Guide wheel, steering bogie, and vehicle
US-2016355059-A1 · Dec 8, 2016 · US
US2023191851A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2023191851-A1 |
| Application number | US-202117924600-A |
| Country | US |
| Kind code | A1 |
| Filing date | Apr 22, 2021 |
| Priority date | May 13, 2020 |
| Publication date | Jun 22, 2023 |
| Grant date | — |
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A tire (10) for a passenger vehicle comprises a tread comprising at least one regulation wear indicator (46) defining a regulation wear threshold, a tread layer (52) comprising an elastomeric tread material exhibiting a complex dynamic shear modulus G*_1 and a dynamic loss tanD0_1, and a backing layer (54) for the tread layer (52) that comprises an elastomeric backing material exhibiting a complex dynamic shear modulus G*_2 and a dynamic loss tanD0_2 such that tanD0_2≥0.37×tanD0_1 and G*2≥0.90×G*1.
Opening claim text (preview).
1 .- 15 . (canceled) 16 . A tire ( 10 ) for a passenger vehicle, the tire comprising a tread ( 14 ) comprising cuts ( 40 ) and tread pattern blocks ( 42 ), the cuts ( 40 ) separating the tread pattern blocks ( 42 ) from one another, the tread ( 14 ) being intended to come into contact with a ground when the tire ( 10 ) is running via a tread surface ( 38 ), the tread ( 14 ) comprising at least one regulation wear indicator ( 46 ) defining a regulation wear threshold, and, in an axially central portion (P 1 ) of the tread ( 14 ) having an axial width (L 1 ) equal to at least 70% of the width (L) of the tread surface ( 38 ), the tread ( 14 ) comprises: a tread layer ( 52 ) bearing the tread surface ( 38 ), the tread layer ( 52 ) comprising an elastomeric tread material exhibiting: a complex dynamic shear modulus G*_1, measured at 10% strain in accordance with standard ASTM D-5992-96, at a temperature of 23° C. and a frequency of 10 Hz, and a dynamic loss tanD0_1, measured in accordance with standard ASTM D-5992-96, at a temperature of 0° C. and a frequency of 10 Hz; a backing layer ( 54 ) for the tread layer ( 52 ) arranged radially on an inside of the tread layer ( 52 ), the backing layer ( 54 ) comprising an elastomeric backing material exhibiting: a complex dynamic shear modulus G*_2, measured at 10% strain in accordance with standard ASTM D-5992-96, at a temperature of 23° C. and a frequency of 10 Hz, and a dynamic loss tanD0_2, measured in accordance with standard ASTM D-5992-96, at a temperature of 0° C. and a frequency of 10 Hz, wherein the elastomeric tread material is different from the elastomeric backing material such that the tread layer ( 52 ) and the backing layer ( 54 ) are contiguous via an interface ( 56 ) describing an interface trajectory ( 58 ) in a meridian section plane comprising the regulation wear indicator ( 46 ), wherein tanD0_2≥0.37×tanD0_1 and G*_2≥0.90×G*_1, wherein, in the axially central portion (P 1 ) of the tread ( 14 ), by defining, in the meridian section plane, a regulation wear trajectory ( 60 ) that is parallel to the tread surface ( 38 ) of the tire ( 10 ) when new and passes through a radially outermost point ( 51 ) of the regulation wear indicator ( 46 ), at least 75% of the length (l) of the interface trajectory ( 58 ) located radially below the tread pattern blocks ( 42 ) is arranged, in the meridian section plane, radially on an inside of the regulation wear trajectory ( 60 ), and wherein, in the axially central portion (P 1 ) of the tread ( 14 ), at least 75% of the length (l) of the interface trajectory ( 58 ) located radially below the tread pattern blocks ( 42 ) is arranged, in the meridian section plane, at a mean radial distance (d 1 ) less than or equal to 2.0 mm from the regulation wear trajectory ( 60 ). 17 . The tire according to claim 16 , wherein tanD0_2≥0.5×tanD0_1. 18 . The tire ( 10 ) according to claim 16 , wherein G*_2≥0.92×G*_1. 19 . The tire ( 10 ) according to claim 16 , wherein, in the axially central portion (P 1 ) of the tread ( 14 ), at least 75% of the length (l) of the interface trajectory ( 58 ) located radially below the tread pattern blocks ( 42 ) is arranged, in the meridian section plane, radially on an outside of a trajectory ( 62 ) which is parallel to the tread surface ( 38 ) of the tire ( 10 ) when new and passes through a radially innermost point ( 48 ) of a or each deepest cut ( 44 ). 20 . The tire ( 10 ) according to claim 16 , wherein, in the axially central portion (P 1 ) of the tread ( 14 ), at least 75% of the length (l) of the interface trajectory ( 58 ) located radially below the tread pattern blocks ( 42 ) is arranged, in the meridian section plane, at a mean radial distance (d 1 ) greater than or equal to 0.4 mm from the regulation wear trajectory ( 60 ). 21 . The tire ( 10 ) according to claim 16 , wherein, in the axially central portion (P 1 ) of the tread ( 14 ), at least a non-zero length (l′) of the interface trajectory ( 58 ) located radially below the tread pattern blocks ( 42 ) is arranged, in the meridian section plane, radially on an outside of the regulation wear trajectory ( 60 ). 22 . The tire according to claim 16 , wherein tanD0_1 ranges from 0.50 to 1.00. 23 . The tire ( 10 ) according to claim 16 , wherein tanD0_2 ranges from 0.60 to 1.10. 24 . The tire ( 10 ) according to claim 16 , wherein G*_1 ranges from 1.30 MPa to 4.10 MPa. 25 . The tire ( 10 ) according to claim 16 , wherein G*_2 is greater than or equal to 2.00 MPa. 26 . The tire ( 10 ) according to claim 16 further comprising a crown ( 12 ) comprising a crown reinforcement ( 16 ) arranged radially on the inside of the tread ( 14 ), wherein, in the axially central portion (P 1 ) of the tread ( 14 ), a mean distance (d 2 ) between a layer ( 28 ) comprising radially outermost reinforcing elements ( 280 ) of the crown reinforcement ( 16 ) and a radially innermost point ( 48 ) of a or each deepest cut ( 44 ) is less than or equal to 2.50 mm. 27 . The tire ( 10 ) according to claim 16 further comprising a crown ( 12 ) comprising a crown reinforcement ( 16 ) arranged radially on the inside of the tread ( 14 ), wherein, in the axially central portion (P 1 ) of the tread ( 14 ), a mean distance (d 2 ) between a layer ( 28 ) comprising radially outermost reinforcing elements ( 280 ) of the crown reinforcement ( 16 ) and a radially innermost point ( 48 ) of a or each deepest cut ( 44 ) is greater than or equal to 1.0 mm. 28 . The tire ( 10 ) according to claim 16 , wherein the elastomeric tread material exhibits a dynamic loss tanDMAX23_1, measured in accordance with standard ASTM D-5992-96, at a temperature of 23° C. and a frequency of 10 Hz, ranging from 0.13 to 0.70. 29 . The tire ( 10 ) according to claim 16 , wherein the elastomeric backing material exhibits a dynamic loss tanDMAX23_2, measured in accordance with standard ASTM D-5992-96, at a temperature of 23° C. and a frequency of 10 Hz, ranging from 0.13 to 0.53. 30 . The tire ( 10 ) according to claim 16 , wherein a surface-area void ratio of the tire ( 10 ) exhibiting a tread pattern height (HS) equal to 2.0 mm after wear ranges from 20% to 35%.
characterised by the tread rubber · CPC title
Wear-indicating arrangements · CPC title
Modulus or tan delta · CPC title
Thickness of the tread · CPC title
with cap and base layers · CPC title
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