Pneumatic tire having a zigzag center main groove and shoulder oblique grooves
10071601 ยท 2018-09-11
Assignee
Inventors
Cpc classification
B60C11/1236
PERFORMING OPERATIONS; TRANSPORTING
B60C2011/0374
PERFORMING OPERATIONS; TRANSPORTING
B60C2011/1254
PERFORMING OPERATIONS; TRANSPORTING
B60C2011/0344
PERFORMING OPERATIONS; TRANSPORTING
B60C11/13
PERFORMING OPERATIONS; TRANSPORTING
B60C2011/1213
PERFORMING OPERATIONS; TRANSPORTING
B60C2011/0372
PERFORMING OPERATIONS; TRANSPORTING
B60C2011/0395
PERFORMING OPERATIONS; TRANSPORTING
B60C2011/0348
PERFORMING OPERATIONS; TRANSPORTING
International classification
B60C11/11
PERFORMING OPERATIONS; TRANSPORTING
B60C11/12
PERFORMING OPERATIONS; TRANSPORTING
B60C11/13
PERFORMING OPERATIONS; TRANSPORTING
Abstract
Each shoulder land region 4E defined by a shoulder circumferential main groove 3E is provided with a circumferential narrow groove 20 and axially inner and outer shoulder oblique grooves 22 and 21 extending therefrom. The axially outer shoulder oblique grooves 21 are inclined with respect to the tire axial direction to one direction. The axially inner shoulder oblique grooves 22 are inclined with respect to the tire axial direction to one direction opposite to that of the axially outer shoulder oblique grooves 21. Crown oblique grooves 8 are inclined with respect to the tire axial direction to one direction same as that of the axially outer shoulder oblique grooves 21. Imaginary extensions 21K of the axially outer shoulder oblique grooves 21 are not overlapped with openings Q1 of the axially inner shoulder oblique grooves 22 at the circumferential narrow groove 20. Imaginary extensions 22K of the axially inner shoulder oblique grooves 22 are not overlapped with openings Q2 of the crown oblique grooves 8 at the shoulder circumferential main groove 3E, and are not overlapped with openings Q3 of the axially outer shoulder oblique grooves 21 at the circumferential narrow groove 20. Imaginary extensions 8K of the crown oblique grooves 8 are not overlapped with openings Q4 of the axially inner shoulder oblique grooves 22 at the shoulder circumferential main groove 3E.
Claims
1. A pneumatic studless tire having a number of sipes, wherein a tread portion is provided with a pair of shoulder circumferential main grooves disposed one on each side of the tire equator so that the tread portion is axially divided into a crown land region between the shoulder circumferential main grooves, and a pair of shoulder land regions between the shoulder circumferential main grooves and the tread edges, a circumferential narrow groove disposed in each of the shoulder land regions, axially outer shoulder oblique grooves disposed in each of the shoulder land regions and extending axially outwardly from the circumferential narrow groove beyond the tread edge while inclining with respect to the tire axial direction to one direction, axially inner shoulder oblique grooves disposed in each of the shoulder land regions and extending axially inwardly from the circumferential narrow groove beyond the shoulder circumferential main groove while inclining with respect to the tire axial direction to one direction opposite to that of the axially outer shoulder oblique grooves so as to have their axially inner ends terminated within the crown land region, crown oblique grooves extending from one of the shoulder circumferential main grooves to the other while inclining with respect to the tire axial direction to one direction same as that of the axially outer shoulder oblique grooves, wherein imaginary extensions of the axially outer shoulder oblique grooves are shifted in the tire circumferential direction from openings of the axially inner shoulder oblique grooves at the circumferential narrow groove so that the imaginary extensions do not overlap with the openings in the tire circumferential direction at the circumferential narrow groove, imaginary extensions of the axially inner shoulder oblique grooves are shifted in the tire circumferential direction from openings of the crown oblique grooves at the shoulder circumferential main groove so that the imaginary extensions do not overlap with the openings in the tire circumferential direction at the shoulder circumferential main groove, the imaginary extensions of the axially inner shoulder oblique grooves are shifted in the tire circumferential direction from openings of the axially outer shoulder oblique grooves at the circumferential narrow groove so that the imaginary extensions do not overlap with the openings in the tire circumferential direction at the circumferential narrow groove, imaginary extensions of the crown oblique grooves are shifted in the tire circumferential direction from openings of the axially inner shoulder oblique grooves at the shoulder circumferential main groove so that the imaginary extensions do not overlap with the openings in the tire circumferential direction at the shoulder circumferential main groove, wherein each of the axially outer shoulder oblique grooves is a straight groove, the crown land region is provided with a center circumferential main groove extending circumferentially of the tire to axially divide each of the crown oblique grooves into two lateral groove parts, the center circumferential main groove is a zigzag groove composed of alternate lateral groove segments and longitudinal groove segments, each of the longitudinal groove segments extends straight between the circumferentially adjacent crown oblique grooves, each of the longitudinal groove segments has longitudinal groove walls extending at an angle () of not less than 60 degrees with respect to the tire axial direction, and each of the lateral groove segments has lateral groove walls extending at an angle () of not more than 5 degrees with respect to the tire axial direction.
2. The pneumatic tire according to claim 1, wherein an angle (a) of the axially outer shoulder oblique grooves with respect to the tire axial direction is 15 to 30 degrees, an angle (b)) of the axially inner shoulder oblique grooves with respect to the tire axial direction is 15 to 30 degrees, and an angle (c) of the crown oblique grooves with respect to the tire axial direction is 15 to 35 degrees.
3. The pneumatic tire according to claim 1, wherein the crown land region is provided with sipes inclined with respect to the tire axial direction to one direction opposite to that of the crown oblique grooves.
4. The pneumatic tire according to claim 1, wherein the two lateral groove parts of each crown oblique groove are respectively connected to the axial ends of one of the lateral groove segments, whereby each of the crown oblique grooves extends from one of the shoulder circumferential main grooves to the other through the lateral groove segment.
5. The pneumatic tire according to claim 4, wherein the lateral groove walls have a length (L1) in the tire axial direction of 2% to 10% of the tread width (TW).
6. The pneumatic tire according to claim 5, wherein a ratio (W2/W1) of a groove width (W2) of the lateral groove segments to a groove width (W1) of the longitudinal groove segments is 0.8 to 2.0.
7. The pneumatic tire according to claim 5, wherein the longitudinal groove segments are inclined with respect to the tire axial direction to one direction same as that of the crown oblique grooves.
8. The pneumatic tire according to claim 1, wherein each of the shoulder circumferential main grooves is a straight groove.
9. The pneumatic tire according to claim 4, wherein the crown land region is divided into crown blocks in two rows by the center circumferential main groove and the crown oblique grooves, and the crown blocks are each provided with sipes inclined with respect to the tire axial direction to one direction opposite to that of the crown oblique grooves.
10. The pneumatic tire according to claim 4, wherein the angle () of the longitudinal groove walls is not less than 75 degrees, and an angle (c) of the crown oblique grooves with respect to the tire axial direction is 15 to 35 degrees.
11. The pneumatic tire according to claim 1, wherein each of the axially inner shoulder oblique grooves is a straight groove.
12. The pneumatic tire according to claim 8, wherein each of the axially inner shoulder oblique grooves is a straight groove.
13. The pneumatic tire according to claim 12, wherein each of the circumferential narrow grooves is a straight groove having a width of less than 3 mm.
14. The pneumatic tire according to claim 1, wherein each of the circumferential narrow grooves is a straight groove having a width of less than 3 mm.
15. The pneumatic tire according to claim 8, wherein each of the circumferential narrow grooves is a straight groove having a width of less than 3 mm.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1)
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(8)
DESCRIPTION OF THE PREFERRED EMBODIMENTS
(9) Embodiments of present invention will now be described in detail in conjunction with accompanying drawings.
(10) As shown in
(11) Thereby, the tread portion 2 is axially divided into a crown land region 4C between the shoulder circumferential main grooves 3E, and a pair of shoulder land regions 4E between the shoulder circumferential main grooves 3E and the tread edges Te.
(12) Here, the term main groove means a relatively wide groove having a width of not less than 3.0 mm. A groove having a width of less than 3.0 mm is called narrow groove. A groove having a width of less than 2.0 mm (inclusive of a cut having substantially no groove width) is called sipe.
(13) The crown land region 4C is provided with crown oblique grooves 8 extending from one of the shoulder circumferential main grooves 3E to the other, while inclining with respect to the tire axial direction.
(14) Each of the shoulder land regions 4E is provided with
(15) a circumferential narrow groove 20 extending circumferentially of the tire,
(16) axially outer shoulder oblique grooves 21 extending axially outwardly from the circumferential narrow groove 20 beyond the tread edge Te, and
(17) axially inner shoulder oblique grooves 22 extending axially inwardly from the circumferential narrow groove 20 beyond the shoulder circumferential main groove 3E.
(18) By the circumferential narrow groove 20, the shoulder land region 4E is axially divided into an axial inner part 4Ei and an axially outer part 4Eo.
(19) The axially inner part 4Ei is circumferentially divided by the axially inner shoulder oblique grooves 22 into a plurality of axially inner shoulder blocks BEi.
(20) The axially outer part 4Eo is circumferentially divided by the axially outer shoulder oblique grooves 21 into a plurality of axially outer shoulder blocks BEo.
(21) The axially outer shoulder oblique grooves 21 are inclined with respect to the tire axial direction to one direction same as that of the crown oblique grooves 8.
(22) The axially inner shoulder oblique grooves 22 are inclined with respect to the tire axial direction to one direction opposite to that of the axially outer shoulder oblique grooves 21.
(23) The axially inner ends 22e of the axially inner shoulder oblique grooves 22 are terminated within the crown land region 4C.
(24) In this embodiment, the axially outer shoulder oblique grooves 21 and the axially inner shoulder oblique grooves 22 extend straight along the respective entire lengths.
(25) As shown in
(26) Further, imaginary axially inward extensions 22K of the axially inner shoulder oblique grooves 22 are shifted in the tire circumferential direction from the openings Q2 of the crown oblique grooves 8 at the shoulder circumferential main groove 3E not to overlap with the openings Q2, and
imaginary axially outward extensions 22K of the axially inner shoulder oblique grooves 22 are shifted in the tire circumferential direction from the openings Q3 of the axially outer shoulder oblique grooves 21 at the circumferential narrow groove 20 not to overlap with the openings Q3.
Furthermore, imaginary axially outward extensions 8K of the crown oblique grooves 8 are shifted in the tire circumferential direction from the openings Q4 of the axially inner shoulder oblique grooves 22 at the shoulder circumferential main groove 3E not to overlap with the openings Q4.
Therefore, during cornering on snowy road, for example as shown in
(27) Further, the axially outer shoulder oblique grooves 21 are inclined oppositely to the axially inner shoulder oblique grooves 22 which are inclined oppositely to the crown oblique grooves 8. Namely, the axially adjacent oblique lateral grooves are inclined oppositely to each other.
(28) Therefore, the tread pattern rigidity becomes hard to be biased, and it becomes possible to increase the lateral grip force without largely deteriorating the wear resistance.
(29) As shown in
(30) the angle c of the crown oblique grooves 8 with respect to the tire axial direction is preferably set in a range of 15 to 35 degrees.
(31) If the angles a to c become less than the respective lower limits, then the lateral grip force during cornering is decreased, and the effect to improve the cornering performance on snowy roads is decreased.
(32) If the angles a to c become more than the respective upper limits, then although the lateral grip force is increased, as the tread pattern rigidity is biased, the uneven wear resistance is liable to decrease.
(33) As shown in
(34) In this example, all of the circumferential main grooves 3 have the same depth D3.
(35) Preferably, the depth D8 of the crown oblique grooves 8 is less than the depth D3. In this example, the depth D8 is set in a range of 60% to 80% of the depth D3.
(36) Each of the crown oblique grooves 8 may be provided with a tie bar 12 rising from the groove bottom and connecting between the circumferentially adjacent crown blocks to increase the rigidity of the crown blocks.
(37) It is preferable that, as shown in
(38) In this example, the depths D21 and D22 are set in a range of the 60% to 80% of the depth D3.
(39) Each of the axially outer shoulder oblique grooves 21 may be provided with a tie bar 24 similar to the tie bar 12.
(40) Each of the axially inner shoulder oblique grooves 22 may be provided with a tie bar 25 similar to the tie bar 12.
(41) The depth D20 of the circumferential narrow grooves 20 is preferably less than the depth D3 and less than the depths D21 and D22.
(42) In this example, as shown in
(43) Thereby, the crown land region 4C is axially divided into two parts 4CA and 4CA each of which is circumferentially divided into crown blocks BC in a circumferential row.
(44) Further, the crown oblique grooves 8 are each axially divided into two lateral groove parts 8A and 8A.
(45) The lateral groove parts 8A of the crown oblique grooves 8 extend straight along the respective entire lengths.
(46) The above-mentioned imaginary extensions 8K of each crown oblique groove 8 are two axially outward extensions from the respective lateral groove parts 8A.
(47) In this example, the center circumferential main groove 3C is a saw-tooth like zigzag groove made up of alternate lateral groove segments 5 and longitudinal groove segments 6. The lateral groove segments 5 extend substantially parallel with the tire axial direction. The longitudinal groove segments 6 extend at a small angle with respect to the tire circumferential direction.
(48) The lateral groove segments 5 are distinguished from the longitudinal groove segments 6 as shown in
(49) In this example, the zigzag amplitude center line of the center circumferential main groove 3C coincides with the tire equator Co. But, it may be possible that the zigzag amplitude center line does not coincide with the tire equator Co, or the center circumferential main groove 3C is separated from the tire equator Co.
(50) The opposite groove walls 5S of the lateral groove segment 5 (hereinafter, the lateral groove walls 5S) extend at an angle of not more than 5 degrees with respect to the tire axial direction.
(51) The opposite groove walls 6S of the longitudinal groove segment 6 (hereinafter, the longitudinal groove walls 6S) extend at an angle of not less than 60 degrees with respect to the tire axial direction.
(52) One lateral groove segment 5 and one longitudinal groove segment 6 as one unit PC are repeated circumferentially of the tire.
(53) In this example, the axial ends of each of the lateral groove segments 5 are connected to the axially inner ends of two of the lateral groove parts 8A disposed on both sides thereof.
(54) Meanwhile, the crown land region 4C is such a region where the ground contacting pressure is relatively high and whose ground contacting length in the tire circumferential direction is relatively long. Accordingly, its effect on the snow performance is large.
(55) Therefore, in this example, the saw-tooth like center circumferential main groove 3C and the crown oblique grooves 8 are disposed in this region in order to maximally derive the undermentioned effects, and thereby to further improve the snow performance.
(56) First, by inclining the lateral groove walls 5S at the angle of not more than 5 degrees, the center circumferential main groove 3C can most effectively contribute to the traction performance in relation to the zigzag amplitude.
(57) When snow in the center circumferential main groove 3C is compacted during running on snowy road, as shown in
(58) And this compression force F is transmitted to snow in the lateral groove segment 5.
(59) Since both ends of the lateral groove segment 5 are connected to the lateral groove parts 8A, the compression force F is transmitted to snow in the lateral groove parts 8A through the snow in the lateral groove segment 5.
(60) As a result, the snow in the longitudinal groove segment 6, the snow in the lateral groove segment 5, and the snow in the lateral groove parts 8A are compacted and form a substantially T-shaped hard compacted snow together.
(61) Such compacted snow therefore can exert large sharing force in both of the tire circumferential direction and the tire axial direction, and the grip performance on snowy roads is improved.
(62) Thus, it is possible to further improve the snow performance including the cornering performance.
(63) From this standpoint, it is preferable that the length L1 in the tire axial direction of the lateral groove walls 5S as shown in
Even if the length L1 is increased over 10% of the tread width TW, a further increase in the sharing force of the compacted snow can not be obtained.
In addition, the rigidity of the crown blocks BC is decreased disadvantageously for the wear resistance and the uneven wear resistance because the zigzag amplitude increases with the increase in the length L1, and as a result, a maximum WB1 of the axial width of the crown block BC is increased and a minimum WB2 thereof is decreased. Namely, the rigidity of the crown block BC becomes more uneven. Thus, the wear resistance and the uneven wear resistance are deteriorated.
(64) From this viewpoint, it is desirable that the length L1 is not less than 4%, but not more than 8% of the tread width TW. From a point of view of the wear resistance and the uneven wear resistance, it is desirable that the angle of the longitudinal groove walls 6S is not less than 75 degrees.
(65) In order to fully stop the snow in the longitudinal groove segment 6, the length L1 is preferably not less than the width W6 in the tire axial direction of the longitudinal groove segment 6.
(66) Preferably, the ratio W2/W1 of the groove width W2 of the lateral groove segment 5 to the groove width W1 of the longitudinal groove segment 6 is set in a range of from 0.8 to 2.0.
(67) The groove width W1 is the distance between the lateral groove walls 5S of the lateral groove segment 5 measured perpendicularly to the groove's length direction.
(68) The groove width W2 is the distance between the longitudinal groove walls 6S of the longitudinal groove segment 6 measured perpendicularly to the groove's length direction.
(69) If the ratio W2/W1 becomes outside the above-mentioned range, the thicknesses of the compacted snows become imbalanced, and there is a tendency such that the strength is decreased and the compacted snow's sharing force is decreased.
(70) Further, there is a possibility that the width of the center circumferential main groove 3C is partially decreased to deteriorate the drainage.
(71) As shown in
(72) In this case, the length L1 of the lateral groove wall 5S is defined by the length of the lateral groove wall 5S excluding the chamfer 11.
(73) It is preferable that the lateral groove parts 8A are inclined with respect to the tire axial direction to one direction same as that of the longitudinal groove segments 6. In
(74) By inclining to the same direction as explained above, water flows J between the lateral groove parts 8A and the longitudinal groove segments 6 (shown in
(75) The crown blocks BC are provided with sipes 10.
(76) The sipes 10 are inclined with respect to the tire axial direction to one direction opposite to that of the lateral groove parts 8A.
(77) In
(78) By oppositely orienting as explained above, deformation of the crown blocks BC is facilitated, and snow in the lateral groove parts 8A is moved and compressed toward the lateral groove segments 5. As a result, the snow is compacted near the junctions of the lateral groove parts 8A and the lateral groove segments 5, and the strength of the compacted snow is increased. Further, the sipes 10 improve the ice performance and snow performance of the tire by their edge effect.
In this example, the shoulder circumferential main grooves 3E extend straight in the tire circumferential direction.
Thereby, the drainage and the self ejection of snow are improved. Further, the straight running stability is improved during running on snowy roads.
Comparison Test 1
(79) Based on the tread pattern shown in
(80) The tire were tested for the snow performance and wear resistance as follows.
(81) <Cornering Performance on Snow>
(82) The test tires were mounted on all of the four wheels of a medium-sized van (Engine displacement 2800 cc, front tire pressure 390 kPa, rear tire pressure 350 kPa, load 50% of maximum load), and a test driver evaluated the lateral grip force during running on a snow covered road surface of a tire test course. The results are indicated in Table 1 by an index based on Comparative example tire Ref.1 being 100, wherein the larger the index number, the higher the lateral grip force, namely, the better the cornering performance on snow.
(83) <Wear Resistance>
(84) Using the above-mentioned test vehicle, after running for 30000 km on a dry road surface of a tire test course, the amount of tread wear was measured. The results are indicated in Table 1 by an index based on Comparative example tire Ref.1 being 100, wherein the larger the index number, the better the wear resistance.
(85) Comparison Test 2
(86) Based on the tread pattern shown in
(87) The tire were tested for the snow performance as above and the wet performance as follows. The results of the snow performance test are indicated in Table 2.
(88) <Wet Performance>
(89) Using the above-mentioned test vehicle, the test driver evaluated the steering stability during running on a wet road surface of the tire test course. The results are indicated in Table 2 by an index based on Comparative example tire Ref.A1 being 100, wherein the larger the index number, the better the wet performance.
(90) As shown in Table 1 and Table 2, the working example tires were improved in the cornering performance on snow.
(91) TABLE-US-00001 TABLE 1 Tire Ref. 1 Ref. 2 Ref. 3 Ref. 4 Ex. 1 Ex. 2 Ex. 3 Ex. 4 Ex. 5 Ex. 6 Ex. 7 Ex. 8 axially outer shoulder oblique grooves angle a (deg.) *1 +15 +25 +25 +25 +5 +15 +25 +30 +35 +25 +25 +25 axially inner shoulder oblique grooves angle b (deg.) *1 +15 25 25 25 25 25 25 25 25 5 15 25 crown oblique grooves angle c (deg.) *1 +15 +30 +30 +30 +30 +30 +30 +30 +30 +30 +30 +30 (O)verlap or (N)ot imaginary extension 21K & opening Q1 N O N N N N N N N N N N imaginary extension 22K & opening Q3 N N O N N N N N N N N N imaginary extension 8K & opening Q4 N N N O N N N N N N N N center sipes' inclining direction *2 opposite center circumferential main groove lateral groove segment angle (deg.) 0 0 0 0 0 0 0 0 0 0 0 0 longitudinal groove segment angle (deg.) 78 78 78 78 78 78 78 78 78 78 78 78 cornering performance on snow 100 95 98 95 110 120 130 120 120 110 120 130 wear resistance 100 100 100 100 100 100 100 100 90 100 100 100 Total 200 195 198 195 210 220 230 220 210 210 220 230 Tire Ex. 9 Ex. 10 Ex. 11 Ex. 12 Ex. 13 Ex. 14 Ex. 15 Ex. 16 Ex. 17 Ex. 18 Ex. 19 axially outer shoulder oblique grooves angle a (deg.) *1 +25 +25 +25 +25 +25 +25 +25 +25 +25 +25 +25 axially inner shoulder oblique grooves angle b (deg.) *1 30 35 25 25 25 25 25 25 25 25 25 crown oblique grooves angle c (deg.) *1 +30 +30 +5 +15 +25 +30 +35 +25 +30 +30 +30 (O)verlap or (N)ot imaginary extension 21K & opening Q1 N N N N N N N N N N N imaginary extension 22K & opening Q3 N N N N N N N N N N N imaginary extension 8K & opening Q4 N N N N N N N N N N N center sipes' inclining direction *2 opposite same opposite opposite center circumferential main groove lateral groove segment angle (deg.) 0 0 0 0 0 0 0 0 0 5 0 longitudinal groove segment angle (deg.) 78 78 78 78 78 78 78 78 78 78 60 cornering performance on snow 120 120 110 120 130 125 120 120 125 125 120 wear resistance 100 90 100 100 100 100 100 90 100 100 100 Total 220 210 210 220 230 225 220 210 225 225 220 *1 + (plus sign): inclined upward to the right (minus sign): inclined downward to the right *2 opposite: inclined to the opposite direction to the crown oblique grooves same: inclined to the same direction as the crown oblique grooves
(92) TABLE-US-00002 TABLE 2 Tire Ref. A1 Ex. A1 Ex. A2 Ex. A3 Ref. A2 Ex. A4 Ref. A3 Ex. A5 center circumferential main groove lateral groove segment angle (deg.) 0 0 0 0 0 5 10 0 longitudinal groove segment angle (deg.) 78 78 78 78 78 78 78 78 length ratio L1/TW(%) 1 2 4 10 15 4 4 4 groove width ratio W2/W1 1 1 1 1 1 1 1 0.5 inclination crown oblique grooves and longitudinal groove segments same same same same same same same same crown oblique grooves and sipes opposite opposite opposite opposite opposite opposite opposite opposite crown oblique groove angle c (deg.) 30 30 30 30 30 30 30 30 snow performance 100 108 115 120 110 110 102 108 wet performance 100 100 98 95 86 100 95 94 total 200 208 213 215 196 210 197 202 Tire Ex. A6 Ex. A7 Ex. A8 Ex. A9 Ex. A10 Ex. A11 Ex. A12 Ex. A13 center circumferential main groove lateral groove segment angle (deg.) 0 0 0 0 0 0 0 0 longitudinal groove segment angle (deg.) 78 78 78 78 60 78 78 78 length ratio L1/TW(%) 4 4 4 4 4 4 4 4 groove width ratio W2/W1 0.8 2 2.5 1 1 1 1 1 inclination crown oblique grooves and longitudinal groove segments same same same opposite same same same same crown oblique grooves and sipes opposite opposite opposite opposite same opposite opposite opposite crown oblique groove angle c (deg.) 30 30 30 30 30 30 15 35 snow performance 110 110 105 115 112 110 115 110 wet performance 98 102 105 95 98 98 92 98 total 208 212 210 210 210 208 207 208
REFERENCE SIGNS LIST
(93) 1 pneumatic tire 2 tread portion 3C center circumferential main groove 3E shoulder circumferential main groove 4C crown land region 4E shoulder land region 5 lateral groove segment 5S lateral groove wall 6 longitudinal groove segment 6S longitudinal groove wall 8 crown oblique groove 8K imaginary extension 10 sipe 20 circumferential narrow groove 21 axially outer shoulder oblique groove 22e inner end 22 axially inner shoulder oblique groove 21K imaginary extension 22K imaginary extension BC crown block Co tire equator Q1, Q2, Q3, Q4 opening