Embodiments of the present invention relate generally to methods and apparatus for separating workpieces and, more specifically, to methods for separating workpieces into unit pieces having different sizes, geometries, and the like.
It can be difficult to asymmetrically cut or separate brittle workpieces along a desired separation path. For example, cracks propagating through the workpiece tend to undesirably veer away from the desired separation path when the path is closer to one side of the workpiece than another. This phenomenon is especially noticeable with workpieces formed of chemically strengthened glass, which can have compressive surface stresses of up to 1 GPa. To avoid this problem, workpieces have typically been separated only symmetrically (i.e., by dividing the material into two equal pieces and, if necessary, dividing subsequently formed pieces in half). Separating workpieces by this method, however, can place an unreasonable restriction on the size and shape of the pieces ultimately formed, as well as on the separation process itself.
Embodiments of the present invention are described more fully hereinafter with reference to the accompanying drawings, in which example embodiments of the invention are shown. These embodiments may, however, be implemented in many different forms and should not be construed as limited to the embodiments set forth herein. Rather, the embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the invention to those skilled in the art. In the drawings, the shapes, sizes and relative sizes of layers, regions, components, may be exaggerated for clarity. Unless otherwise specified, a range of values, when recited, includes both the upper and lower limits of the range, as well as any sub-ranges there between.
Referring to
In the illustrated embodiment, the first primary surface region 102 and the second primary surface region are both substantially flat are parallel to one another. Accordingly, the distance from the first primary surface region 102 and the second primary surface region can define the thickness of the workpiece 100. In one embodiment, the thickness of the workpiece is in a range from 200 μm to 10 mm. In another embodiment, however, the thickness of the workpiece can be less than 200 μm or greater than 10 mm. In yet another embodiment, the first primary surface region 102 and the second primary surface region may not be substantially flat, may not be parallel to one another, or a combination thereof.
Generally, the workpiece 100 is formed of a brittle material such as sapphire, silicon, a ceramic, a glass, a glass-ceramic, or the like or a combination thereof. In one embodiment, the workpiece 100 is provided as a sheet of glass (e.g., thermally strengthened glass, chemically strengthened glass, or unstrengthened glass). The sheet of glass can be formed of any glass composition such as soda-lime glass, borosilicate glass, aluminosilicate glass, aluminoborosilicate glass, sodium-aluminosilicate glass, calcium-aluminosilicate glass, phosphate glass, fluoride glass, chalcogenide glass, bulk metallic glass, or the like, or a combination thereof. When the sheet of glass is strengthened, each of the first primary surface region 102 and the second primary surface region can be compressively stressed while a region in the interior of the sheet of glass is in a state of tension to compensate for the surface compression at the first primary surface region 102 and the second primary surface region. Thus, the sheet of strengthened glass can be characterized as including a pair of compression regions (i.e., regions where the glass is in a state of compression) extending from the first primary surface region 102 and the second primary surface region and separated by a central tension region (i.e., a regions where the glass is in a state of tension). The thickness of a compression region is known as the “depth of layer” (DOL).
Generally, the surface compression at each of the first primary surface region 102 and the second primary surface region can be in a range from 69 MPa to 1 GPa. In other embodiments, however, the surface compression at any of the first primary surface region 102 or second primary surface region can be less than 69 MPa or greater than 1 GPa. Generally, the DOL can be in a range from 20 μm to 100 μm. In other embodiments, however, the DOL can be less than 20 μm or greater than 100 μm. The maximum tensile stress of the sheet within the tension region can be determined by the following formula:
CS is the aforementioned surface compression at the first primary surface region 102 and second primary surface region, t is the thickness of the sheet of glass (expressed in millimeters, mm), DOL is the depth of layer of the compression region(s) (expressed in mm), and CT is the maximum central tension within the sheet of glass (expressed in MPa).
Having exemplarily described a workpiece 100 capable of being separated according to embodiments of the present invention, exemplary embodiments of separating the workpiece 100 will now be described. Upon implementing these methods, the workpiece 100 can be separated along a desired separation path such as separation path 108. As exemplarily illustrated, the separation path 108 extends along a straight line, completely between the first pair of edge surface regions 104a and 104b (e.g., between points A and B). In other embodiments, however, the desired separation path may extend along a curved line, may be spaced apart from one or both of the edge surface regions 104a and 104b, or a combination thereof. As exemplarily illustrated, the separation path 108 parallel to the second pair of edge surface regions 106a and 106b such that the separation path 108 is spaced apart from an edge surface region (e.g., edge surface region 106b) by a distance D, wherein D is approximately half of W. In other embodiments, however, that is not parallel to the edge surface region 106a or edge surface region 106b. Further as will be discussed in greater detail below, the distance from which the separation path 108 is spaced apart from edge regions such as edge surface region 106a and 106b may be less than half of W (e.g., in a range from about 1% to about 40% of W).
In one embodiment, the workpiece 100 can be separated along the separation path 108 by first defining the separation path 108. The separation path 108 represents a region within the workpiece 100 having one or properties (e.g., defect density, stress states, temperature, composition, etc.) different from properties in the remaining bulk of the workpiece 100. The property differences are significant enough to guide or otherwise influence the path that a crack (once initiated) will propagate through the workpiece 100. Generally, however, the separation path 108 can be defined by mechanically scribing a portion of one or both of the first and second primary surface regions, chemically etching a portion of one or both of the first and second primary surface regions, heating a portion of one or both of the first and second primary surface regions, cooling a portion of one or both of the first and second primary surface regions, subjecting the workpiece 100 to a bending moment, modifying material within the interior of the workpiece 100 (e.g., as described in International Patent Publication No. WO 2012/006736 A2, which is incorporated herein by reference).
In one embodiment, the separation path 108 can be defined by performing one or more processes as described in any of U.S. Provisional Application No. 61/604,380, filed Feb. 28, 2012, U.S. Provisional Application No. 61/604,416 filed Feb. 28, 2012, U.S. Patent App. Pub. No. 2011/0226832 A1, published Sep. 22, 2011, U.S. Patent App. Pub. No. 2011/0127244 A1, published Jun. 2, 2011, U.S. Patent App. Pub. No. 2011/0049765 A1, published Mar. 3, 2011, U.S. Pat. No. 6,992,026, issued Jan. 31, 2006, U.S. Pat. No. 5,826,772, issued Oct. 27, 1998, all of which are incorporated herein by reference in their entirety. In one embodiment, the separation path 108 can be defined by the directing laser energy onto a portion of the workpiece 100 (e.g., to induce vaporization, ionization, ablation, heating, or the like or a combination thereof, of material within the workpiece 100).
In one embodiment, the laser energy can have one or more wavelengths of light in a range from 100 nm to 11 μm (e.g., 266 nm, 523 nm, 532 nm, 543 nm, 780 nm, 800 nm, 1064 nm, 1550 nm, 10.6 μm, etc.). For example, the laser energy can have one or more wavelengths of light in a range from 100 nm to 11 μm (e.g., 266 nm, 523 nm, 532 nm, 543 nm, 780 nm, 800 nm, 1064 nm, 1550 nm, 10.6 μm, etc.), depending on the material from which the workpiece 100 is formed. In another example, the laser energy can be in form of at least one pulse of light having pulse duration in a range from 10 fs to 500 ns (or less than 10 fs or more than 500 ns) and a pulse repetition rate in a range from 10 Hz to 100 MHz (or less than 10 Hz or more than 100 MHz).
Referring to
Generally, the initiation defect can be defined by mechanically scribing a portion of the workpiece 100 (e.g., at the first primary surface region 102, the second primary surface region, the edge surface region 104b, or the like or a combination thereof) at a location at or near point A, chemically etching a portion of the workpiece 100 (e.g., at the first primary surface region 102, the second primary surface region, the edge surface region 104b, or the like or a combination thereof) heating a portion of the workpiece 100 (e.g., at the first primary surface region 102, the second primary surface region, the edge surface region 104b, or the like or a combination thereof) at a location at or near point A, cooling a portion of the workpiece 100 (e.g., at the first primary surface region 102, the second primary surface region, the edge surface region 104b, or the like or a combination thereof) at a location at or near point A, subjecting a portion of the workpiece 100 (e.g., at the first primary surface region 102, the second primary surface region, the edge surface region 104b, or the like or a combination thereof) at a location at or near point A to a bending moment, modifying material within the interior of the workpiece 100 at a location at or near point A (e.g., as described in International Patent Publication No. WO 2012/006736 A2, which is incorporated herein by reference), or the like, or a combination thereof. In one embodiment, the initiation defect can be formed by applying laser energy onto a portion of the workpiece. In such an embodiment, the laser energy used in forming the initiation defect can have characteristics (e.g., wavelength, pulse duration, pulse repetition rate, or the like or a combination thereof) that are the same as or different from the laser energy characteristics used in defining the separation path 108.
In one embodiment, the initiation defect is configured so that a crack, such as crack 200, having a crack tip 200a extending generally from the first primary surface region 102 to the second primary surface region, propagates through the workpiece 100 (e.g., along the desired separation path from desired start point A to desired end point B, as shown in
In another embodiment, the initiation defect is configured that that a crack such as crack 200 propagates through the workpiece 100 (e.g., along the desired separation path from desired start point A to desired end point B, as shown in
While the workpiece separation process described above with respect to
While not wishing to be bound by any particular theory, the inventors believe that acoustic energy generated at the crack tip 200a (i.e., as the crack 200 propagates through the workpiece 100) is transmitted in one or more directions that are perpendicular to the direction in which the crack 200 propagates. As used herein, the term “acoustic energy” refers to mechanical vibrations within the workpiece 100 generated upon cracking of the material in the workpiece 100 at the crack tip 200a as the crack 200 propagates through the workpiece 200. Thus it is believed that the phenomenon described with respect to
In view of the above, the aforementioned workpiece separation process can, according to one embodiment, further include a process of acoustically contacting at least a portion of the workpiece 100 to an acoustic couplant so as to form an energy transmissive interface that is at least substantially continuous so as to enable acoustic energy generated at the crack tip 200a to be transmitted out of the workpiece 100. For purposes of discussion herein, an energy transmissive interface that is “at least substantially continuous” can be either continuous or discontinuous. However if the energy transmissive interface is discontinuous, any gaps between the acoustic couplant and the workpiece 100 should be sufficiently small so as to not cause any significant reflection of acoustic energy back into the workpiece 100.
Generally, the acoustic impedance of the acoustic couplant at the energy transmissive interface will be greater than that of air at 20° C. and 1 atm (i.e., greater than 400 kg·m−2·s−1). Further, the acoustic impedance of the acoustic couplant at the energy transmissive interface can be selected such that the reflection coefficient, R, at the energy transmissive interface is less than 0.98, less than 0.95, less than 0.9, less than 0.85, less than 0.8, less than 0.5, or even less than 0.3. For purposes of discussion, R, can be calculated as follows:
where Z1 is the acoustic impedance of the workpiece 100, Z2 is the acoustic impedance of the acoustic couplant at the energy transmissive interface. Generally, the acoustic impedance of the acoustic couplant at the energy transmissive interface (i.e., Z2) may be less than or equal to the acoustic impedance of the workpiece (i.e., Z1). In one embodiment, Z2 (when measured at 20° C. and 1 atm) may be in a range from 1·(106) kg·m−2·s−1 to 20·(106) kg·m−2·s−1. In other embodiments, however, the acoustic impedance of the portion of the acoustic couplant at the aforementioned interface may be greater than the acoustic impedance of the workpiece 100.
The acoustic couplant may include one or more materials such as a liquid (e.g., water, oil (e.g., SAE 20), silicone oil, glycerin, propylene glycol, ethylene glycol, or the like or a combination thereof), a gel (e.g., glycerin, honey, or the like or a combination thereof), a grease (e.g., brown grease, silicone grease, petroleum jelly, or the like or a combination thereof), an elastomer compound (e.g., silicone, or the like), an adhesive (e.g., silicone adhesive, hot-melt glue, cyanoacrylate, dental cement, wax beads, or the like or a combination thereof), or the like or a combination thereof. Liquid-based acoustic couplants are generally suitable when the exterior surface of the workpiece 100 is relatively smooth, gels and greases are generally suitable when the exterior surface of the workpiece 100 is relatively rough. If possible, it is desirable to clean the exterior surface of the workpiece 100 to remove dust and other particles that may trap air at the interface between the workpiece 100 and the acoustic couplant.
Referring to
Having exemplarily described exemplary embodiments of a workpiece separation process, exemplary embodiments of an apparatus for separating the workpiece 100 will now be described with reference to
Referring to
In embodiments in which the acoustic couplant 600 is a liquid, gel, grease, or the like, the apparatus 800 may further include a dam 806 configured to retain at least a portion of the acoustic couplant 600 (e.g., to prevent the acoustic couplant 600 from spilling or otherwise flowing undesirably away from the workpiece 100). Although
In one embodiment, the workpiece 100 may be introduced to the apparatus 800 by first disposing the workpiece 100 on the workpiece support 804 such that the first primary surface region 102 faces away from the workpiece support 804 and the second primary surface region faces toward the workpiece support 804, and subsequently contacting a portion of the exterior surface to the acoustic couplant 600 (e.g., the first primary surface region 102, one or more of the edge surface regions, or the like or a combination thereof). In another embodiment, however, the acoustic couplant 600 may first be disposed on the workpiece support 804 (e.g., so as to be retained by the dam 806) and then the workpiece 100 may be disposed on the workpiece support 804 such that the acoustic couplant 600 is disposed between the workpiece 100 and the workpiece support 804. In yet another embodiment, the acoustic couplant 600 may first be disposed on the workpiece 100 and then the workpiece 100 having the acoustic couplant 600 contacted thereto can be disposed on the workpiece support 804.
The foregoing is illustrative of embodiments of the invention and is not to be construed as limiting thereof. Although a few example embodiments of the invention have been described, those skilled in the art will readily appreciate that many modifications are possible in the example embodiments without materially departing from the novel teachings and advantages of the invention. In view of the foregoing, it is to be understood that the foregoing is illustrative of the invention and is not to be construed as limited to the specific example embodiments of the invention disclosed, and that modifications to the disclosed example embodiments, as well as other embodiments, are intended to be included within the scope of the appended claims. The invention is defined by the following claims, with equivalents of the claims to be included therein.
This application is a Non-Provisional application which claims benefit of U.S. Patent Provisional Application Ser. No. 61/704,968, which was filed on 24 Sep. 2012, the contents of which are herein incorporated by reference in their entirety for all purposes.
Number | Date | Country | |
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61704968 | Sep 2012 | US |