Techniques for manufacturing birefringent optical fiber

1. A method for fabricating a birefringent optical fiber, comprising:

(a) fabricating a preform rod having a longitudinal axis, an outer peripheral surface, and a selected refractive index variation;

(b) cutting at least one longitudinal groove into the preform rod through its outer peripheral surface;

(c) loading a respective birefringence-inducing stress element into the at least one longitudinal groove, wherein the respective stress element has a cross sectional area that is substantially equal to that of the at least one longitudinal groove, and wherein the respective birefringence-inducing stress element and the at least one longitudinal groove are shaped, such that when the respective birefringence-inducing stress element is loaded into the at least one longitudinal groove, a portion of the stress element protrudes outside of the outer peripheral surface of the preform rod;

(d) creating a preform assembly by positioning the loaded preform rod within an overcladding tube; and

(e) drawing the preform assembly into optical fiber,

wherein step (e) includes collapsing the overcladding tube around the preform rod and the at least one stress element loaded therein, such that an inner surface of the overcladding tube presses against the protruding portion of the at least one stress element so as to cause the stress element to be deformed and molded into the at least one longitudinal groove.

2. The method of claim 1 , wherein step (d) comprises:

closing one end of the overcladding tube; and

sliding the core assembly into the overcladding tube.

3. The method of claim 1 , wherein step (e) includes drawing the preform assembly using an overclad during draw technique.

4. The method of claim 1 , wherein step (b) includes using a surface grinder to cut the at least one longitudinal groove into the preform rod.

5. The method of claim 4 , wherein step (b) includes positioning the preform rod with respect to the grinder such that any bow of the preform rod lies in a plane that is parallel to that of the grinding surface.

6. The method of claim 1 , wherein the preform rod includes a plurality of concentric regions, including a core region and a cladding region surrounding the core.

7. The method of claim 6 , wherein the stress element is positioned within the cladding region parallel to the core region.

8. The method of claim 7 , wherein the plurality of stress elements comprises a first stress rod and a second stress rod that are symmetrically disposed on respective first and second sides of the core region.

9. The method of claim 1 , wherein the preform rod is fabricated using a modified chemical vapor deposition technique.

10. An optical fiber preform assembly for fabricating a birefringent optical fiber, comprising:

a preform rod with a selected refractive index variation, wherein the preform rod includes at least one longitudinal groove cut into its outer peripheral surface, wherein the at least one longitudinal groove is shaped to closely receive a respective stress element;

a respective birefringence-inducing stress element seated in the at least one longitudinal groove, wherein the stress element has a respective cross sectional area that is substantially equal to that of the at least ore longitudinal groove, and wherein the respective birefringence-inducing stress element and the at least one longitudinal groove are shaped, such that the stress element protrudes outside of the outer peripheral surface of the preform rod; and

an overcladding tube surrounding the preform rod and stress element, wherein the overcladding tube, the at least one longitudinal groove, and the overcladding tube are configured to result in a collapse, during draw, of the overcladding tube around the preform rod and the at least one stress element loaded therein, such that inner surface of the overcladding tube presses against the protruding portion of the at least one stress element so as to cause the stress element to be deformed and molded into the at least one longitudinal groove.

11. The optical fiber preform assembly of claim 10 , wherein the overcladding tube includes an open end and a closed end.

12. The optical fiber preform assembly of claim 10 , wherein the preform rod includes a plurality of concentric regions, including a core region and a cladding region surrounding the core.

13. The optical fiber preform assembly of claim 12 , wherein the stress element is positioned within the cladding region parallel to the core region.

14. The optical fiber preform assembly of claim 13 , wherein the plurality of stress elements comprises a first stress rod and a second stress rod that are symmetrically disposed on respective first and second sides of the core region.

15. The optical fiber preform assembly of claim 10 , wherein the preform rod is fabricated using a modified chemical vapor deposition technique.