Method of fabrication of fiber optic coupler

• US 4,431,260 A
• Filed: 01/23/1981
• Issued: 02/14/1984
• Est. Priority Date: 02/26/1979
• Status: Expired due to Term

• Current Assignee: Hughes Missile Systems Company
• Original Assignee: General Dynamics
• Inventors: Palmer, John P.
• Primary Examiner(s): Lee, John D.
• Assistant Examiner(s): FONT, FRANK G
• Application Number:
  US06/227,712
• Time in Patent Office: 1,117 Days
• Field of Search: 350/96.15, 350/96.16
• US Class Current: 385/51
• 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: Y10S 359/90 Methods

Abstract

A low-loss bidirectional optical coupler is provided by mounting together and joining with epoxy resin two like fiber optic elements in face-to-face relationship along a common plane. Each of the elements is fabricated by affixing a portion of an optical fiber with epoxy resin along the curved surface of a solid support form. After the epoxy securing the fiber to the form is cured and hardened, a planar surface extending partially into and along the fiber is established by lapping and polishing the element to a carefully controlled depth. The techniques employed and the resulting devices permit coupling between pairs of individual fibers joined in the manner described.

Claims

1. The method of fabricating an optical fiber coupler comprising:

machining a solid form to develop a curved side having a preselected radius of curvature of between 5 and 8 cm;

applying a coating of liquid epoxy resin on the curved side of the form;

embedding a portion of an optical fiber in the liquid epoxy resin and allowing the resin to harden, thereby affixing the fiber to the form along the curved side thereof.

repeating the first, second and third steps with a second solid form and a second optical fiber;

mounting the two sections thus formed in a lapping and polishing fixture;

lapping the epoxy and portions of the fibers embedded therein to develop essentially planar surfaces along the epoxy resin and fibers extending to a predetermined depth into the core of each fiber such that each fiber protrudes slightly above the planar surface of the adjacent epoxy;

polishing the lapped surfaces;

joining the two lapped and polished sections together at their planar surfaces along a common plane with optically transmitting epoxy;

preliminarily aligning the fibers by initially moving the two sections parallel to each other along their planar surfaces to detect the protruding fibers contacting each other;

finally aligning the two sections and the preliminarily aligned fibers thereof by focusing laser light into one of the fiber ends and monitoring the intensity of the light coupled into the other fiber while gradually adjusting the relative positions of the fibers; and

curing the epoxy joining the two planar surfaces together while maintaining the established alignment thereof.

2. The method of claim 1 further comprising the step of mounting the thus-fabricated assembly in a housing and coupling optical connectors to each of the fiber ends, respectively.

3. The method of claim 1 wherein each form is machined to a radius of curvature of 6 cm.

4. The method of claim 1 wherein each form is machined from an aluminum block.

5. The method of claim 1 wherein the lapping step is performed without removing any of the surface of the previously machined form.

6. The method of claim 5 further including the step of terminatng the lapping prior to contacting the surface of the form.