Claims
- 1. A shield assembly for a chemical vapor deposition system, the shield assembly comprising:
(a) a plurality of shield bodies, each shield body having a screen and a conduit with an array of holes therein to deliver shield gas through the screen; and (b) a plurality of flowpaths, at least one flowpath coupled to each conduit to supply shield gas thereto; and (c) a flow limiter in each of the plurality of flowpaths, the flow limiter having an orifice with a cross-sectional area (Aorifice) sized so that substantially equal flows of shield gas are provided from each of the plurality of shield bodies.
- 2. A shield assembly according to claim 1 wherein the holes in each conduit comprise a total cross-sectional area (Aholes) and the flowpath associated with the conduit comprises a cross-sectional area (Aflowpath) and wherein Aorifice<Aholes<Aflowpath.
- 3. A shield assembly according to claim 1 wherein a sum of the cross-sectional areas of the orifices in the flow limiters in all of the flowpaths (Total Aorifice) is less than a sum of the cross-sectional areas of the holes in all of the conduits (Total Aholes), and wherein Total Aholes is less than a sum of the cross-sectional areas of all of the flowpaths (Total Aflowpaths), Total Aorifice<Total Aholes<Total Aflowpath.
- 4. A shield assembly according to claim 1 wherein the plurality of flowpaths supply shield gas to the conduits from a single shield gas supply, and wherein the orifices are sized to provide a substantially constant flow of shield gas from each of the plurality of shield bodies even with variations in pressure or flow of shield gas from the shield gas supply.
- 5. A gas distribution system for distributing gas in a chamber to process a substrate, the gas distribution system comprising:
(a) a process gas injector capable of introducing process gas into the chamber; (b) a shield assembly having a plurality of shield bodies adjacent to the process gas injector to reduce deposition of process byproducts thereon, each shield body having a screen and a conduit with an array of holes therein to deliver shield gas through the screen; (c) a plurality of flowpaths, at least one flowpath coupled to each conduit to supply shield gas thereto; and (d) a flow limiter in each of the plurality of flowpaths, the flow limiter having an orifice with a cross-sectional area (Aorifice).
- 6. A system according to claim 5 wherein the Aorifice is sized to provide substantially equal back pressure at each of the conduits.
- 7. A system according to claim 6 wherein the holes in each conduit comprise a total cross-sectional areas (Aholes) that is substantially equal to that of other conduits so that substantially equal flows of shield gas are provided from each of the plurality of shield bodies.
- 8. A system according to claim 5 wherein the holes in each conduit comprise a total cross-sectional area (Aholes) and the flowpath associated with the conduit comprises a cross-sectional area (Aflowpath) and wherein Aorifice<Aholes<Aflowpath.
- 9. A system according to claim 5 wherein a sum of the cross-sectional areas of the orifices in the flow limiters in all of the flowpaths (Total Aorifice) is less than a sum of the cross-sectional areas of the holes in all of the conduits (Total Aholes), and wherein Total Aholes is less than a sum of the cross-sectional areas of all of the flowpaths (Total Aflowpaths), Total Aorifice<Total Aholes<Total Aflowpath.
- 10. A system according to claim 9 wherein Total Aorifice/Total Aholes≧1.5 and wherein Total Aflowpath/Total Aholes≧1.
- 11. A system according to claim 5 wherein each of the flowpaths comprise a delivery line to supply shield gas to an inlet of the conduit, and wherein the flow limiter is in the delivery line.
- 12. A system according to claim 11 wherein the flow limiter in each of the plurality of flowpaths is located a substantially equal distance along the delivery line from the inlet of the conduit.
- 13. A system according to claim 11 wherein the flow limiter is in the inlet of the conduit.
- 14. A system according to claim 5 wherein the plurality of flowpaths supply shield gas to the conduits from a single shield gas supply, and wherein the orifices are sized to provide a substantially constant flow of shield gas from each of the plurality of shield bodies even with variations in pressure or flow of shield gas from the shield gas supply.
- 15. A chemical vapor deposition system comprising the gas distribution system of claim 5, the chemical vapor deposition system further comprising:
(a) a heater to heat the chamber in which the substrate is processed; and (b) an exhaust system having a plurality of exhaust ports in the chamber to exhaust gases and byproducts from the chamber.
- 16. A system according to claim 15 wherein the shield assembly further comprises a plurality of vent shield bodies adjacent to the exhaust ports to reduce deposition of process byproducts thereon.
- 17. A method of operating a chemical vapor deposition system to process a substrate, the method comprising steps of:
(a) providing a shield assembly comprising a plurality of shield bodies adjacent to a process gas injector to reduce deposition of process byproducts thereon, each shield body having a screen and a conduit with an array of holes therein capable of delivering shield gas through the screen to reduce deposition of process byproducts thereon; (b) supplying shield gas to the conduits through a plurality of flowpaths; (c) limiting flow of shield gas through the plurality of flowpaths by providing in each flowpath a flow limiter having an orifice therein, the orifice having a cross-sectional area (Aorifice) sized so that substantially equal flows of shield gas are provided from each of the plurality of shield bodies; (d) placing the substrate in a chamber; and (e) introducing process gas into the chamber through the process gas injector to process the substrate.
- 18. A method according to claim 17 wherein the holes in each conduit comprise a total cross-sectional area (Aholes), and wherein step (b) comprises the step of supplying shield gas through flowpaths having a cross-sectional area (Aflowpath) sized so that Aholes<Aflowpath.
- 19. A method according to claim 18 wherein step (c) comprises the step of providing flow limiters having an orifice sized so that Aorifice<Aholes<Aflowpath.
- 20. A method according to claim 17 wherein all of the holes in all of the conduits comprise a total cross-sectional area (Total Aholes), and wherein step (b) comprises the step of supplying shield gas through flowpaths having a total cross-sectional area (Total Aflowpaths) greater than the total cross-sectional area of the holes, and wherein step (c) comprises the step of providing flow limiters having orifices sized so that a sum of the cross-sectional areas of all the orifices (Total Aorifice) is less than the total cross-sectional area of the holes, Total Aorifice<Total Aholes<Total Aflowpath.
- 21. A method according to claim 20 wherein step (b) comprises the step of supplying shield gas through flowpaths having a total cross-sectional area such that Total Aflowpath/Total Aholes≧1, and wherein step (c) comprises the step of providing flow limiters having orifices sized so that Total Aorifice/Total Aholes≧1.5.
- 22. A method according to claim 17 wherein each of the flowpaths comprise a delivery line to supply shield gas to an inlet of the conduit, and wherein step (c) comprises the step of providing flow limiters in the delivery lines.
- 23. A method according to claim 22 wherein step (c) comprises the step of locating the flow limiter in each of the plurality of flowpaths at a substantially equal distance along the delivery line from the inlet of the conduit.
- 24. A method according to claim 22 wherein step (c) comprises the step of locating the flow limiter in the inlet of each of the conduits.
- 25. A method according to claim 17 wherein the plurality of flowpaths supply shield gas to the conduits from a single shield gas supply, and wherein step (c) comprises the step of providing flow limiters having orifices sized to provide a substantially constant flow of shield gas from each of the plurality of shield bodies even with variations in pressure or flow of shield gas from the shield gas supply.
- 26. A chemical vapor deposition system for processing a substrate, the system comprising:
(a) a chamber in which the substrate is processed; (b) a process gas injector capable of introducing process gas into the chamber to process the substrate; (c) a shield assembly having a plurality of shield bodies adjacent to the process gas injector to reduce deposition of process byproducts thereon, each shield body having a screen and a conduit with an array of holes therein to deliver shield gas through the screen; (d) a plurality of flowpaths, at least one flowpath coupled to each conduit to supply shield gas thereto; and (e) means for providing a substantially equal flow of shield gas from each of the plurality of shield bodies; and (f) an exhaust system having at least one exhaust port in the chamber to exhaust gases and byproducts therefrom.
- 27. A system according to claim 26 wherein the means for providing a substantially equal flow of shield gas from each of the conduits comprises a flow limiter in each of the plurality of flowpaths, the flow limiter having an orifice with a cross-sectional area (Aorifice) sized so that substantially equal flows of shield gas are provided from each of the plurality of shield bodies.
- 28. A system according to claim 27 wherein the holes in each conduit comprise a total cross-sectional area (Aholes) and the flowpath associated with the conduit comprises a cross-sectional area (Aflowpath) and wherein Aorifice<Aholes<Aflowpath.
- 29. A system according to claim 27 wherein a sum of the cross-sectional areas of the orifices in the flow limiters in all of the flowpaths (Total Aorifice) is less than a sum of the cross-sectional areas of the holes in all of the conduits (Total Aholes), and wherein Total Aholes is less than a sum of the cross-sectional areas of all of the flowpaths (Total Aflowpaths).
CROSS REFERENCE TO RELATED APPLICATIONS
[0001] This application claims priority from U.S. Provisional Patent Application Ser. No. 60/134,443 filed May 17, 1999, which is incorporated herein by reference.
Provisional Applications (1)
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Number |
Date |
Country |
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60134443 |
May 1999 |
US |