Claims
- 1. A method for locally sealing a vacuum microcavity, the method comprising:
providing a device having an access passageway communicating the vacuum microcavity with ambient; and plugging the access passageway with material to locally seal the vacuum microcavity.
- 2. The method of claim 1 further comprising evacuating gas from the microcavity wherein the sealed microcavity has an initial base pressure therein.
- 3. A system for locally sealing a vacuum microcavity formed in a device having an access passageway communicating the vacuum microcavity with ambient, the system comprising:
a mechanism for plugging the access passageway with material to locally seal the vacuum microcavity.
- 4. The system of claim 3 wherein the mechanism includes a sealing heater located at the access passageway for causing the material to plug the access passageway.
- 5. A method for monitoring pressure in a vacuum microcavity, the method comprising:
measuring pressure in the microcavity and providing a signal when the pressure exceeds a maximum desired level.
- 6. The method as claimed in claim 5 wherein the vacuum microcavity is a sealed microcavity wherein the step of measuring is performed in the sealed microcavity.
- 7. The method as claimed in claim 6 wherein the sealed microcavity has an initial base pressure therein less than the maximum desired level.
- 8. The method as claimed in claim 6 wherein a plugged access passageway is located between the microcavity and ambient.
- 9. The method as claimed in claim 5 wherein the step of measuring pressure is performed indirectly.
- 10. The method as claimed in claim 5 wherein the step of measuring pressure is performed directly.
- 11. The method as claimed in claim 5 wherein a pressure-sensitive measuring device is located within the microcavity to perform the step of measuring.
- 12. The method as claimed in claim 5 wherein at least one microstructure with a quality factor is located within the microcavity and wherein the step of measuring includes the steps of vibrating the at least one microstructure and monitoring the quality factor of the at least one vibrating microstructure.
- 13. The method as claimed in claim 5 wherein the maximum desired level of pressure within the microcavity is 50 mTorr or less.
- 14. The method as claimed in claim 5 wherein the microcavity is enclosed by a pair of substrates.
- 15. The method as claimed in claim 5 wherein at least one MEMS device is located within the microcavity.
- 16. The method as claimed in claim 12 wherein the at least one microstructure includes a pair of comb resonators.
- 17. A system for monitoring pressure in a vacuum microcavity, the system comprising:
means for measuring pressure in the microcavity; and means for providing a signal when the pressure exceeds a maximum desired level.
- 18. The system as claimed in claim 17 wherein the vacuum microcavity is a sealed microcavity and wherein the means for measuring is located in the sealed microcavity.
- 19. The system as claimed in claim 18 wherein the sealed microcavity has an initial base pressure therein less than the maximum desired level.
- 20. The system as claimed in claim 18 wherein a plugged access passageway is located between the microcavity and ambient.
- 21. The system as claimed in claim 17 wherein the means for measuring measures pressure indirectly.
- 22. The system as claimed in claim 17 wherein the means for measuring measures pressure directly.
- 23. The system as claimed in claim 17 wherein the means for measuring includes a pressure-sensitive measuring device located within the microcavity.
- 24. The system as claimed in claim 17 wherein the means for measuring includes at least one microstructure having a quality factor located within the microcavity and wherein the means for measuring further includes means for vibrating the at least one microstructure and means for monitoring the quality factor of the at least one vibrating microstructure.
- 25. The system as claimed in claim 17 wherein the maximum desired level of pressure within the microcavity is 50 mTorr or less.
- 26. The system as claimed in claim 17 wherein the microcavity is enclosed by a pair of substrates.
- 27. The system as claimed in claim 17 wherein at least one MEMS device is located within the microcavity.
- 28. The system as claimed in claim 24 wherein the at least one microstructure includes a pair of comb resonators.
- 29. A method for controlling pressure in a vacuum microcavity, the method comprising:
measuring pressure in the microcavity and providing a feedback signal when the pressure exceeds a maximum desired level; and reducing the pressure in the microcavity to a pressure at or below the maximum desired level in response to the feedback signal to compensate for vacuum degradation within the vacuum microcavity.
- 30. The method as claimed in 29 wherein the vacuum microcavity is a sealed microcavity and wherein the steps of measuring and reducing are performed in the sealed microcavity.
- 31. The method as claimed in claim 30 wherein the sealed microcavity has an initial base pressure therein less than the maximum desired level.
- 32. The method as claimed in claim 30 wherein a plugged access passageway is located between the microcavity and ambient.
- 33. The method as claimed in claim 29 wherein the step of measuring pressure is performed indirectly.
- 34. The method as claimed in claim 29 wherein the step of measuring pressure is performed directly.
- 35. The method as claimed in claim 29 wherein a pressure-sensitive measuring device is located within the microcavity to perform the step of measuring.
- 36. The method as claimed in claim 29 wherein at least one microstructure with a quality factor is located within the microcavity and wherein the step of measuring includes the steps of vibrating the at least one microstructure and monitoring the quality factor of the at least one vibrating microstructure.
- 37. The method as claimed in claim 29 wherein the step of reducing includes the step of gettering gas within the microcavity.
- 38. The method as claimed in claim 29 wherein the maximum desired level of pressure within the microcavity is 50 mTorr or less.
- 39. The method as claimed in claim 29 wherein the microcavity is enclosed by a pair of substrates.
- 40. The method as claimed in claim 29 wherein at least one MEMS device is located within the microcavity.
- 41. The method as claimed in claim 36 wherein the at least one microstructure includes a pair of comb resonators.
- 42. A system for monitoring pressure in a vacuum microcavity, the system comprising:
means for measuring pressure in the microcavity and providing a feedback signal when the pressure exceeds a maximum desired level; and means for reducing the pressure in the microcavity to a pressure at or below the maximum desired level in response to the feedback signal to compensate for vacuum degradation within the vacuum microcavity.
- 43. The system as claimed in claim 42 wherein the vacuum microcavity is a sealed microcavity and wherein the means for measuring and the means for reducing are located in the sealed microcavity.
- 44. The system as claimed in claim 43 wherein the sealed microcavity has an initial base pressure therein less than the maximum desired level.
- 45. The system as claimed in claim 43 wherein a plugged access passageway is located between the microcavity and ambient.
- 46. The system as claimed in claim 42 wherein the means for measuring pressure measures pressure indirectly.
- 47. The system as claimed in claim 42 wherein the means for measuring pressure measures pressure directly.
- 48. The system as claimed in claim 42 wherein the means for measuring includes a pressure-sensitive measuring device located within the microcavity.
- 49. The system as claimed in claim 42 wherein the means for measuring includes at least one microstructure having a quality factor located within the microcavity and wherein the means for measuring further includes means for vibrating the at least one microstructure and means for monitoring the quality factor of the at least one vibrating microstructure.
- 50. The system as claimed in claim 42 wherein the means for reducing includes means for gettering gas within the microcavity.
- 51. The system as claimed in claim 42 wherein the maximum desired level of pressure within the microcavity is 50 mTorr or less.
- 52. The system as claimed in claim 42 wherein the microcavity is enclosed by a pair of substrates.
- 53. The system as claimed in claim 42 wherein at least one MEMS device is located within the microcavity.
- 54. The system as claimed in claim 49 wherein the at least one microstructure includes a pair of comb resonators.
- 55. A method for trimming resonant frequency of a microstructure located within a vacuum microcavity, the method comprising:
locally depositing material onto the microstructure to increase mass of the microstructure whereby resonant frequency of the microstructure is decreased.
- 56. The method as claimed in claim 55 wherein the step of locally depositing includes the step of controllably heating the microstructure.
- 57. The method as claimed in claim 56 wherein the microstructure has a resistance and wherein the step of heating includes the step of causing an electrical current to flow through the microstructure to heat the microstructure.
- 58. A system for trimming resonant frequency of a microstructure located within a vacuum microcavity, the system comprising:
a power supply; and means for transferring power from the power supply to the microstructure so that the microstructure converts the transferred power to a controlled amount of heat over a period of time sufficient to getter material within the microcavity onto the microstructure whereby resonant frequency of the microstructure is decreased.
CROSS-REFERENCE TO RELATED APPLICATION
[0001] This application claims the benefit of U.S. provisional application Serial No. 60/336,292, filed Oct. 25, 2001.
STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT
[0002] This invention was made with government support under DARPA Grant No. F30602-98-2-0227. The Government has certain rights in the invention.
Provisional Applications (1)
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Number |
Date |
Country |
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60336292 |
Oct 2001 |
US |