US2016347639A1PendingUtilityA1
Method and apparatus for making a glass laminate
Est. expiryOct 6, 2028(~2.2 yrs left)· nominal 20-yr term from priority
C03C 3/093C03C 3/091C03C 1/00C03B 17/068C03B 17/067C03B 17/02B32B 17/06C03B 17/064
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Claims
Abstract
An apparatus for making a glass laminate, including: a source of a glass core sheet; a source of a first force that tensions the glass core sheet in a first axial direction; a source of a second force that tensions the glass core sheet in a second axial direction; and at least one molten glass reservoir extending along a length of the apparatus and on opposite sides of the glass core sheet that delivers a source of at least two glass dads to the opposite side surfaces of the bi-axially tensioned glass core sheet. Also disclosed are methods for making a glass laminate sheet using the disclosed apparatus, as defined herein.
Claims
exact text as granted — not AI-modifiedWhat is claimed is:
1 . An apparatus for making a glass laminate comprising:
a source of a glass core sheet; a source of a first force that produces a first tension on the glass core sheet in a first axial direction; a source of a second force that produces a second tension on the glass core sheet in a second axial direction; and at least one molten glass reservoir extending along a length of the apparatus and on opposite sides of the glass core sheet that delivers a source of at least two glass dads to the surface of the first and second axially tensioned glass core sheet.
2 . The apparatus of claim 1 further comprising the at least one molten glass reservoir having a pass-through region situated between the source of at least two glass dads.
3 . The apparatus of claim 1 wherein the first axial direction and the second axial direction are orthogonal.
4 . The apparatus of claim 1 wherein the source of the first force and the source of the second force, when applied to the core glass sheet, produce a biaxial tension on the core glass sheet.
5 . The apparatus of claim 1 wherein the source of the glass core sheet is selected from at least one of: a preformed sheet; a sheet generated in situ; or a combination thereof.
6 . The apparatus of claim 1 wherein the source of the glass core sheet is static, semi-static, or dynamic.
7 . The apparatus of claim 1 wherein the CTE of the core sheet (CTE core ) is greater than the CTE of the clad layer (CTE clad ), and the difference CTE clad −CTE core is less than 10×10 −7 /° C.
8 . The apparatus of claim 1 wherein the glass laminate has a compressive stress strength of from 20 to 50 MPa, and the glass laminate is at least one of: alkali-free, a high scratch resistant surface having a Knoop scratch threshold larger than 5 Newton, is free of ion-exchange, or a combination thereof.
9 . A method for strengthening a glass laminate, the glass laminate having a glass core sheet and at least one glass clad layer on at least one of the opposite sides of the glass core sheet, comprising:
heating the glass laminate, the glass laminate having the glass core sheet has a strain point having a difference of at least 50° C. compared to the strain point of the at least one glass clad layer; applying biaxial force to the glass core sheet while the glass clad layers are in a state of stress relaxation; cooling the glass laminate; and releasing the biaxial force on the glass core sheet.
10 . The method of claim 9 wherein the strengthened glass laminate has a compressive stress on the clad layers that is increased by from 10 MPa to 200 MPa compared to an un-strengthened glass laminate.
11 . The method of claim 9 wherein heating the glass laminate is accomplished at from 560 to 600° C.
12 . A method for strengthening a glass laminate, the glass laminate having a glass core sheet and a glass clad layer on at least one of the opposite sides of the glass core sheet, comprising:
a first heating of the glass laminate to 50° C. below the strain point of the glass core sheet, and the glass core sheet has a strain point of at least 50° C. higher than the strain point of the glass clad layer; a second heating of the glass laminate to between the anneal point of the glass clad and the strain point of the glass core sheet, the second heating is accomplished at a temperature above the strain point of the clad layer and below the strain point of the core sheet; bi-axially tensioning the second heated glass laminate at from 10 to 50 MPa for a sufficient time for the stress in the clad layers to relax; cooling the laminate to ambient temperature; and removing the bi-axial tensioning.
13 . The method of claim 12 wherein removing the bi-axial tensioning creates a compressive stress on glass clad layers.
14 . A method for strengthening a glass laminate, the glass laminate having a glass core sheet and a glass clad layer on at least one of the opposite sides of the glass core sheet, comprising:
contacting the opposite sides of a biaxially tensioned core glass sheet with molten clad glass from a source of molten clad glass.
15 . The method of claim 14 wherein the glass laminate strengthening is accomplished free of a CTE mismatch condition.
16 . The method of claim 14 wherein the source of molten clad glass is a modified fusion draw apparatus.
17 . The method of claim 14 wherein the biaxially tensioned core glass sheet is a preformed single sheet, or is continuously produced in situ by a modified double fusion draw apparatus.
18 . A glass laminate article comprising:
a glass core sheet; and at least one glass clad layer on at least one side of the glass core sheet, wherein the glass laminate article is birefringent.
19 . The article of claim 18 wherein the birefringent property is not attributable to:
thermal tempering, a polymer, an anisotropic additive, or any combination thereof.Cited by (0)
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