Atmospheric plasma treatment of reinforcement cords and use in rubber articles
US-9441325-B2 · Sep 13, 2016 · US
US10695796B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10695796-B2 |
| Application number | US-201715396876-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 3, 2017 |
| Priority date | Jul 1, 2016 |
| Publication date | Jun 30, 2020 |
| Grant date | Jun 30, 2020 |
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A manufacturing method of a long fiber composite material according to an exemplary embodiment of the present invention includes: preparing a main body where inlets and outlets through which a plurality of fiber bundles are respectively charged into and discharged from are formed; adjusting a height of a plurality of first through-hole plates and a height of a second through-hole plate that are disposed in the main body to be the same; having the plurality of fiber bundles penetrated through the first through-hole plate and the second through-hole plate; and adjusting the height of the first through-hole plate and the height of the second through-hole plate to be different from each other after penetrating the plurality of fiber bundles through the first through-hole plate and the second through-hole plate.
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What is claimed is: 1. A manufacturing method of a fiber composite material, comprising: preparing a main body where inlets and outlets through which a plurality of fiber bundles are respectively charged into and discharged from are formed; adjusting a height of a plurality of first through-hole plates and a height of a second through-hole plate that are disposed in the main body to be the same; having the plurality of fiber bundles penetrated through the first through-hole plate and the second through-hole plate; and adjusting the height of the plurality of first through-hole plates and the height of the second through-hole plate to be different from each other after the plurality of fiber bundles penetrate through the plurality of first through-hole plates and the second through-hole plate, wherein a second hole through which the plurality of fiber bundles are penetrated is provided in the second through-hole plate, and has a predetermined length, and wherein a plurality of protrusions are formed only in an inner wall of the second hole, and arranged along a length direction of the second hole, wherein the second through-hole plate is disposed between a pair of first through-hole plates that are adjacent to each other among the plurality of first through-hole plates. 2. The manufacturing method of the fiber composite material of claim 1 , after the adjusting of the height of the first through-hole plate and the height of the second through-hole plate to be different from each other, further comprising moving the plurality of fiber bundles in a direction of the outlet from the inlet. 3. The manufacturing method of the fiber composite material of claim 1 , wherein in the adjusting of the heights of the first and second through-hole plates, the plurality of fiber bundles that penetrate the first through-hole plate and the second through-hole plate are adjusted to a straight line. 4. The manufacturing method of the fiber composite material of claim 1 , wherein, in the adjusting of the heights of the first and second through-hole plates, the second through-hole plate is disposed at a height that is lower than that of the first through-hole plate. 5. The manufacturing method of the fiber composite material of claim 1 , wherein, in the adjusting of the heights of the first and second through-hole plates, the second through-hole plate is disposed at a height that is higher than that of the first through-hole plate. 6. The manufacturing method of the fiber composite material of claim 1 , wherein the plurality of first through-hole plates are disposed in parallel with each other along a first direction in the main body, and a plurality of first holes through which the plurality of fiber bundles are formed in the respective first through-hole plates. 7. The manufacturing method of the fiber composite material of claim 6 , wherein the plurality of first holes have circular-shaped cross-sections. 8. The manufacturing method of the fiber composite material of claim 6 , wherein the plurality of fiber bundles penetrated through the first through-hole plate penetrate the second through-hole plate. 9. The manufacturing method of the fiber composite material of claim 1 , wherein the plurality of protrusions have curved shapes. 10. The manufacturing method of the fiber composite material of claim 1 , wherein the second hole is provided in plural. 11. The manufacturing method of the fiber composite material of claim 1 , wherein the second through-hole plate is provided in plural.
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