Edge chamfering by mechanically processing laser cut glass
US-2017008793-A1 · Jan 12, 2017 · US
US10118255B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10118255-B2 |
| Application number | US-201615086062-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 31, 2016 |
| Priority date | Mar 31, 2015 |
| Publication date | Nov 6, 2018 |
| Grant date | Nov 6, 2018 |
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A cutting method of a multilayer structure containing a brittle layer is provided. The cutting method includes: cutting the multilayer structure to form a cut edge; removing a material of the multilayer structure other than the brittle layer along the cut edge, wherein the material of the multilayer structure other than the brittle layer has a width ranging from 1 micron to 2 millimeter; and modifying an edge of the brittle layer remaining after removing the material of the multilayer structure other than the brittle layer by a laser beam.
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What is claimed is: 1. A cutting method of a multilayer structure containing a brittle layer, the cutting method comprising: cutting the multilayer structure to form a cut edge; removing a material of the multilayer structure other than the brittle layer along the cut edge, wherein the material of the multilayer structure other than the brittle layer has a width ranging from 1 micron to 2 millimeter; and modifying an edge of the brittle layer remaining after removing the material of the multilayer structure other than the brittle layer by a laser beam. 2. The cutting method according to claim 1 , wherein modifying the edge of the brittle layer by the laser beam comprises: causing the laser beam to strike the edge of the brittle layer adjacent to the cut edge so as to peel off a layer of chippings at the edge of the brittle layer. 3. The cutting method according to claim 2 , wherein the laser beam strikes at least one of a top surface and a bottom surface of the brittle layer, and the top surface and the bottom surface are arranged along a thickness direction of the brittle layer. 4. The cutting method according to claim 2 , wherein a spot of the laser beam on the brittle layer satisfies 0.5≤b/a≤2, where a is a diameter of the spot of the laser beam on a surface of the brittle layer, and b is the distance from the center of a focus of the laser beam to the edge of the brittle layer along a direction perpendicular to a thickness direction of the brittle layer. 5. The cutting method according to claim 2 further comprising: controlling a scanning path and a scanning speed of the laser beam striking on the brittle layer and allowing the laser beam to complete the scanning path. 6. The cutting method according to claim 5 , wherein scanning of the laser beam starts at a straight path segment or a convex path segment of the scanning path. 7. The cutting method according to claim 5 , wherein the scanning speed of the laser beam on a surface of the brittle layer ranges from 10 mm/s to 100 mm/s. 8. The cutting method according to claim 2 , wherein an average power of the laser beam on a surface of the brittle layer ranges from 1 W to 50 W. 9. The cutting method according to claim 2 , a diameter of a spot of the laser beam on a surface of the brittle layer ranges from 50 microns to 1000 microns. 10. The cutting method according to claim 1 , wherein the laser beam generates an strain area on the brittle layer along the edge of the brittle layer, and a strain propagates chippings at the edge of the brittle layer along the edge of the brittle layer, so as to peel off a layer of chippings at the edge of the brittle layer, thereby modifying the edge of the brittle layer. 11. The cutting method according to claim 1 , wherein the brittle layer is a glass layer or a ceramic layer. 12. The cutting method according to claim 1 , wherein the multilayer structure further contains an adhesive layer and a polymeric layer, and the adhesive layer is disposed between the brittle layer and the polymeric layer, and removing the material of the multilayer structure other than the brittle layer along the cut edge comprises removing a material of the adhesive layer and a material of the polymeric layer. 13. The cutting method according to claim 1 further comprising: disposing at least one protective film on at least one side of the multilayer structure before modifying the edge of the brittle layer by the laser. 14. The cutting method according to claim 13 , wherein the protective film is made of polyethylene terephthalate (PET), polyethylene naphthalate (PEN), polycarbonate (PC), or a combination thereof. 15. The cutting method according to claim 1 , wherein a wavelength of the laser beam ranges from 3 microns to 12 microns. 16. The cutting method according to claim 1 , wherein a thickness of the brittle layer ranges from 1 micron to 1 millimeter. 17. The cutting method according to claim 1 , wherein a size of chippings at the edge of the brittle layer formed after cutting the multilayer structure is controlled so that a width of a layer of the chippings ranges from 1 microns to 2 millimeters. 18. The cutting method according to claim 1 , wherein a width of chippings at the edge of the brittle layer formed after cutting the multilayer structure is controlled to be smaller than twice a thickness of the brittle layer. 19. A cutting method of a multilayer structure containing a brittle layer, the cutting method comprising: cutting the multilayer structure to form a cut edge; and causing a laser beam to strike an edge of the brittle layer adjacent to the cut edge so as to peel off a layer of chippings at the edge of the brittle layer, wherein a spot of the laser beam on the brittle layer satisfies 0.5≤b/a≤2, where a is a diameter of the spot of the laser beam on a surface of the brittle layer, and b is the distance from the center of a focus of the laser beam to the edge of the brittle layer along a direction perpendicular to a thickness direction of the brittle layer. 20. The cutting method according to claim 19 , wherein the laser beam generates an strain area on the brittle layer along the edge of the brittle layer, and a strain propagates chippings at the edge of the brittle layer along the edge of the brittle layer, so as to peel off the layer of chippings at the edge of the brittle layer, thereby modifying the edge of the brittle layer. 21. The cutting method according to claim 19 , wherein the brittle layer is a glass layer or a ceramic layer. 22. The cutting method according to claim 19 further comprising: disposing at least one protective film on at least one side of the multilayer structure before causing the laser beam to strike the edge of the brittle layer adjacent to the cut edge.
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