The present disclosure relates to a tyre, more particularly to a tyre including a tread portion having a designated mounting direction to a vehicle.
Recently, tyres having tread portions with a. designated mounting direction to a vehicle have been proposed. For example, the following Patent document 1 discloses a pneumatic tyre including a tread center land portion which is provided with a plurality of center sipes having a width of less than 2 mm, but is not provided with any grooves that have groove widths more than 2 mm and that traverse the land portion completely in the tyre axial direction. The above-mentioned pneumatic tyre enhances stiffness of the tread center land portion, thus expecting to improve steering stability on dry road conditions.
Since the tread center land portion has high stiffness, the above-mentioned pneumatic tyre tends to deteriorate noise performance due to large impact noise generated by the tread center land portion upon grounding. The inventors have found out that steering stability and noise performance of tyre can be improved by improving an arrangement of the lateral grooves in tyres having a tread portion with a designated mounting direction.
The present disclosure has been made in view of the above problem and has a major object to provide a tyre capable of improving steering stability and noise performance.
In one aspect of the disclosure, a tyre includes a tread portion having a designated mounting direction to a vehicle, the tread portion including a first tread edge and a second tread edge to be located outwardly and inwardly of a vehicle, respectively, when being mounted to the vehicle, two or more main grooves extending continuously in a tyre circumferential direction between the first tread edge and the second tread edge, and two or more land portions divided by the main grooves, wherein the main grooves include a first shoulder main groove disposed between the first tread edge and a tyre equator, a second shoulder main groove disposed between the second tread edge and the tyre equator, and a crown main groove disposed between the first shoulder main groove and the second shoulder main groove, the land portions include a first middle land portion defined between the first shoulder main groove and the crown main groove, and a second middle land portion defined between the second shoulder main groove and the crown main groove, the first middle land portion is provided with two or more first middle lateral grooves traversing the first middle land portion completely in a tyre axial direction, the second middle land portion is provided with two or more second middle lateral grooves traversing the second middle land portion completely in the tyre axial direction, at least one of the first middle lateral grooves includes a raised portion in which a groove bottom thereof is raised, the raised portion of the at least one of the first middle lateral grooves traversing a center location in the tyre axial direction of the first middle land portion, at least one of the second middle lateral grooves includes a raised portion in which a groove bottom thereof is raised, the raised portion of the at least one of the second middle lateral grooves traversing a center location in the tyre axial direction of the second middle land portion, and a length in the tyre axial direction of the raised portion of the at least one of the first middle lateral grooves is greater than a length in the tyre axial direction of the raised portion of the at least one of the second middle lateral grooves.
In another aspect of the disclosure, the length in the tyre axial direction of the raised portion of the at least one of the first middle lateral grooves may be in a range of from 1.05 to 1.25 times the length in the tyre axial direction of the raised portion the at least one of the second middle lateral grooves.
In another aspect of the disclosure, a depth of the raised portion of the at least one of the first middle lateral grooves and a depth of the raised portion of the at least one of the second middle lateral grooves may be in a range of from 0.10 to 0.60 times a depth of the crown main groove.
In another aspect of the disclosure, in a plan view of the tread portion, each of the first middle lateral grooves and the second middle lateral grooves may be provided with the raised portion which is inclined at an angle with respect to the tyre axial direction, a first outer portion extending from a first end of the raised portion and having a smaller angle with respect to the tyre axial direction than the angle of the raised portion, and a second outer portion extending from a second end of the raised portion and having a smaller angle with respect to the tyre axial direction than the angle of the raised portion, so as to form a curved groove.
In another aspect of the disclosure, the curved groove may have an S-shaped manner.
In another aspect of the disclosure, in each of the first middle lateral grooves and the second middle lateral grooves, a length in the tyre axial direction of the raised portion may be greater than those in the tyre axial direction of the first outer portion and the second outer portion.
In another aspect of the disclosure, in each of the second middle lateral grooves, a length in the tyre axial direction of the second outer portion may be greater than a length in the tyre axial direction of the first outer portion.
In another aspect of the disclosure, in each of the second middle lateral grooves, a length in the tyre axial direction of the second outer portion may be in a range of from 1.10 to 2.00 times a length in the tyre axial direction of the first outer portion.
In another aspect of the disclosure, in each of the second middle lateral grooves, the second outer portion may be arranged on the second tread edge side with respect to the raised portion.
In another aspect of the disclosure, in each first middle lateral groove, a length in the tyre axial direction of the first outer portion may be same as a length in the tyre axial direction of the second outer portion.
In another aspect of the disclosure, in a. plan view of the tread portion, each of the first middle lateral grooves and the second middle lateral grooves may be a curved groove which includes a first convex portion located on a first side with respect to groove-reference-straight-line that connects both ends of a groove centerline thereof and a second convex portion located on a second side with respect to the groove-reference-straight-line of the curved groove.
In another aspect of the disclosure, in a plan view of the tread portion, the raised portion of the at least one of the first middle lateral grooves may be inclined in a first direction with respect to the tyre axial direction, and the raised portion of the at least one of the second middle lateral grooves may be inclined in a second direction which is opposite to the first direction with respect to the tyre axial direction.
In another aspect of the disclosure, an angle θ1 with respect to the tyre axial direction of the raised portion of the at least one of the first middle lateral grooves may be smaller than an angle θ2 with respect to the tyre axial direction of the raised portion of the at least one of the second middle lateral grooves.
In another aspect of the disclosure, the first middle lateral grooves and the second middle lateral grooves, at both ends thereof in the tyre axial direction, may have a depth in a range of from 0.30 to 0.80 times a depth of the crown main groove.
In another aspect of the disclosure, a length in the tyre axial direction of the raised portion of the at least one of the first middle lateral grooves may be in a range of from 0.30 to 0.80 times a width in the tyre axial direction of the first middle land portion.
In another aspect of the disclosure, a length in the tyre axial direction of the raised portion of the least one of the second middle lateral grooves may be in a range of from 0.30 to 0.80 times a width in the tyre axial direction of the second middle land portion.
In another aspect of the disclosure, the first middle land portion may include two or more first middle blocks divided by the first middle lateral grooves, the second middle land portion may include two or more second middle blocks divided by the second middle lateral grooves, each first middle lateral groove may have a groove-reference-straight-line that connects both ends of a groove centerline thereof being inclined in a first direction with respect to the tyre axial direction, and each second middle lateral groove may have a groove-reference-straight-line that connects both ends of a groove centerline thereof being inclined in a second direction which is opposite to the first direction with respect to the tyre axial direction.
In another aspect of the disclosure, each first middle block may be a smooth block having a ground contacting face which is not provided with any grooves nor sipes, and each second middle block may be provided with at least one second middle sipe extending from the second shoulder main groove and terminating within the second middle block.
In another aspect of the disclosure, in a plan view of the tread portion, the raised portion of the at least one of the second middle lateral grooves may overlap with the at least one second middle sipe in the tyre axial direction
In another aspect of the disclosure, a length in the tyre circumferential direction of the groove-reference-straight-line of each first middle lateral groove may he smaller than a length in the tyre circumferential direction of the groove-reference-straight-line of each second middle lateral groove.
An embodiment of the present disclosure will be explained below with reference to the accompanying drawings.
As illustrated in
The first tread edge Te1 and the second tread edge Te2, when the tyre 1 is a pneumatic tyre, are the axial outermost edges of the ground contacting patch of the tyre 1 which occurs under a normal condition with a standard tyre load when the camber angle of the tyre is zero. As used herein, the “normal condition” is such that the tyre 1 is mounted onto a standard wheel rim with a standard pressure but loaded with no tyre load. Unless otherwise noted, dimensions of respective portions of the tyre 1 are values measured under the normal condition.
The “standard wheel rim” is a wheel rim officially approved for each tyre by standards organizations on which the tyre is based, wherein the standard wheel rim is the “standard rim” specified in JATMA, the “Design Rim” in TRA, and the “Measuring Rim” in ETRTO, for example.
The “standard pressure” is a standard pressure officially approved for each tyre by standards organizations on which the tyre is based, wherein the standard pressure is the “maximum air pressure” in JATMA, the maximum pressure given in the “Tire Load. Limits at Various Cold inflation Pressures” table in TRA, and the “Inflation Pressure” in ETRTO, for example.
The standard tyre load is a tyre load officially approved for each tyre by standards organizations in which the tyre is based, wherein the standard tyre load is the “maximum load capacity” in JATMA, the maximum value given in the above-mentioned table in TRA, the “Load Capacity” in ETRTO, for example.
The tread portion 2 includes two or more main grooves 3 extending continuously in the tyre circumferential direction between the first tread edge Te1 and the second tread edge Te2, and two or more land portions 4 divided by the main grooves 3.
The main grooves 3 include a first shoulder main groove 5 disposed between the first tread edge Te1 and the tyre equator C, a second shoulder main groove 6 disposed between the second tread edge Te2 and the tyre equator C, and a crown main groove 7 disposed between the first shoulder main groove 5 and the second shoulder main groove 6.
It is preferable that a length La in the tyre axial direction from the tyre equator C to a groove centerline of either one of the first shoulder main groove 5 or the second shoulder main groove 6, for example, is in a range of from 0.15 to 0.30 times the tread width TW. The tread width TW is a distance in the tyre axial direction from the first tread edge Te1 to the second tread edge Te2 under the normal condition.
As the crown main groove 7 according to the present embodiment, a single crown groove is provided on the tyre equator C, for example. In another aspect, two crown main groove 7 may be provided such that the tyre equator C is located therebetween, for example.
Each main groove 3 according to the present embodiment, for example, extends in a straight shape parallel with the tyre circumferential direction, i.e., having a pair of groove edges extending straight shape parallel with the tyre circumferential direction. Alternatively, the main grooves 3, for example, may extend in a zigzag or wavy manner.
It is preferable that a groove width Wa of the main grooves 3, for example, is in a range of from 4.0% to 7.0% of the tread width TW. It is preferable that a depth of the main grooves 3, for example, is in a range of from 5 to 10 mm for a pneumatic passenger car tyre.
The land portions 4 include a first middle land portion 11, a second middle land portion 12, a first shoulder land portion 13, and a second shoulder land portion 14. The tread portion 2 according to the present embodiment has a four-rib pattern which is configured by three main grooves 3 and four land portions 4. In another aspect of the present disclosure, the tread portion 2 may have a five-rib pattern which is configured by five land portions 4 divided by four main grooves including two crown main grooves 7, for example.
The first middle land portion 11 is defined between the first shoulder main groove 5 and the crown main groove 7. The second middle land portion 12 is defined between the second shoulder main groove 6 and the crown main groove 7. The first shoulder land portion 13 is defined between the first shoulder main groove 5 and the first tread edge Te1. The second shoulder land portion 14 is defined between the second shoulder main groove 6 and the second tread edge Te2.
The first middle land portion 11 is provided with two or more first middle lateral grooves 16. The first middle lateral grooves 16 traverse the first middle land portion 11 completely in the tyre axial direction. The second middle land portion 12 is provided with two or more second middle lateral grooves 17. The second middle lateral grooves 17 traverse the second middle land portion 12 completely in the tyre axial direction. A groove width of the first middle lateral grooves 16 and the second middle lateral grooves 17, for example, is in a range of from 0.10 to 0.20 times a groove width of the crown main groove 7.
To help understand the raised portions 18 and 19, they are colored on one of the first middle lateral grooves 16 and one of the second middle lateral grooves 17 in
Further, the first middle lateral grooves 16 and the second middle lateral grooves 17 can reduce pumping noise by the raised portions which disturb air flow through the grooves. In addition, the first middle lateral grooves 16 and the second middle lateral grooves 17 with the raised portions can ensure sufficient stiffness of the respective middle land portions, thus improving steering stability.
As illustrated in
In some preferred embodiments, the length L3 of the raised portions 18 of the first middle lateral grooves 16 is in a range of from 1.05 to 1.25 times the length L4 of the raised portions 19 of the second middle lateral grooves 17. Such a configuration of the raised portions can help to improve steering stability and ride comfort in a well-balanced manner.
The length L3 in the tyre axial direction of the raised portions 18 of the first middle lateral grooves 16 is in a range of from 0.30 to 0.80 times the width W1 (shown in
A depth d2 of the raised portions 18 and 19, for example, is preferably equal to or more than 0.10 times, more preferably equal to or more than 0.20 times a depth d1 of the crown main groove 7, but preferably equal to or less than 0.60 times, more preferably equal to or less than 0.50 times the depth d1. In addition, the first middle lateral grooves 16 and the second middle lateral grooves 17, at both ends thereof in the tyre axial direction, have a depth in a range of from 0.30 to 0.80 times the depth d1 of the crown main groove 7. The first middle lateral grooves 16 and the second middle lateral grooves 17 configured as such can improve steering stability and ride comfort in a well-balanced manner.
As illustrated in
Since the first middle lateral grooves 16 and the second middle lateral grooves 17 can mitigate stiffness of the respective middle land portions, impact noise generated by the respective middle land portions can be reduced. In particular, the S-shaped first and second middle lateral grooves 16 and 17 can facilitate deformation along the respective groove-reference-straight-lines so that impact noise can be reduced. In addition, the above-mentioned curved grooves can help to reduce pumping noise upon grounding since the curved grooves enable to make the air flowing in the grooves slow down.
In the present embodiment, each first middle lateral groove 16 is configured such that an entire center portion 16d in the tyre axial direction thereof is the above-mentioned raised portion 18. Specifically, each first middle lateral groove 16 includes the center portion 16d (the raised portion 18) traversing the center location in the tyre axial direction of the first middle land portion 11 obliquely, a first outer portion 16e, and a second outer portion 16f. The first outer portion 16e extends from one end side of the center portion 16d at a smaller angle with respect to the tyre axial direction than that of the center portion 16d. The second outer portion 16f extends from the other end side of the center portion 16d at a smaller angle with respect to the tyre axial direction than that of the center portion 16d. In the present embodiment, the first outer portion 16e is arranged on the first tread edge Te1 side with respect to the center portion 16d, and the second outer portion 16f is arranged on the second tread edge Te2 side with respect to the center portion 16d.
Similarly, each second middle lateral grooves 17 is configured such that an entire center portion 17d in the tyre axial direction thereof is the above-mentioned raised portion 19. Specifically, each second middle lateral groove 17 includes the center portion 17d (the raised portion 19) traversing the center location in the tyre axial direction of the second middle land portion 12 obliquely, a first outer portion 17e, and a second outer portion 17f. The first outer portion 17e extends from one end side of the center portion 17d at a smaller angle with respect to the tyre axial direction than that of the center portion 17d. The second outer portion 17f extends from the other end side of the center portion 17d at a smaller angle with respect to the tyre axial direction than that of the center portion 17d. In the present embodiment, the first outer portion 17e is arranged on the first tread edge Te1 side with respect to the center portion 17d, and the second outer portion 17f is arranged on the second tread edge Te2 side with respect to the center portion 17d.
In the present embodiment, the groove-reference-straight-line 16c of each first middle lateral groove 16, for example, is inclined in a first direction (e.g. downward to the right) with respect to the tyre axial direction. In addition, it is preferable that each first middle lateral groove 16 has the raised portion 18 which is inclined in the first direction with respect to the tyre axial direction. In each first middle lateral groove 16, an angle θ1 of the raised portion 18 with respect to the tyre axial direction is greater than an angle of the groove-reference-straight-line 16c with respect to the tyre axial direction. Specifically, the angle θ1 of the raised portion 18 of each first middle lateral groove 16 with respect to the tyre axial direction is preferably in a range of from 5 to 40 degrees, more preferably from 15 to 30 degrees.
In the present embodiment, the groove-reference-straight-line 17c of each second middle lateral groove 17, for example, is inclined with respect to the tyre axial direction in a second direction (e.g., upward to the right) opposite to the first direction.
The first middle lateral grooves 16 and the second middle lateral grooves 17 configured as such can suppress “tyre pull” in which unequal forces cause a vehicle to pull to the side due to the tread pattern even when it is steered straight ahead, thus improving steering stability. in addition, the first middle lateral grooves 16 and the second middle lateral grooves 17 help to disperse frequency ranges of the respective pumping noise, thus improving noise performance.
In each second middle lateral groove 17, it is preferable that the raised portion 19 is inclined in the second direction with respect to the tyre axial direction. In each second middle lateral groove 17, an angle θ2 of the raised portion 19 with respect to the tyre axial direction is greater than an angle of the groove-reference-straight-line 17c with respect to the tyre axial direction. Specifically, the angle θ2 of the raised portion 19 of each second middle lateral groove 17 with respect to the tyre axial direction is preferably in a range of from 20 to 60 degrees, more preferably in a range of from 40 to 55 degrees.
In the present embodiment, the angle θ1 of the raised portion 18 of each first middle lateral groove 16 with respect to the tyre axial direction is smaller than the angle θ2 of the raised portion 19 of each second middle lateral groove 17 with respect to the tyre axial direction. Thus, stiffness of the first middle land portion 11 in the tyre axial direction can be enhanced relatively, improving steering stability further.
As illustrated in
In each first middle lateral groove 16, the length L6 in the tyre axial direction of the second outer portion 16f is preferably in a range of from 0.90 to 1.10 times the length L5 in the tyre axial direction of the first outer portion 16e. In the present embodiment, in each first middle lateral groove 16, the length L6 of the second outer portion 16f is the same as the length L5 of the first outer portion 16e.
In each second middle lateral groove 17, it is preferable that the length L8 in the tyre axial direction of the second outer portion 17f is greater than the length L7 in the tyre axial direction of the first outer portion 17e. Specifically, the length L8 of the second outer portion 17f, for example, is preferably in a range of from 1.10 to 2.00 times the length L7 of the first outer portion 17e. Thus, stiffness of the second middle lateral grooves 17 on the first tread edge Te1 side can be enhanced, enabling to provide a linear steering response upon cornering.
Further, by configuring the raised portions 18 and 19 as described above, the respective ranges of frequency of pumping noise generated by the first middle lateral grooves 16 and the second middle lateral grooves 17 can be deviated, generating white noise.
As illustrated in
It is preferable that the length in the tyre circumferential direction of the groove-reference-straight-line 16c of each first middle lateral groove 16 is in a range of from 0.20 to 0.40 times the length in the tyre circumferential direction of the groove-reference-straight-line 17c of each second middle lateral groove 17. Such a groove arrangement can improve a linear steering response upon cornering further.
It is preferable that the length L1 in the tyre circumferential direction of the groove-reference-straight-line 16c of each first middle lateral groove 16, for example, is smaller than pitch lengths P1 in the tyre circumferential direction of the first middle lateral grooves 16. Specifically, the length L1 in the tyre circumferential direction of the groove-reference-straight-line 16c of each first middle lateral groove 16 is preferably in a range of from 0.05 to 0.20 times the pitch lengths P1 in the tyre circumferential direction of the first middle lateral grooves 16, for example. An arrangement of the first middle lateral grooves 16 as such helps to prevent uneven wear of the first middle land portion 11.
In the same view point, it is preferable that the length L2 in the tyre circumferential direction of the groove-reference-straight-line 17c of each second middle lateral groove 17, for example, is smaller than pitch lengths P2 in the tyre circumferential direction of the second middle lateral grooves 17. Specifically, the length L2 in the tyre circumferential direction of the groove-reference-straight-line 17c of each second middle lateral groove 17 is preferably in a range of from 0.35 to 0.50 times the pitch lengths P2 in the tyre circumferential direction of the second middle lateral grooves 17, for example. Note that the pitch lengths P2 of the second middle lateral grooves 17 are the same as the pitch lengths P1 of the first middle lateral grooves 16.
A maximum distance L9 of each first middle lateral groove 16 between a groove edge thereof and the groove-reference-straight-line 16c thereof is smaller than a maximum distance L10 of each second middle lateral groove 17 between a groove edge thereof and the groove-reference-straight-line 17c thereof. Thus, stiffness of the first middle land portion 11 can be enhanced relatively, and the above-mentioned effects can further be improved.
It is preferable that the first middle lateral grooves 16 are arranged so as to be continuous to the respective second middle lateral grooves 17 smoothly through the crown main groove 7. As used herein, “one lateral groove is continuous to another lateral groove smoothly through a main groove” shall mean that respective regions in which the lateral grooves are elongated along the respective groove longitudinal directions, in the tyre circumferential direction, overlap with one another within the main groove, or that the respective regions, in the tyre circumferential direction, are located away from one another within a distance of less than 1.0 mm within the main groove. If a lateral groove is curved, the above-mentioned region is defined such that the lateral groove is elongated while keeping the radius of curvature of an axial end thereof on the main groove side.
The first middle land portion 11 includes a plurality of first middle blocks 21 divided by the first middle lateral grooves 16. The second middle land portion 12 includes a plurality of second middle blocks 22 divided by the second middle lateral grooves 17.
In the present embodiment, each first middle blocks 21, for example, is a smooth block having a ground contacting face which is not provided with any grooves nor sipes. As used herein, “sipe” shall mean a narrow cut having a width of less than 1.5 mm.
Each second middle block 22 is provided with a second middle sipe 23 which extends from the second shoulder main groove 6 and which terminates within the second middle block 22. In the present embodiment, the second middle sipe 23, for example, has a width of from 0.5 to 1.0 mm. Such first middle blocks 21 and second middle blocks 22 can enhance stiffness of the first middle land portion 11 relatively, providing a linear steering response so that steering stability can be improved.
It is preferable that a length L11 in the tyre axial direction of each second middle sipe 23, for example, is in a range of from 0.20 to 0.80 times the width W2 in the tyre axial direction of the second middle land portion 12. Such a second middle sipe 23 can help to improve steering stability and ride comfort in a well-balanced manner.
It is preferable that the raised portion 19 of each second middle lateral groove 17 overlaps with the respective second middle sipes 23 in the tyre axial direction. Thus, the second middle sipes 23 can help to reduce impact noise generated when the second middle land portion 12 grounds, improving noise performance,
For example, a maximum depth of the second middle sipes 23 is in a range of from 0.90 to 1.10 times the depths of the raised portions 19 of the second middle lateral grooves 17. In the present embodiment, the maximum depth of the second middle sipes 23 is the same as the depths of the raised portions 19 of the second middle lateral grooves 17. The second middle sipes 23 can help to prevent uneven wear of the second middle land portion 12.
Each first shoulder lateral groove 25, for example, is inclined in the second direction. An angle θ3 of the first shoulder lateral grooves 25, for example, is in a range of from 5 to 15 degrees with respect to the tyre axial direction.
It is preferable that an inner end in the tire axial direction of at least one of the first shoulder lateral grooves 25 is located in a different position in the tyre circumferential direction from the axially outer ends of the respective first middle lateral grooves 16. In addition, it is preferable that a minimum distance L12 in the tyre circumferential direction between the inner end of the at least one of the first shoulder lateral grooves 25 and the outer ends of the respective first middle lateral grooves 16, for example, is equal to or less than 0.35 times pitch lengths P3 in the tyre circumferential direction of the first shoulder lateral grooves 25. Note that the minimum distance L12 is measured between groove centerlines of the inner end and the respective first shoulder lateral grooves 25. Thus, pumping noise generated when regions of intersections of the first shoulder lateral grooves 25 and the first shoulder main groove 5 come into contact with the ground can be reduced.
Preferably, a length L13 in the tyre axial direction of the shallow bottom portion 26 of the first shoulder lateral grooves 25, for example, is in a range of from 0.20 to 0.30 times the width W3 (shown in
Each second shoulder lateral groove 31, for example, extends from the second tread edge Te2 inwardly in the tyre axial direction and terminates so as to have a terminating end 31a within the second shoulder land portion 14. A length L14 in the tyre axial direction of the second shoulder lateral grooves 31, for example, is in a range of from 0.50 to 0.70 times the width W4 in the tyre axial direction of the second shoulder land portion 14. A groove width of the second shoulder lateral grooves 31, for example, is in a range of from 0.30 to 0.50 times the groove width of the second shoulder main groove 6.
Each connecting sipe 32 extends from the terminating end 31a of a respective one of the second shoulder lateral grooves 31 to the second shoulder main groove 6. A length L15 in the tyre axial direction of the connecting sipes 32, for example, is in a range of from 0.30 to 0.50 times the width W4 in the tyre axial direction of the second shoulder land portion 14. The second shoulder lateral grooves 31 and the connecting sipes 32 can help to ensure stiffness of the second shoulder land portion 14, exerting superior steering stability. In addition, the second shoulder lateral grooves 31 and the connecting sipes 32 can generate less pumping noise, improving noise performance.
Each connecting sipe for example, includes a first portion 32a, a second portion 32b and a third portion 32c which have different depths from one another. The first portion 32a is connected to the second shoulder lateral groove 31. The second portion 32b is connected to the first portion 32a on the second shoulder main groove 6 side and has a depth greater than that of the first portion 32a. The third portion 32c is connected to the second portion 32b on the second shoulder main groove 6 side and has a depth smaller than those of the first portion 32a and the second portion 32b, Such a connecting sipe 32 can mitigate stiffness of the second shoulder land portion 14 moderately, improving steering stability and ride comfort in a well-balanced manner.
In each connecting sipe 32, depths of the first portion 32a and the second portion 32b, for example, are greater than that of the raised portions 19 of the second middle lateral grooves 17. A depth of the third portion 32c of each connecting sipe 32 is preferably smaller than that of the raised portions 19 of the second middle lateral grooves 17. Such a connecting sipe 32 can help to prevent uneven wear of the second shoulder land portion 14.
As illustrated in
Each non-traversing narrow groove 33, for example, extends from the second shoulder main groove 6 and terminates within the second shoulder land portion14. A length L16 in the tyre axial direction of each non-traversing narrow groove 33. for example, is in a range of from 0.50 to 0.65 times the width W4 in the tyre axial direction of the second shoulder land portion 14. The non-traversing narrow grooves 33 configured as such can improve noise performance while ensuring steering stability.
In some preferred embodiments, it is preferable that the length L16 in the tyre axial direction of each non-traversing narrow groove 33 is greater than the length L15 in the tyre axial direction of each connecting sipe 32. Such a non-traversing narrow groove 33 can mitigate stiffness of the second shoulder land portion 14 moderately, improving ride comfort.
It is preferable that the non-traversing narrow grooves 33, for example, are arranged so as to be continuous to the respective second middle lateral grooves 17 smoothly through the second shoulder main groove 6. Such a groove arrangement can help to reduce impact noise since the non-traversing narrow grooves 33 as well as the second middle lateral grooves 17 are easy to open when the second shoulder land portion 14 grounds.
As illustrated in
While the particularly preferable embodiments in accordance with the present disclosure have been described in detail, the present disclosure is not limited to the illustrated embodiments, but can be modified and carried out in various aspects.
Tyres (205/55R16) having the basic tread pattern shown in
rim size: 16×6.5J;
tyre inner pressure: front 200 kPa and rear 200 kPa;
test vehicle: FF vehicle having displacement of 1600 cc; and
tyre location: all wheels.
A test driver drove the above-mentioned test vehicle on a dry road, and evaluated steering stability by the driver's sense when driving in low speed ranges (40 to 80 km/h) and high-speed ranges (100 to 120 km/h). The test results are shown in Table 1 using a score based on Ref. 1 being 100. The larger value indicates better steering stability.
Car interior noise was measured when the above-mentioned test vehicle was traveling on a dry road having bumps at speed ranges between 40 to 100 km/h in order to evaluate the maximum level of sound pressure of frequency ranges between 100 to 350 Hz. The test results are shown in Table 1 using an index based on Ref. 1 being 100. The smaller value indicates better noise performance.
Table 1 shows the test results.
From the test results, it is confirmed that the tyres (Ex. 1 to Ex. 9) improve steering stability and noise performance.
Tyres (205/55R16) having the basic tread pattern shown in
Table 2 shows the test results.
From the test results, it is confirmed that the tyres (Ex. 10 to Ex. prove steering stability and noise performance.
Tyres (205/55R16) having the basic tread pattern shown in
Table 3 shows the test results.
From the test results, it is confirmed that the tyres (Ex. 23 to Ex. 29) improve steering stability and noise performance.
Number | Date | Country | Kind |
---|---|---|---|
2019-023714 | Feb 2019 | JP | national |
2019-023717 | Feb 2019 | JP | national |
2019-023719 | Feb 2019 | JP | national |
2019-066630 | Mar 2019 | JP | national |