Claims
- 1. A method of separating a brittle material along a scribe line on said brittle material comprising heating said brittle material on the scribe line, to one side of said scribe line, or on both sides of said scribe line, whereby to establish a greater temperature differential in said material across said scribe line.
- 2. The method according to claim 1, wherein said heating comprises the application of a high energy beam.
- 3. The method according to claim 2, wherein said high energy beam comprises a laser.
- 4. The method according to claim 3, wherein said heating comprises the I 1 application of said laser energy proximate to an outer surface of said brittle material.
- 5. The method according to claim 3, wherein said heating comprises the application of said laser energy to the interior of said brittle material.
- 6. The method according to claim 3, wherein said laser comprises a carbon dioxide laser.
- 7. The method according to claim 3, wherein said laser comprises a Nd:YAG laser.
- 8. The method according to claim 1, wherein said heating comprises impinging said brittle material with a heated fluid.
- 9. The method according to claim 1, wherein said heating comprises application of infrared energy.
- 10. The method according to claim 1, wherein said heating comprises application of ultraviolet or shorter wavelength energies.
- 11. The method according to claim 1, wherein said scribe line comprises a micro-crack.
- 12. The method according to claim 1, wherein said brittle material is a material selected from the group consisting of a mineral glass, vitreous silica, a metal glass, a ceramic, and a crystalline material.
- 13. A method of separating a part of a brittle material, said part being captured in a “closed shape”, along a closed scribe line, such scribe line closing on itself and not necessarily opening to an outside surface—or vent, on said brittle material comprising chilling said brittle material to one side of said scribe line, whereby to establish a temperature differential in said material across said scribe line.
- 14. A method according to claim 13, wherein said one side comprises an inner side, whereby a higher temperature is caused to exist on an outside surface and a lower temperature on an inside surface of said part.
- 15. A method according to claim 13, wherein said scribe line is chilled to the part side of the material.
- 16. The method according to claim 13 wherein said scribe line comprises a micro-crack.
- 17. The method according to claim 13, wherein said chilling comprises applying a chilled fluid to the surface of the brittle material.
- 18. The method according to claim 15, wherein said chilled fluid is selected from chilled air, dry liquid nitrogen, and gasified liquid nitrogen.
- 19. The method according to claim 15, wherein said chilled fluid comprises carbon dioxide.
- 20. The method according to claim 15, wherein said chilled fluid comprises fluidized solid carbon dioxide “snow”.
- 21. The method according to claim 13, wherein said material is chilled by application of a low boiling temperature material to the surface of the brittle material.
- 22. The method according to claim 13, wherein said material is chilled by a thermoelectric cooling apparatus.
- 23. The method according to claim 13, wherein said chilling comprises the use of a thermo-mechanical apparatus.
- 24. A method of separating a closed shape brittle material along a scribe line on said brittle material comprising heating said brittle material to an outer side of said scribe line to a higher temperature than an inner side of said scribe line, whereby a temperature differential is established across said scribe line.
- 25. The method according to claim 24, wherein said heating is to an outer side of said scribe line and an inner side of said scribe line is chilled.
- 26. The method according to claim 24, wherein said inner side of said scribe line and said outer side of said scribe line are both heated, and wherein the outer side is heated to a higher temperature than the inner side.
- 27. The method according to claim 24, wherein said scribe line comprises a micro-crack.
- 28. The method according to claim 24, wherein said heating comprises the application of a high energy beam.
- 29. The method according to claim 24, wherein said high energy beam comprises a laser.
- 30. The method according to claim 24, wherein said heating comprises the application of said laser energy proximate to an outer surface of said brittle material in a closed shape.
- 31. The method according to claim 24, wherein said heating comprises the application of said laser energy to the interior of said brittle material in a closed shape.
- 32. The method according to claim 29, wherein said laser comprises a carbon dioxide laser or Nd:YAG laser.
- 33. The method according to claim 24, wherein said heating comprises impinging said brittle material with a heated gas.
- 34. The method according to claim 24, wherein said heating comprises application of infrared energy.
- 35. The method according to claim 24, wherein said chilling comprises applying a chilled gas to the surface of the brittle material.
- 36. The method according to claim 35, wherein said chilled gas comprises chilled air.
- 37. The method according to claim 35, wherein said chilled gas comprises dry liquid nitrogen or gasified liquid nitrogen.
- 38. The method according to claim 35, wherein said chilled gas comprises carbon dioxide.
- 39. The method according to claim 24, wherein said chilling comprises the application of a low boiling temperature material to the surface of the brittle material.
- 40. The method according to claim 24, wherein said chilling comprises the use of a thermoelectric cooling apparatus.
- 41. The method according to claim 24, wherein said chilling comprises the use of a thermo-mechanical apparatus.
- 42. The method according to claim 24, wherein said heating occurs prior to said chilling.
- 43. The method according to claim 24, wherein said heating occurs subsequent to or generally simultaneously with said chilling.
- 44. A method of separating a brittle material along a scribe line comprising, prior to forming said scribe line, applying a gassing tape to a surface of the brittle material such that said gassing tape is at least partially disposed beneath said scribe line, and causing said gassing tape to out-gas a gaseous substance generally beneath said scribe line, whereby said gaseous substance generates sufficient mechanical pressure to fracture said brittle material along said scribe line.
- 45. The method according to claim 44, wherein said gassing tape is thermally activated.
- 46. The method according to claim 45, wherein said scribe line comprises a micro-crack produced by laser scribing, and wherein said laser scribing provides sufficient heat to said gassing tape to produce said out-gassing.
- 47. The method according to claim 44, wherein said gassing tape is activated by exposure to radiation of a predetermined wavelength.
- 48. The method according to claim 47, wherein said out-gassing is produced by impinging said gassing tape along said scribe line with a laser at said predetermined wavelength.
- 49. The method according to claim 47, wherein said gassing tape is activated by exposure to infrared radiation.
- 50. The method according to claim 47, wherein said gassing tape is activated by exposure to ultraviolet radiation.
- 51. The method according to claim 44, wherein said gassing tape comprises a single-sided tape.
- 52. The method according to claim 51, wherein said single-sided tape comprises a paper backing.
- 53. The method according to claim 51, wherein said single-sided tape comprises a polymer backing.
- 54. The method according to claim 44, wherein said gassing tape comprises a double sided tape.
- 55. A method for separating a brittle material, in a closed shape, along a scribe line comprising ultrasonically energizing said brittle material to one side of said scribe line.
- 56. The method according to claim 55, wherein said scribe line defines a locked workpiece, closed shape, and wherein said locked workpiece is ultrasonically energized.
- 57. The method according to claim 55, comprising mechanically coupling an ultrasonic horn to said brittle material on one side of said scribe line, wherein said ultrasonic horn is ultrasonically energized, whereby said ultrasonic horn ultrasonically energizes said brittle material.
- 58. The method according to claim 55, further comprising applying a force to said brittle material in a direction normal to the plane of said brittle material.
- 59. The method according to claim 58, wherein said force is applied to said brittle material through said ultrasonic horn.
- 60. The method according to claim 58, wherein said force is applied by a fluid expelled through a port in said ultrasonic horn.
- 61. The method according to claim 59 wherein said ultrasonic horn is coupled to said brittle material by a vacuum port in said ultrasonic horn, and wherein said force is applied by moving said ultrasonic horn away from said brittle material.
- 62. The method according to claim 57, further comprising urging said ultrasonic horn into contact with a surface of said brittle material, whereby said force is applied to said brittle material.
- 63. The method according to claim 57, further comprising applying a pressurized fluid to a surface of said brittle material opposite said ultrasonic horn, whereby said normal force is applied to said brittle material.
- 64. The method according to claim 55, further comprising ultrasonically energizing a fluid and impinging said brittle material with said fluid, whereby said fluid applied to said brittle material is ultrasonically energized.
- 65. The method according to claim 64, wherein said fluid impinging said brittle material applies a normal force to said brittle material.
- 66. The method according to claim 65, wherein said fluid comprises a stream of a liquid or a gas directed at said brittle material.
- 67. An apparatus for separating a brittle material along a scribe line comprising an ultrasonic generator coupled to an ultrasonic horn, said ultrasonic horn in turn being mechanically coupled to said brittle material about a contact face of said ultrasonic horn.
- 68. The apparatus according to claim 67, wherein said ultrasonic horn comprises at least one vacuum port on said contact face for applying a vacuum force to said brittle material relative to said contact face.
- 69. The apparatus according to claim 67, wherein said ultrasonic horn comprises at least one fluid port on said contact face, wherein said at least one fluid port is coupled to a fluid supply, whereby a fluid may be expelled from said at least one fluid port, therein applying a force on said brittle material.
- 70. An apparatus for separating a brittle material along a scribe line including a supply of pressurized fluid coupled to at least one nozzle, wherein said nozzle comprises an ultrasonic transducer coupled to an ultrasonic generator for ultrasonically exciting a stream of fluid passing through said at least one nozzle.
- 71. The apparatus according to claim 70, wherein said supply of pressurized fluid comprises a gas.
- 72. The apparatus according to claim 70, wherein said supply of pressurized fluid comprises a liquid.
- 73. A method of separating a brittle material along a micro-crack scribe line comprising directing a stream of pressurized fluid into and along said micro-crack, whereby sufficient fluid-dynamic force is generated to separate said brittle material along said micro-crack.
- 74. The method according to claim 73, wherein said pressurized fluid comprises a pressurized gas.
- 75. The method according to claim 74, wherein said pressurized gas is at a pressure of about 60-120 psi.
- 76. The method according to claim 74, wherein said pressurized gas is directed at an angle of attack of 30 to 60 degrees.
- 77. The method according to claim 76, wherein said pressurized gas is directed at an angle of attack of about 45 degrees.
- 78. An apparatus for separating a brittle material along a micro-crack scribe line, including a nozzle configured to selectively dispense a low pressure cooling medium during a laser cutting process, and a high pressure stream of gas, wherein the high pressure stream of gas is capable of generating sufficient aerodynamic force to separate said brittle material along said scribe line.
- 79. A method of separating a brittle material along a micro-crack scribe line comprising directing a stream of pressurized gas into and along said micro-crack, wherein said stream of pressurized gas is excited in a stream of ultrasonic pulses.
- 80. An apparatus for separating a brittle material along a micro-crack scribe line comprising a nozzle coupled to a supply of pressurized gas, and an ultrasonic transducer coupled to said nozzle for energizing a stream of pressurized gas passing through said nozzle in ultrasonic pulses.
- 81. A method of forming a micro-crack in a brittle material comprising heating said brittle material along a desired cut path with a composite footprint energy pattern comprising at least a first and a second incident energy beam respectively projecting at least a first and a second incident footprint.
- 82. The method according to claim 81, wherein said composite footprint is generally symmetrical about said desired cut path.
- 83. The method according to claim 81, wherein said at least first and second incident energy beams comprise laser beams.
- 84. The method according to claim 81, wherein said at least first and second incident footprints are non-overlapping.
- 85. The method according to claim 81, wherein said at least first and second incident footprints each have an energy distribution that is generally Gaussian in form across the width of each footprint.
- 86. The method according to claim 81, wherein said at least first and second incident footprints are at least partially overlapping, therein defining a region of overlap.
- 87. The method according to claim 81, wherein said composite footprint has a net energy distribution that is an aggregate of the individual energy distributions of said at least first and second incident footprints, and wherein said energy distributions of said at least first and second incident footprints are accumulative in said region of overlap.
- 88. The method according to claim 87, wherein said net energy distribution of said composite footprint has a tri-modal configuration, wherein the center peak of said net energy distribution is generally aligned with said cut path.
- 89. The method according to claim 87, wherein said net energy distribution has a head and shoulders configuration, whereby a dominant energy peak is generally aligned with said cut path, and a first and a second secondary peak are respectively disposed on either side of said dominant peak.
- 90. An apparatus for inducing a micro-crack in a brittle material comprising a source for at least a first and a second energy beam, and a targeting optic configured to direct said at least first and second energy beam to impinge said brittle material.
- 91. The apparatus according to claim 90, wherein said source for at least a first and a second energy beam comprises at least a first and a second energy beam source.
- 92. The apparatus according to claim 90, wherein said source for at least a first and a second energy beam comprises a single energy beam source emitting a single energy beam, wherein said single energy beam is split into at least a first and a second separate energy beam.
- 93. The apparatus according to claim 90, wherein said targeting optic comprises a V mirror.
- 94. The apparatus according to claim 93, wherein said V mirror comprises at least two independent variable angle mirrors.
- 95. The apparatus according to claim 90, wherein said targeting optic comprises a prism.
- 96. The apparatus according to claim 90, further comprising at least a first and a second shift mirror configured to direct said at least first and second energy beam to said targeting optic.
- 97. The apparatus according to claim 90, wherein said targeting optic is configured to direct said at least first and second energy beam along respective parallel paths.
- 98. The apparatus according to claim 90, wherein said source for at least a first and a second energy beam comprises a laser source.
CROSS REFERENCE TO RELATED APPLICATIONS
[0001] This applications claims benefit of U.S. Provisional Application Serial Nos. 60/203,289, 60/204,099, 60/204,109 and 60/204,110, filed May 11, 2000, May 15, 2000, May 15, 2000 and May 15, 2000 respectively.
Provisional Applications (4)
|
Number |
Date |
Country |
|
60203289 |
May 2000 |
US |
|
60204099 |
May 2000 |
US |
|
60204109 |
May 2000 |
US |
|
60204110 |
May 2000 |
US |