Claims
- 1. A method for forming a silicon oxide film on a substrate comprising the steps of:
(a) heating said substrate to a deposition temperature of between about 25° C. to 250° C.; (b) providing tetramethylsilane (TMS) in a gas flow amount up to about 1,000 sccm in a plasma discharge; (c) developing pressure between about 0.001 Torr and 100 Torr; and (d) depositing SiO2 on said substrate.
- 2. The method as recited in claim 1, wherein said substrate comprises at least one of: a semiconductor, a dielectric, a conductor, a glass, a polymer, a plastic, a metal foil or combinations thereof.
- 3. The method as recited in claim 1, wherein said deposition temperature is from about 100° C. to 200° C. and said pressure of step (c) is between about 2 Torr to about 8 Torr.
- 4. The method as recited in claim 1, wherein said TMS is provided in a gas flow amount up to about 100 sccm in a plasma discharge.
- 5. The method as recited in claim 1, wherein said plasma discharge comprises oxygen atoms, radicals and ions.
- 6. The method as recited in claim 5, wherein said TMS to oxygen flow rate ratio is between about 1:10 to about 1:2000.
- 7. The method as recited in claim 1, further comprising the step of providing RF power of between about 1 W to 1000 W.
- 8. The method as recited in claim 1, further comprising a post-deposition annealing step which comprises applying a forming gas and heating said silicon oxide film to an annealing temperature at or below said deposition temperature of step (a).
- 9. The method as recited in claim 8, wherein said forming gas comprises hydrogen and a gas selected from the group consisting of: argon, nitrogen, helium and mixtures thereof.
- 10. The method as recited in claim 8, wherein the leakage current through said silicon oxide film is reduced while said annealing temperature of said silicon oxide film is maintained at or below said deposition temperature of step (a).
- 11. The method as recited in claim 8, wherein the interface trap state density of said silicon oxide film is reduced while said annealing temperature of said silicon oxide film is maintained at or below said deposition temperature of step (a).
- 12. The method as recited in claim 8, wherein the oxide charge density in said silicon oxide film is reduced while said annealing temperature of said silicon oxide film is maintained at or below said deposition temperature of step (a).
- 13. The method as recited in claim 8, wherein the amount of trapped charges in said oxide film as demonstrated by bi-directional dynamic capacitance-voltage (C-V) sweep is reduced while said annealing temperature of said silicon oxide film is maintained at or below said deposition temperature of step (a).
- 14. A method for controlling the stress level of a silicon oxide film which is formed on a substrate comprising the steps of:
(a) heating said substrate to a deposition temperature of between about 25° C. to 250° C.; (b) providing TMS in a gas flow amount up to about 1,000 sccm in a plasma discharge; (c) developing a pressure between about 0.001 Torr and 100 Torr; and (d) depositing SiO2 on said substrate,
whereby said silicon oxide film exhibits a stress level between about −1.0 GPa to 0.5 GPa.
- 15. The method as recited in claim 14, wherein said silicon oxide film exhibits a stress level between about −0.5 GPa to 0.12 GPa.
- 16. The method as recited in claim 14, wherein the stress of said silicon oxide film is adjusted by varying at least one condition selected from the group consisting of: TMS flow rate, TMS:O2 flow rate ratio, RF power, temperature, deposition pressure, substrate material and film thickness.
- 17. The method as recited in claim 16, wherein said silicon oxide film exhibits zero stress or 0 GPa.
- 18. The method as recited in claim 14, further comprises at least one step from the group consisting of: decreasing the deposition temperature of step (a) and increasing the pressure of step (c), whereby said silicon oxide film exhibits tensile stress between about 0 GPa to about 0.5 GPa.
- 19. The method as recited in claim 14, further comprises at least one step from the group consisting of: increasing the deposition temperature of step (a) and decreasing the pressure of step (c), whereby said silicon oxide film exhibits compressive stress between about −1.0 GPa to about 0 GPa.
- 20. A method for controlling the conformality of a silicon oxide film formed on a substrate comprising the steps of:
(a) heating said substrate to a deposition temperature of between about 25° C. to 250° C.; (b) providing TMS in a gas flow amount up to about 1,000 sccm in a plasma discharge; (c) developing pressure between about 0.001 Torr and 100 Torr; and (d) depositing SiO2 on said substrate.
- 21. The method as recited in claim 20, wherein the conformality of said silicon oxide film is adjusted by varying at least one condition selected from the group consisting of: TMS flow rate, TMS:O2 flow rate ratio, RF power, temperature, substrate material and film thickness.
- 22. The method as recited in claim 21, wherein said silicon oxide film exhibits bumps, voids or combinations thereof.
- 23. The method as recited in claim 20, further comprises at least one step from the group consisting of: decreasing the deposition temperature of step (a) to less than about 200° C. and increasing the pressure of step (c) to above about 3 Torr, whereby said silicon oxide film exhibits conformal deposition topology on said substrate.
- 24. The method as recited in claim 23, wherein said deposition temperature is between about 25° C. to 200° C. and said pressure is between about 5 Torr and 100 Torr.
- 25. The method as recited in claim 20, further comprises at least one step from the group consisting of: increasing the deposition temperature of step (a) to at least 50° C. and decreasing the pressure of step (c) to below about 10 Torr, wherein said silicon oxide film exhibits non-conformal deposition topology having a void or a seam disposed between said film and said substrate or within said film.
- 26. The method as recited in claim 25, wherein said deposition temperature is between about 50° C. to about 250° C. and said pressure is below about 8 Torr.
Parent Case Info
[0001] This application claims benefit from U.S. Ser. No. 09/110,923 filed Jul. 6, 1998 and Provisional Application No. 60/051,823 filed Jul. 7, 1997, the contents of all are hereby incorporated by reference into this application.
Government Interests
[0002] U.S. Ser. No. 09/110,923, filed Jul. 6, 1998 was made with United States Government support under a grant by DARPA under contract #F33615-94-1-1464. Accordingly, the U.S. Government has certain rights in the invention.
Provisional Applications (1)
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Number |
Date |
Country |
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60051823 |
Jul 1997 |
US |