Optical fiber launch coupler

• US 4,307,933 A
• Filed: 02/20/1980
• Issued: 12/29/1981
• Est. Priority Date: 02/20/1980
• Status: Expired due to Term

• Current Assignee: Hughes Missile Systems Company
• Original Assignee: General Dynamics
• Inventors: Palmer, John P., Ward, Phillip B. Jr.
• Primary Examiner(s): Lee, John D.
• Application Number:
  US06/123,034
• Time in Patent Office: 678 Days
• Field of Search: 350/96.15, 350/96.16, 350/96.30, 350/320, 65/4 B, 65/61, 51/283 R, 156/153, 156/154
• US Class Current: 385/42
• CPC Class Codes: G02B 6/2826 using mechanical machining means for shaping of the couplers, e.g. grinding or polishing grinding, polishing in general B24
• CPC Class Codes: G02B 6/283 couplers being tunable or adjustable
• CPC Class Codes: Y10S 359/90 Methods

Abstract

A low-loss unidirectional optical coupler utilizing clad monofilament fibers of different diameters is provided by mounting each fiber on a curved surface, lapping the smaller (launch) fiber substantially tangentially to the curved surface until the core of the launch fiber has been lapped through to produce two elliptical flat surfaces, independently lapping the other (throughput) fiber tangentially to its surface to produce a fiber surface of substantially the same size as one of those produced on the launch fiber, aligning the throughput fiber surface with one of the launch fiber surfaces, and bonding them together.

Claims

1. A fiber optic coupler comprising a curved throughput fiber having a longitudinal planar surface and a curved launch fiber having two longitudinal planar surfaces exposing the severed core of the launch fiber, the ratio of the diameter of the throughput fiber to the diameter of the launch fiber being from 3:

2 to 4;

1 and said throughput fiber being joined to only one of the launch fiber planar surfaces.

2. The coupler of claim 1 wherein the ratio is from 1.6:

1 to 2.4;

1.

3. The coupler of claim 1 wherein the throughput fiber core diameter is from 100 to 400 microns, and the launch fiber core diameter is up to 100 microns.

4. The coupler of claim 3 wherein said throughput core diameter is from 125 to 250 microns and said launch core diameter is from 5 to 70 microns.

5. The coupler of claim 1 wherein each of said fibers adheres to an arcuate surface, and the fibers are adhered together by a coating surrounding the junction thereof.

6. The coupler of claim 1 wherein said fibers are monofilament glass-clad glass fibers.

7. The coupler of claim 6 wherein the width of the planar surface on the throughput fiber is substantially the diameter of the launch fiber.

8. The coupler of claim 1 wherein the launch fiber is a glass-clad glass fiber, the longitudinal planar surfaces are elliptical and the core is severed.

9. The coupler of claim 8 wherein the glass cladding of the launch fiber remains at least partly intact.

10. The coupler of claim 1 wherein the planar surface of the launch fiber contains two elliptical surfaces, the planar surface of the throughput fiber is elliptical, the elliptical surfaces are substantially of the same area and one of the launch fiber surfaces is overlapped with the throughput fiber surface.

11. The method of manufacturing fiber optic couplers comprising:

bonding a first glass fiber to a first arcuate surface;

bonding a second glass fiber to a second arcuate surface, the second fiber being substantially smaller in diameter than the first fiber;

lapping each of said bonded fibers, individually, along said arcuate surfaces to expose a planar, substantially elliptical surface on said first fiber and a pair of planar, substantially elliptical surfaces on said second fiber, the lapping of the first fiber removing less than half the thickness of the fiber core;

positioning one of said elliptical surfaces on said second fiber adjacent said elliptical surface on the first fiber, the surface areas of the adjacent elliptical surfaces being substantially equal; and

coating the fibers with an adhesive to adhere and join the surfaces together.

12. The method of claim 11 further comprising bonding the fibers to the arcuate surface by utilizing a curable epoxy resin mixed with glass beads.

13. The method of claim 12 wherein the planar surfaces are provided by lapping the resin and fiber with an alumina slurry to produce the planar surfaces.

14. The method of claim 12 wherein the glass beads are of a diameter equal to or less than the core diameter of the optical fiber to be lapped.

15. The improvement of claim 14 wherein said glass beads are up to 5 microns in diameter.

16. The method of claim 11 further comprising utilizing monofilament optical fibers wherein the ratio of the diameter of the first fiber to the diameter of second fiber is from 3:

2 to 4;

1 and the width of the planar surface on the first fiber substantially equals the diameter of the second fiber.

17. The method of claim 16, further comprising selecting glass-clad monofilament glass fibers for the first and second fibers.

18. The method of claim 17 further comprising banding the monofilament fibers by utilizing a curable epoxy resin containing glass beads, and lapping the resin and the fibers to produce the surfaces.

19. The method of claim 18 further comprising lapping the second fiber in amount sufficient to sever the core thereof.

20. The method of claim 19 further comprising terminating the lapping procedures on the second fiber before complete severance of the glass cladding.

21. The method of claim 11 wherein said fibers are bonded together through the use of an optically transparent epoxy resin.

22. A method of manufacturing a fiber optic launch coupler comprising:

positioning and bonding a throughput monofilament clad glass fiber on a first arcuate surface;

positioning and bonding a launch monofilament fiber optic clad glass fiber on a second arcuate surface, the launch fiber being substantially smaller in diameter than the throughput fiber;

lapping the throughput fiber through said bonding material and the cladding of said fiber and exposing a portion of the core thereof with less than half the thickness of the fiber being removed;

lapping the launch fiber through said bonding material, through the cladding thereof, and through the core thereof on said arcuate surface and producing a flat surface chordal to the arc of the fiber comprising two elliptical sections of the core of said launch fiber, the surface area of one of the elliptical sections of said launch fiber core being substantially equal to the surface area of the core exposed in the throughput fiber;

positioning one of the launch surfaces and the throughput core surface in a mating relationship; and

bonding said surfaces in said mating relationship.

23. The method of claim 22 wherein the ratio of the core diameter of the throughput fiber to the core diameter of the launch fiber is from 1.6:

1 to 2.4;

1.

24. The method of claim 22 wherein the throughput fiber core diameter is from 100 to 400 microns, and the launch fiber core diameter is up to 100 microns.

25. The method of claim 24 wherein said throughput core diameter is from 125 to 250 microns and said launch core diameter is from 5 to 70 microns.

26. A fiber optic coupler comprising:

a throughput fiber having a lapped planar surface; and

a launch fiber having a pair of planar surfaces formed by lapping entirely through the core of the launch fiber, the ratio of the diameter of the throughput fiber to the diameter of the launch fiber being from 3;

2 to 4;

1, said fibers being curved and in contact along the planar surface of the throughput fiber and only one of the planar surfaces of the launch fiber, said contacting surfaces being aligned along the curvature of the fibers, wherein the width of the planar surface on the throughput fiber is equal to the core diameter of the launch fiber.