Claims
- 1. A method of reducing a hydrogen content of an optical fiber or preform, which comprises applying a deuterium plasma to the optical fiber or preform for exchanging at least a portion of the hydrogen contained within the optical fiber or preform with deuterium.
- 2. The method as defined in claim 1 further comprising the steps of placing the optical fiber or preform in a cavity; providing a deuterium gas to the cavity; and generating a deuterium plasma from the deuterium gas prior to the step of applying the deuterium plasma.
- 3. The method as defined in claim 2 further comprising the step of heating the optical fiber or preform in the deuterium plasma.
- 4. The method as defined in claim 3 wherein the optical fiber is heated to a temperature of up to 200° C.
- 5. The method as defined in claim 3 wherein the preform is heated to a temperature of up to an annealing point of a core material of the preform.
- 6. The method as defined in claim 2 further comprising the step of reducing an amount of oxygen in the cavity prior to providing the deuterium gas.
- 7. The method as defined in claim 6 wherein the step of reducing the amount of oxygen comprises the steps of evacuating the cavity, providing an inert gas to the cavity, and removing said inert gas from the cavity.
- 8. The method as defined in claim 7 wherein the inert gas is selected from the group consisting of helium, neon, and argon.
- 9. The method as defined in claim 1 wherein the preform is a tube having a bore therethrough, and wherein said deuterium plasma is being applied to the bore.
- 10. An optical fiber or preform having a reduced hydrogen content made by the method as defined in claim 1.
- 11. A method of making an optical fiber or preform for reducing hydrogen induced losses of said optical fiber or preform comprising at following steps:
a) placing the optical fiber or preform in a cavity; b) providing a deuterium gas to the cavity; c) forming a deuterium plasma from the deuterium gas; and d) allowing the optical fiber or preform to remain in the deuterium plasma for exchanging at least a portion of hydroxyls with deuteroxyls.
- 12. The method as defined in claim 11 further comprising the step of heating the optical fiber or preform while said optical fiber or preform remains in the deuterium plasma.
- 13. The method as defined in claim 12 wherein the optical fiber is heated to a temperature of up to 200° C.
- 14. The method as defined in claim 12 wherein the preform is heated to a temperature of up to an annealing point of a core glass material of the preform.
- 15. The method as defined in claim 11 further comprising the step of reducing an amount of oxygen in the cavity prior to performing step b) for reducing a number of defect sites in a core glass material of the optical fiber or preform.
- 16. The method as defined in claim 15 wherein the step of reducing the amount of oxygen in the cavity includes the steps of:
evacuating the cavity; providing an inert gas to the cavity; and evacuating said inert gas from the cavity.
- 17. A method for at least partially protecting an optical fiber from an attenuation increase due to hydrogen, said optical fiber being made from a preform tube having a bore therethrough, the method comprising the step of applying a deuterium plasma to the bore of the preform tube.
- 18. The method as defined in claim 17 wherein a core glass material is deposited on an inner wall of the bore.
- 19. The method as defined in claim 18 further comprising the step of heating the preform tube while applying the deuterium plasma.
- 20. The method as defined in claim 18 further comprising the steps of providing a deuterium gas to the bore; and generating a deuterium plasma from the deuterium gas in the bore prior to the step of applying the deuterium plasma.
CROSS-REFERENCE TO RELATED APPLICATIONS
[0001] This applications claims priority of U.S. Provisional Patent Application No. 60/345,135 file don Oct. 19, 2001, entitled “Deuterium Plasma and High Temperature Methods for Passivating Er Doped Fiber or Preform” which is incorporated herein by reference for all purposes.
Provisional Applications (1)
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Number |
Date |
Country |
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60345135 |
Oct 2001 |
US |