METHOD AND APPARATUS FOR FORMING A COMPOSITE APEX
20200198412 ยท 2020-06-25
Inventors
- Hongbing Chen (Broadview Heights, OH, US)
- Christopher David Dyrlund (Canton, OH, US)
- Adam Mark Baldan (Akron, OH, US)
Cpc classification
B60C13/02
PERFORMING OPERATIONS; TRANSPORTING
B29D30/48
PERFORMING OPERATIONS; TRANSPORTING
B60C2001/0058
PERFORMING OPERATIONS; TRANSPORTING
B60C2015/061
PERFORMING OPERATIONS; TRANSPORTING
B29D2030/482
PERFORMING OPERATIONS; TRANSPORTING
B60C15/0607
PERFORMING OPERATIONS; TRANSPORTING
International classification
B60C15/06
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A method for forming a composite apex, the method comprising the steps of: forming a coextruded strip of a first compound and a second compound, wherein the second compound is a compound different than the first compound, wherein the apex is formed from winding the coextruded strip while varying the ratio of the first compound to the second compound.
Claims
1. A method for forming a composite apex, the method comprising the steps of: forming a coextruded strip of a first compound and a second compound, wherein the second compound is a compound different than the first compound, wherein the apex is formed from winding the coextruded strip while varying the ratio of the first compound to the second compound.
2. The method of claim 1 wherein the radially outer portion of the apex is 100% of the second compound.
3. The method of claim 1 wherein the radially inner portion of the apex is formed from a coextruded strip having a ratio of 95% of the first compound and 5% of the second compound.
4. The method of claim 1 wherein the apex is formed from a dual layer of strip lamination.
5. The method of claim 1 wherein the second compound is selected for high stiffness.
6. The method of claim 1 wherein the coextruded strip is formed by: extruding a first compound through a first extruder and a first gear pump and into a first passageway of a coextrusion nozzle; extruding a second compound through a second extruder and a second gear pump and into a second passageway of the coextrusion nozzle; and wherein the first and second passageways are joined together immediately upstream of the die outlet of the coextrusion nozzle.
7. The method of claim 6 wherein the coextrusion nozzle has an insert which divides the nozzle into a separate first and second passageway.
8. The method of claim 7 wherein the insert has a distal end for positioning adjacent a die outlet of the coextrusion nozzle, wherein the distal end has an elongated flat portion.
9. The method of claim 1 wherein the ratio of the volume of the first compound to the volume of the second compound is varied by changing the ratio of the speed of the first gear pump to the second gear pump.
10. The method of claim 6 wherein the ratio of the first gear pump to the second gear pump may be varied during operation of the system.
11. The method of claim 7 wherein the insert is removable.
12. The method of claim 7 wherein the insert has a rectangular cross-sectional shape.
13. The method of claim 1 wherein the strip is formed in a continuous manner.
14. The method of claim 1 wherein the strip is applied in a continuous manner to a tire building machine to build a tire component.
15. A method for forming a tire component, the method comprising the steps of: providing a tire, forming a coextruded strip of a first compound and a second compound, wherein the second compound is a compound different than the first compound, wherein the tire component is formed from winding the coextruded strip onto the tire building drum while varying the ratio of the first compound to the second compound.
16. The method of claim 1 wherein the second compound comprises a rubber composition having a shear storage modulus G measured at 1% strain and 100 C. according to ASTM D5289 ranging from 23 to 31 MPa.
17. The method of claim 1 wherein the first compound comprises a rubber composition having a shear storage modulus G measured at 1% strain and 100 C. according to ASTM D5289 ranging from 1.4 to 2.3 MPa.
18. The method of claim 1 wherein the radially outer strip windings have an axis X-X oriented in the radial direction.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0020] The invention will be described by way of example and with reference to the accompanying drawings in which:
[0021]
[0022]
[0023]
[0024]
[0025]
[0026]
[0027]
[0028]
DETAILED DESCRIPTION OF THE INVENTION
[0029]
[0030]
[0031] The first layer 212 is formed from a first rubber compound which is typically used to form an apex. The second compound is preferably a rubber compound preferably having high stiffness properties. The first and second rubber compounds of the strip are formed in discrete layers 212,214, and thus are not mixed together.
[0032] The first layer thickness of the first compound is preferably in the range of about 0.3 mm to about 2 mm, and more preferably in the range of about 0.6 to about 1.2 mm. The second layer thickness of the second compound preferably has a thickness in the range of about 0.01 mm to about 0.2 mm, more preferably about 0.01 mm to about 0.1 mm. The overall width of the strip 230 is in the range of about 10 mm to about 50 mm, more preferably 20-40 mm. The term about as used herein means a variation of +/10%.
[0033] The coextruded strip 210 shown in
[0034] The coextruded strip forming apparatus 10 is used to form the desired apex profile 200 shown in
[0035] The stiffness may be characterized by the dynamic modulus G, which are sometimes referred to as the shear storage modulus or dynamic modulus, reference may be made to Science and Technology of Rubber, second edition, 1994, Academic Press, San Diego, Calif., edited by James E. Mark et al, pages 249-254. The shear storage modulus (G) values are indicative of rubber compound stiffness which can relate to tire performance. The tan delta value at 100 C. is considered as being indicative of hysteresis, or heat loss.
[0036] In a first embodiment, the second rubber compound comprises a stiff rubber composition having a shear storage modulus G measured at 1% strain and 100 C. according to ASTM D5289 ranging from 18 to 32 MPa, and the first rubber compound comprises a rubber composition having a shear storage modulus G measured at 1% strain and 100 C. according to ASTM D5289 ranging from 1.2 to 10 MPa. In a more preferred embodiment, the second rubber compound comprises a rubber composition having a shear storage modulus G measured at 1% strain and 100 C. according to ASTM D5289 ranging from 23 to 31 MPa, and the first rubber compound comprises a rubber composition having a shear storage modulus G measured at 1% strain and 100 C. according to ASTM D5289 ranging from 1.4 to 2.3 MPa.
Coextruded Strip Forming Apparatus
[0037] As shown in
[0038] The first compound is extruded by the first extruder 30 and then pumped by the first gear pump 42 into a nozzle 100, while at the same time the second compound is extruded by the second extruder 60 and then pumped by the second gear pump 44 into the coextrusion nozzle 100.
[0039] The coextrusion nozzle 100 has a removable insert 120 that functions to divide the nozzle into a first and second flow passageway 122,124. The removable insert 120 is preferably rectangular in cross-sectional shape. The removable insert 120 has a distal end 130 with tapered ends 132,134 forming a nose 136. The nose 136 is positioned adjacent the nozzle die exit 140 and spaced a few millimeters from the die exit 140. The region between the nose 136 and the die exit 140 is a low volume coextrusion zone 150 that is high pressure. In the low volume coextrusion zone 150, the first compound flowstream 122 merges with the second compound flowstream 124 forming two discrete layers 212,214 joined together at an interface 215.
[0040] The coextrusion nozzle 100 is preferably mounted upon a rotatable head 70.
[0041] The volume ratio of the first compound to the second compound may be changed by varying the ratio of the speed of the first gear pump of the first compound to the speed of the second gear pump of the second compound. The dual coextruded strip forming apparatus 10 can adjust the speed ratios on the fly, and due to the small residence time of the coextrusion nozzle, the apparatus has a fast response to a change in the compound ratios. This is due to the low volume of the coextrusion zone.
[0042] Variations in the present inventions are possible in light of the description of it provided herein. While certain representative embodiments and details have been shown for the purpose of illustrating the subject invention, it will be apparent to those skilled in this art that various changes and modifications can be made therein without departing from the scope of the subject invention. It is, therefore, to be understood that changes can be made in the particular embodiments described which will be within the full intended scope of the invention as defined by the following appended claims.