the adjacent ply and disposed between the said carcass and the tread rubber.

hs the result, the carcass of bias ply tyres is substantially thicker than the carcass of radial tyres and the movement of tread rubber, while a tyre is in contact with ground, is larger than that of radial ply tyre because of the carcass ply construction of textile cords having low stiffness as compared with steel cords.

Further, a carcass and a belt layer has to deform together and this causes variation of the cord angles under load which is the so-called pantographic movement, which leads to increased heat generation and to lower resistance to wear because of the large movement of rubber. This also increases the rolling resistance. These character-istics are summarized in Table 1.

Table 1 Comparison of Performance Between Bias and Radial Tyre Usage Performance Bias Radial (Index) Tyre Tyre Tyres for Tread Wear Resistance 100150-200 Truck and Bus Rolling Resistance (70 km/h) 100 68-72 10.00-20 Fuel Comsumption 100 88-92 10.00 R 20 Heat Generation at Shoulder under High Speed Travelling 100 40-SO

From Table 1 lt can be seen that a radial construction is one which can display its ability under high speed travelling on a good paved road.

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Next, concerning the profile of a tyre, which is generally expressed by the so called aspect ratio, that is, the ratio of the section height to the section width.

The merits of low profile tyres are such that the cornering power is increased by the increase in the lateral stiffness with the increase of overall tyre width due to the adoption of low profile (see Fig lOa~.
Accordingly, the maneuverability of the vehicles is improved together with a decrease in the energy loss brought about by decreasing of the radial deflection of such tyres which leads to a decrease of heat generation and rolling resistance. Accordingly, the durability for high speed running and the fuel consumption are improved (see Fig lOb).

Next, taking consideration of high speed durability from the stand point of material used for the tyre construction, the factors which mainly affect the tyre performance are the tread rubber compound and the cord material of tyres. With regard to the rubber compound for the tread, the material suitable for the tread must be well-balanced with respect to the performances of not only heat generation but also the resistance to wear and cut. As is well known, polybutadiene rubber (BR) and nature rubber are superior to SBR in heat generation and the larger the particle of carbon black as filler for reinforcement the lower the heat generation. It is also known that when the volume of carbon black filler in the rubber compound increases, the heat generation increases. As to the heat resistance of the cord materials for the carcass, it is known that steel cords show the best perfor-mance in the order of steel, polyester, nylon and rayon.

As will be understood from the summary above, research works for the betterment of high speed running durability of tyres have resulted in big range switching over in tyre construction, from bias to radial, from normal aspect ratio tyres to low profile tyres, from rayon to nylon, from nylon to polyester and from polyester to steel which has caused a big advancement of the high speed durability in accordance with these changes.

lZ9~9~2 However, lately with the remarkable improvement of road situations such as the development of expressway networks and the like, the chances to drive at high speed have increased and the demand for tyres having long life has become more conspicuous for economic reasons. However, according to the prior art of tyre design, the high speed performance has been increased only with sacrificing the wear life. Alternatively in the prior art the wear life has only been increased with a sacrifice in the high speed performance.
Hitherto in both there has only been such antinomic design activity in tyres.

For example, in order to increase the durability at high speed, the thickness of the tread has been designed to be as thin as possible to decrease the heat generation. Accordingly, the wear life of such tyres become short as an inevitable consequence.

However, the users of tyres cannot be satisfied with such unbalanced tyre performance for any length of time, the requirement for well balanced tyre properties, which give a long life and an improved high speed durability has become conspicuous of late.

That is, it is required to increase the durability of such tyres together with an increase in the depth of longitudinal main grooves and the thickness of the tread.

As above mentioned the prior art is unable to provide so well balanced an improvement with simultaneous increase in the durability at high speed and resistance to wear (long life).

However, the inventors of the present invention have made various investigations into tread patterns which can decrease the heat generation of tyre as well as being superior in the resistance wear.

¦ Generally, it is known that the temperature generated, while a tyre is in rotation, is highest at both shoulder parts of the tyre. The inventor of this invention, selected for investigation seven items 1;~9~

such as a ratio between surface area of cut grooves at the shoulder parts, shape index (cross sectiona1 area of loaded tyre/free surface area), pattern transverse stiffness, pattern circumferential stiffness, volume of cut groove, shoulder gauge and tread radius as factors of temperature rise and examined the correlation between temperature and the above factors using multiple regression analysis. He discovered that "volume of cut groove" and "pattern circumferential stiffness" greatly contribute to temperature rise.

Accordingly the present invention provides a pneumatic tyre in which the rubber surface of the tyre tread is divided by at least two longitudinal main grooves extending in the circumferential direction of the tyre in the pattern of zigzag or wavy line to provide a tread crown part having a width corresponding to about 30 to 65% of the tread width and centering at the equatorial plane of the tyre and tread shoulder parts lying on either side of the said tread crown part, one or more central ribs or rows of central blocks comprising blocks of various shapes are provided in the said crown part and outer ribs or outer rows of blocks in both shoulder parts, a plurality of narrow cut grooves extending in the axial direction of the tyre being provided for ribs or blocks on both said shoulder parts to provide a circumferential stiffness index of the pattern and a volume index of the cut groove of 30 to 70 and 2.5 to 15, respectively.

~definitionsof"pattern stiffness" and "volume index" of the cut groove are as follows:-Pattern stiffness index In said shoulder parts, pattern stiffness which is pattern stiffnessin contact length with ground under specified load and inner pressure, is defined by below equations.

kp = F = 1/( h + h) ... ..
y 3EI AG

~29~;~t32 kp: pattern stiffness (kg/mm) F: tangential ~orce at grounding surface (kg) y: variation of pattern (mm) h: pattern depth (mm) E: elastic modulus at elongation of tread rubber (kg/mm2) G: shearing modulus (=E/3 (kg/mm2) I: secondary moment at block section (mm4) I = ab3/12 in the block shown in Fig 11 A: sectional area of block (mm2) In the case of actual pattern, the pattern depth is different from the hl of cut groove in the shoulder parts and several number of blocks are adopted, so it is treated follow, the pattern stiffness at tread surface, Kps = Kpsl + Kps2 + ... + Kpsn to use h = hl in equation ~

the pattern stiffness (KpB) at base tread part is to use h = hO - hl (Fig 1) in equation the total pattern stiffness KpT

KpT = 1/ ( Kps KPB

the pattern stiffness Kpo in the case of no subgroove is to use h = ho in equation ~
KPT
25 circumferential stiffness index of the pattern = x 100 Kpo Volume index of the cut groove The ratio of the volume of groove to total volume of shoulder part.

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, ~olume of index volume of cut grooves in shoulder part surface area of shoulder part X pattern depth Some examples of the inven~tion a~d~th~e ~r~ior art will now be described A~ in conjunction with the~drawings~ in which:-Fig 1 is a developed plan view of a tread pattern having a series ofcut grooves in the shoulder parts according to the present invention;

Fig 2 is a developed plan view of a tread pattern having a series of lateral grooves in the shoulder parts according to the prior art;

Fig 3a is a developed plan view of a prior art tread pattern in which the index of groove volume is out of the scope of the present invention;

Fig 3b is a developed plan view of a tread pattern described as No 4 pattern in Fig 7 and Fig 8.

Fig 4 is a graph showing the relation of rubber gauge with heat generation at the shoulder part for the tread pattern of example 1 (Fig 1) according to the present invention, that of control example (shown in Fig 2 and Fig 3), of the conventional tyre;

Fig 5 is a graph showing the relation between pattern circumferential stiffness and temperature in the shoulder part;

Fig 6 is a graph showing the relation between volumes of cut grooves and temperature;
Fig 7 is a graph showing the relation between transverse stiffness and circumferential stiffness;
Fig 8 is a graph showing the relation between transverse stiffness 2S and temperature at the shoulder parts;
Fig 9 is a graph showing the relation between pattern stiffness and volume of groove;

Fig lOa is a graph showing the relation between cornering power and the aspect ratio of a tyre;

Fig lOb is a graph showing the relation between rolling resistance and the aspect ratio;

Fi~ 11 is a view of block sample for describing the secondary mount of the stiffness index at the section of block;

Fig 12 is a developed plane view of another embodiment of tread pattern according to the present invention.

As shown in Fig 1 the tread 1 comprises a crown part CR defined by two main longitudinal grooves Gl/G2 having deepest depth extending in the circumferential direction of the tyre and centered about the equatorial plane C of the tyre so as to be spaced laterally by 30 to 65% of the tread width TW. The crown part CR also includes at both sides circumferentially extending longitudinal narrower grooves 91 and 92 and sub-grooves m and n extending between the longitudinal main grooves Gl, G2 and between the main groove Gl, G2 and the narrow groove 9l, 92 to communicate with each other so as to form rows of blocks Bl, B2 and 83 in the crown part, each row of blocks being approximately parallelogrammatic blocks B.

The shoulders S H of the tyre tread lie outside the main grooves Gl and G2 and include a plurality of cuts S in the circumferential direction of the tyre at equal pitches P of 15 mm and at inclination angle c~ of 30 degrees with respect to the equatorial plane of the tyre. The width t and depth hl of the cuts S are 2 mm and 13 mm respectively and the depth hO of the longitudinal main grooves Gl and G2 is to be that of extra heavy tread type. For example, a depth ranging from 16.6 mm to 20.6 mm is adopted to the tyre of 10.00 R 20 in size. In the present example, a depth is set at 18.00 mm. A width GW of the groove G in the U-shape at cross section A2 - A2 is 14.5 mm. A longitudinal narrow groove g is 18 mm depth and 9.5 mm width, a sub-groove m is 5 mm width and 11 m depth; and another sub-groove n is 2 mm width and 9 mm depth. In the example No 1 shown in Fig 1 the pattern stiffness index and cut groove volume index are 64 and 10.5 respectively.

On the other hand, control examples 1 and 2 according to the prior art were made for trial. The specifications of test samples are listed in Table 4.

All above said test samples were 10.00 R 20 14 PR in si~e and tyre construction except for the tread pattern and the component materials were of the same specification.

Table 4 Control Control Example 1 example 2 example 1 Depth of cut at shoulder part (mm) 13 18 5.5 Width of cut at shoulder part (mm) 2 10 11.5 Ratio of cut surface area at shoulder part I 0.19 0.38 0.18 Shape index i at shoulder part I 0.44 0.34 0.72 Pattern transverse stiffness at shoulder part (kg/mm)- 18.6 8.8 52.7 Pattern circumferential stiffness 15.6 7.7 53.8 at shoulder part (kg/mm) (64) (38) (94) Volume of cut 4.160 14.400 1.898 at shoulder part (cm3) (10.5) (36.4) (4.8) Thickness of rubber at shoulder part (mm) ¦ 23.9 24.6 23.5 Tread radius of curvature at 100% air pressure (mm) l585 585 585 Tread pattern iFig 1 Fig 3a Fig 2 The numeral in parenthesis, ( ), indicates an index.

lZ969~3Z

From these results various conclusions may be drawn. To begin with Fig 5 graphically shows the relation between pattern circumferential stiffness at the shoulder part and temperature, wherein the lower the circumferential stiffness, the lower the temperature at the shoulder part. Fig 6 shows a relation between the volume of cut groove and temperature, wherein the larger the volume of cut groove, the lower the temperature, but as regards an embodiment of this invention, it can be fully understood that even when the volume of cut groove is equal to that of the conventional tyre, a temperature is nearly 20C lower than that in the conventional tyre. A comparison of transverse stiffness with circumferential one of a pattern indicates that, as shown in Fig 8, a temperature in the pattern No 4 having transverse stiffness lower than circumferential stiffness as shown in Fig 7 is 111C, degrees which is not low at all.

Incidentally, circumferential stiffness per pitch in the pattern No 4 was 44.0 whereas transverse stiffness was 25.2. From the above fact, it has been shown that lowering of temperature must depend on a reduction of circumferential stiffness rather than transverse one.

Fig 4 graphically shows that the relation between the tread gauge at the shoulder parts and temperature in the tyre, wherein a temperature rises with the increase in tread gauge in conventional tyre but, in the embodiment of this invention (Fig 1), despite the shoulder gauge of 23.8 mm, the temperature of the tyre is as low as that of the conventional tyre having the tread gauge of 18 to 19 mm.

It is supposed that lowering of stiffness of the pattern depending on pattern effect leads to decrease in resistance of the tyre to wear. However, in this respect, Fig 9 shows that values of pattern stiffness of tyres shown in Fig 1 and Fig 3~are 15.6 and 7.7 respectively, that is 1:0.5 in terms of ratio, and volumes of cut grooves are 4.16 cm3 and 14.4 cm3 respectively, that is 1:3.5 in ratio. In the pattern shown in Fig 1 the volume of groove is small in proportion to pattern stiffness tFig 9) as compared with that shown in Fig 3a. That is to say, it has been found that when reducing pattern stiffness, resistance to wear is reduced with the increase in volume of the cut groove and, therefore, by setting narrow the width t of cut in the shoulder part as in the pattern shown in Fig 1, control over temperature rise and prevention of decrease in resistance to wear are ensured. An appropriate width t of a cut S is from 0.5 to 5 mm, more preferably from 1 to 3 mm.
A volume index of the cut is preferably within the range from 2.5 to 15. An index exceeding 16 results in too large volume of the cut which accelerates wear of rubber and further unfavourably generates noise or collects pebbles. On the other hand, too small an index not exceeding 2.4 degrades wet grip and causes resultant problems in safety of vehicles. An index of circumferential stiffness is preferably from 30 to 70 but because when being low such as not greater than 29, causes the rubber block to tend to chip off and, being 71 or higher, invites problem in generation of heat. Provision of a plurality of cut grooves for adapting the circumferential stiffness index to range from 30 to 70 improves ground contacting performance of the tread and reduces the wear of tyre occurring during slippage, thereby the so-called shoulder wear being markedly eliminated.

The test of durability to high speed running for the said sample tyres was performed according to the following method and the results thereof are shown in Table 5.

Table 5 . . _ .
Breaking speed : length of time of running Example 1 130 km/h : 60 minutes to fail Control example 1 100 km/h : 50 minutes to fail Control example 2 130 km/h : 110 minutes to fail 1'~9~i98Z

Tyres were driven on the drum type running tester according to the stepped speed running method on conditions that:

Load : 3.780 kg Initial internal pressure : 7.25 kgf/cm Rim : 7.50 v wherein results were evaluated by the level of speed at which the tyre failed due to heat generation and the length of time for running at the above speed. The tyre of Example 1 according to the present invention cleared a speed of 130 kg/h, but the tyre of Control example 1 which attached much importance to the resistance to wear, could clear only 100 km/h. The tyre of Control example 2 which sacrificed resistance to wear, cleared a speed of 130 km/h because of lower heat generation due to reduced pattern circumferential stiffness. The tyre according to the present invention designed to be provided with "cut grooves" on the shoulder zones for reducing pattern circumferential stiffness, controlled heat generation of durability.

As regards resistance of the tread to wear, comparison tests using a truck were performed and amounts of wear of tread rubber per 1,000 km running were compared by measurements of remaining groove depth after 50,000 km running. As shown in Table 6, a tyre (Example 1) according to the present invention demonstrated an excellent resistance to wear by the contribution of heat generation to a low degree as above described, more uniform distribution of ground contact pressure and high grip performance.

Table 6 Index of Wear of Tread Rubber Control example 1 100 Control example 2 80 Example 1 105 3 ~

* Note : The larger the index number, the better the resistance to wear.
The above index number may be regarded as a ratio between wear life span of treads.

Values obtained from comparison of wet grip performances are shown in Table 7.

Table 7 Wet Grip Performance Control Control Example 1 example 1 example 2 Index of wet grip 100 110 115 Wet grip performances were observed by confirming braking distances travelled by a truck driven at a speed of 80 km/h on an asphalt-paved wet road and indicated in terms of index on the assumption that the index of braking distance of Control example 1 is 100.
In this case too, the larger the index number the better the performance and the tyre (Example 1) according to the present invention which exhibited a strong braking force was verified to be excellent in wet grip performance as one of important requirements for safety of a truck.

Thus, as has been described, the invention provides a well balanced tyre in which a plurality of narrow cut are disposed on both shoulder parts, where the heat generation is most remarkably low for a tyre.
The low heat generation is by means of decreasing the pattern stiffness so that the high speed durability is improved in spite of the extra heavy tread with deepest longitudinal main grooves and wear life of tread, wandering performance including wet grip performance, ride feeling and handling stability can simultaneously and effectively improved in well-balanced manner.

Claims (13)

1. A pneumatic radial tire having a tread pattern com-prising a tread crown portion of a width of 30 to 65% of the tread width separated from two shoulder parts one on either side of the tread crown portion by two main longitudinal grooves extending circumferentially in a zigzag or wavy line, the tread crown being provided with one or more central ribs or central rows of blocks and both tread shoulder parts comprising a rib or row of blocks having a plurality of narrow cut grooves extending in the direction of the axis of the tire or an acute angle to said axial direction such that the circumferential stiffness index of the pattern and the volume index of the narrow cut grooves are in the ranges of 30 to 70 and 2.5 to 15, respec-tively.

2. A tire according to claim 1, in which the narrow cut grooves extend at an angle to the axial direction of 30°.

3. A tire according to claim 2, in which the narrow cut grooves are spaced apart around the tire at a pitch of 15 mm.

4. A tire according to claim 1, 2 or 3, in which the narrow cut grooves have a width in the range of 0.5 to 5 mm.

5. A tire according to claim 1, 2 or 3, in which the pattern depth is in the range of 16.6 to 20.6 mm.

6. A tire according to claim 1, 2 or 3, in which the main grooves are of V-shaped cross-section and have width of 14.5 mm.

7. A tire according to claim 1, 2 or 3, in which the crown portion comprises tread blocks separated by longitudinal narrow grooves 9.5 nun wide and 18.0 mm deep and transverse narrow grooves 5 mm wide, 11 mm deep and 2 nun wide and 9 mm deep, respectively.

8. A tire according to claim 7, having a pattern stiffness index and cut groove volume index of 64 and 10.5, respectively.

9. A pneumatic radial tire comprising a tread provided with at least two longitudinal main grooves extending circumferentially in a substantially zigzag or wavy line to divide the tread width into two tread shoulder parts and a tread crown part therebetween, said crown part having a width of about 30 to 65% of the tread width; each tread shoulder part having a plurality of generally axially extending narrow grooves to form circumferentially substantially separated blocks; the width of the narrow grooves being in a range of 0.5 to 5 mm and said narrow grooves having a volume index in a range of 2.5 to 15; each shoulder part having a circumferential stiffness index in a range of 30 to 70;
wherein the circumferential stiffness index in the shoulder part and the volume index of the narrow grooves are defined as follows:
the Volume Index = V/(SXd)X100 wherein:
V = total volume of the cut grooves in the shoulder part S = surface area of the shoulder part d = depth of the longitudinal main groove the circumferential stiffness Index = (Kpt/Kpo)X100 wherein:
Kpt = circumferential stiffness in the shoulder part after the narrow grooves are provided Kpo = circumferential stiffness in the shoulder part before the narrow grooves are provided Circumferential Stiffness = F/y wherein:
F = tangential force in the circumferential direction of the tire at the ground contacting surface of the shoulder part y = variation of the ground contacting surface in the circumferential direction of the tire.

10. A pneumatic radial tire as claimed in claim 9 wherein the tread crown part is provided with a plurality of rows of blocks.

11. A pneumatic radial tire as claimed in claim 9 wherein the tread crown part is provided with at least one rib.

12. A pneumatic radial tire as claimed in claim 9 wherein the narrow grooves are shallower than the longitudinal main grooves.

13. A pneumatic radial tire as claimed in claim 1 wherein the narrow grooves are inclined at an angle to the axial direction of the tire.