Claims
- 1. A glass substrate machining method comprising the steps of:
a) preparing a glass substrate in which an amount of air bubbles in said glass substrate is controlled to improve the workability of said glass substrate; b) machining said glass substrate by using a laser to make a hole or a groove in said glass substrate.
- 2. A glass substrate machining method comprising the steps of:
a) preparing a glass substrate in which an amount of air bubbles in said glass substrate is controlled to improve the workability of said glass substrate; b) forming a thin insulator on a surface of said glass substrate; c) machining said glass substrate by using a laser to make a hole or a groove in said glass substrate.
- 3. The glass substrate machining method according to claim 2, wherein said thin insulator on said glass surface is glass formed by coating said surface.
- 4. The glass substrate machining method according to claim 2, wherein said thin insulator formed on said glass surface is an organic insulator film.
- 5. The glass substrate machining method according to claim 4, wherein said thin organic insulator on said glass surface is formed by coating said surface.
- 6. The glass substrate machining method according to claim 4, wherein said thin insulator on said glass surface is united with said glass substrate into a sheet form by lamination therewith.
- 7. The glass substrate machining method according to claim 1, wherein a CO2 laser is used to perform the laser machining.
- 8. The glass substrate machining method according to claim 2, wherein a CO2 laser is used to perform the laser machining.
- 9. A glass substrate machining method comprising the steps of:
machining a glass substrate by using a laser; controlling an amount of air bubbles in a glass substrate so that said glass substrate, after said laser machining, has a large surface area on the machined surface due to bubble traces in glass; and forming a metal film through simple electroless plating, to improve heat radiation property of the metal-film-formed portion.
- 10. The glass substrate machining method according to claim 9, wherein a CO2 laser is used to perform the laser machining.
- 11. In a method of machining a glass substrate by application of laser irradiation to said glass substrate from a laser, the improvement wherein:
said glass substrate is a glass substrate having therein discrete air bubbles; and said laser is a CO2 laser or an excimer laser.
- 12. A machined glass product made by the process of claim 11.
- 13. The method of claim 11, wherein said glass substrate is provided on a surface thereof with a thin layer selected from the group consisting of a thin insulator layer and a thin metal layer.
- 14. The method of claim 13, wherein said thin layer is an insulator layer and has a thickness of about 10-70 μm.
- 15. The method of claim 14, wherein said thin insulator layer is an organic film formed by lamination or an inorganic substance applied by spin coating.
- 16. The method of claim 13, wherein said thin layer is a metal film having a thickness of approximately 10 μm or less.
- 17. The method of claim 11, wherein said laser irradiation is carried out in a plurality of stages.
- 18. The method of claim 17, wherein a first stage of laser irradiation is carried out at a first pulse width, and a second stage of said laser irradiation is carried out with a pulse width greater than said first pulse width.
- 19. The method of claim 18, wherein said second stage of laser irradiation is performed a plurality of times.
- 20. The method of claim 18, wherein said plural stages of laser irradiation are carried out with the diameter of the laser beam remaining substantially unchanged.
- 21. The method of claim 20, wherein the pulse width of laser irradiation between said first stage and said second stage is changed.
- 22. The method of claim 18, wherein the pulse width of laser irradiation between said first stage and said second stage is changed.
- 23. The method of claim 18, wherein said laser irradiation is applied to form a through-hole in said substrate, and the focus of the laser in the depth direction of the through hole is changed from the first stage to the second stage.
- 24. The method of claim 11, wherein the bubble diameter of the discrete air bubbles is greater than or equal to 50 μm.
Priority Claims (1)
Number |
Date |
Country |
Kind |
2000-176183 |
Jun 2000 |
JP |
|
RELATED APPLICATIONS
[0001] This application is a continuing application of co-pending application Ser. No. 09/878,265, filed Jun. 12, 2001.
Continuations (1)
|
Number |
Date |
Country |
Parent |
09878265 |
Jun 2001 |
US |
Child |
10837637 |
May 2004 |
US |