US20030202769A1 - High density fiber terminator/connector - Google Patents

High density fiber terminator/connector Download PDF

Info

Publication number
US20030202769A1
US20030202769A1 US10/448,561 US44856103A US2003202769A1 US 20030202769 A1 US20030202769 A1 US 20030202769A1 US 44856103 A US44856103 A US 44856103A US 2003202769 A1 US2003202769 A1 US 2003202769A1
Authority
US
United States
Prior art keywords
fiber
hole
substrate
optical fiber
fibers
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Abandoned
Application number
US10/448,561
Inventor
Roman Gutierrez
Tony Tang
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
DigitalOptics Corp MEMS
Original Assignee
Siwave Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Siwave Inc filed Critical Siwave Inc
Priority to US10/448,561 priority Critical patent/US20030202769A1/en
Publication of US20030202769A1 publication Critical patent/US20030202769A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/24Coupling light guides
    • G02B6/36Mechanical coupling means
    • G02B6/3628Mechanical coupling means for mounting fibres to supporting carriers
    • G02B6/3648Supporting carriers of a microbench type, i.e. with micromachined additional mechanical structures
    • G02B6/3652Supporting carriers of a microbench type, i.e. with micromachined additional mechanical structures the additional structures being prepositioning mounting areas, allowing only movement in one dimension, e.g. grooves, trenches or vias in the microbench surface, i.e. self aligning supporting carriers
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/24Coupling light guides
    • G02B6/26Optical coupling means
    • G02B6/32Optical coupling means having lens focusing means positioned between opposed fibre ends
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/24Coupling light guides
    • G02B6/36Mechanical coupling means
    • G02B6/3628Mechanical coupling means for mounting fibres to supporting carriers
    • G02B6/3632Mechanical coupling means for mounting fibres to supporting carriers characterised by the cross-sectional shape of the mechanical coupling means
    • G02B6/3644Mechanical coupling means for mounting fibres to supporting carriers characterised by the cross-sectional shape of the mechanical coupling means the coupling means being through-holes or wall apertures
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/24Coupling light guides
    • G02B6/36Mechanical coupling means
    • G02B6/3628Mechanical coupling means for mounting fibres to supporting carriers
    • G02B6/36642D cross sectional arrangements of the fibres
    • G02B6/36722D cross sectional arrangements of the fibres with fibres arranged in a regular matrix array
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/24Coupling light guides
    • G02B6/36Mechanical coupling means
    • G02B6/3628Mechanical coupling means for mounting fibres to supporting carriers
    • G02B6/3684Mechanical coupling means for mounting fibres to supporting carriers characterised by the manufacturing process of surface profiling of the supporting carrier
    • G02B6/3692Mechanical coupling means for mounting fibres to supporting carriers characterised by the manufacturing process of surface profiling of the supporting carrier with surface micromachining involving etching, e.g. wet or dry etching steps
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/24Coupling light guides
    • G02B6/36Mechanical coupling means
    • G02B6/38Mechanical coupling means having fibre to fibre mating means
    • G02B6/3807Dismountable connectors, i.e. comprising plugs
    • G02B6/381Dismountable connectors, i.e. comprising plugs of the ferrule type, e.g. fibre ends embedded in ferrules, connecting a pair of fibres
    • G02B6/3818Dismountable connectors, i.e. comprising plugs of the ferrule type, e.g. fibre ends embedded in ferrules, connecting a pair of fibres of a low-reflection-loss type
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/24Coupling light guides
    • G02B6/36Mechanical coupling means
    • G02B6/38Mechanical coupling means having fibre to fibre mating means
    • G02B6/3807Dismountable connectors, i.e. comprising plugs
    • G02B6/3833Details of mounting fibres in ferrules; Assembly methods; Manufacture
    • G02B6/3834Means for centering or aligning the light guide within the ferrule
    • GPHYSICS
    • G02OPTICS
    • G02BOPTICAL ELEMENTS, SYSTEMS OR APPARATUS
    • G02B6/00Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
    • G02B6/24Coupling light guides
    • G02B6/36Mechanical coupling means
    • G02B6/38Mechanical coupling means having fibre to fibre mating means
    • G02B6/3807Dismountable connectors, i.e. comprising plugs
    • G02B6/3873Connectors using guide surfaces for aligning ferrule ends, e.g. tubes, sleeves, V-grooves, rods, pins, balls
    • G02B6/3885Multicore or multichannel optical connectors, i.e. one single ferrule containing more than one fibre, e.g. ribbon type

Definitions

  • the present invention relates to fiber optic terminators/connectors, and more particularly to a high density fiber terminator/connector.
  • each fiber is terminated with an FC/PC connector as described, and the fibers are connected together one pair at a time. This process is extremely time-consuming and costly when connecting a large number of fibers together.
  • a high density fiber terminator/connector and methods of making the high density fiber terminator/connector are provided in accordance with the present invention.
  • One method uses silicon micro-machining to terminate multiple fibers simultaneously. This simplifies the process and improves the alignment of connecting multiple fibers together or positioning multiple fibers together to free-space optical elements.
  • One method uses Deep Reactive Ion Etching (DRIE) to make precise holes in a silicon wafer.
  • the holes in the silicon may be arranged in any desired pattern by using, for example, a mask fabrication process with electron-beam writing of the mask, such as photolithography masking.
  • a single photolithographic mask provides extremely high precision location positioning, and the relative position of each fiber in the holes can be accurately controlled. The accuracy in the relative positioning of the fibers ensures that all fibers are simultaneously aligned.
  • photolithographic masking and deep reactive ion etching enable the fabrication of connectors for a plurality of fibers. Photolithographic masking and deep reactive ion etching also allow multiple fibers to be accurately aligned to free-space optical components.
  • One aspect of the invention relates to a method of making an optical fiber terminator.
  • the method comprises using deep reactive ion etching to etch a plurality of holes in a silicon substrate, wherein each hole is sized to fit an optical fiber; and placing an optical fiber in at least one hole.
  • optical fiber terminator in an optical switch.
  • the optical fiber terminator comprises a silicon substrate with a plurality of holes formed by deep reactive ion etching, wherein each hole is sized to fit an optical fiber.
  • Another aspect of the invention relates to an optical fiber terminator with holes formed to allow insertion of fibers at an angle with respect to the substrate surface.
  • Another aspect of the invention relates to a method of making an optical fiber terminator.
  • the method comprises etching a plurality of holes in a silicon substrate, wherein each hole is sized to fit an optical fiber; forming a plurality of flaps in the substrate around each hole, the flaps being configured for kinematic alignment of an optical fiber in each hole; and placing an optical fiber in at least one hole.
  • an optical fiber terminator which comprises a silicon substrate.
  • the silicon substrate comprises a plurality of holes etched in the silicon substrate, wherein each hole is sized to fit an optical fiber.
  • the silicon substrate also comprises a plurality of flaps formed in the substrate around each hole. The flaps are configured for kinematic alignment of an optical fiber in each hole.
  • FIG. 1 illustrates one embodiment of an array of holes etched into a silicon wafer/substrate.
  • FIG. 2 illustrates one embodiment of a plurality of optical fibers inserted in a plurality of holes of a portion of the substrate of FIG. 1.
  • FIG. 3 illustrates one embodiment of angling a plurality of holes in a substrate to allow fibers to be positioned and pointed at a specific angle.
  • FIGS. 4 A- 4 B illustrate one embodiment of a substrate with a plurality of holes and a plurality of vertical flaps positioned at an equal distance from each other around each hole.
  • FIG. 5 illustrates the wafer of FIG. 2 with top ends of the fibers removed.
  • FIG. 6 illustrates one embodiment of a plurality of substrate components removed from a base substrate.
  • FIG. 7 illustrates one embodiment of a coating formed on one side of the substrate and fibers in FIG. 5.
  • FIG. 8 illustrates one embodiment of the substrate in FIG. 5 with a plurality of MEMS components inserted in etched recesses.
  • FIG. 9 illustrates one embodiment of the substrate in FIG. 5 with alignment notches, which are used to align the fiber array to a lens array.
  • FIG. 10 illustrates one embodiment of two aligned fiber arrays.
  • FIG. 11 illustrates another embodiment of two aligned fiber arrays.
  • FIG. 12 illustrates one embodiment of an angled fiber array.
  • FIG. 13 illustrates a top view of another embodiment of kinematic alignment features between two fiber arrays.
  • FIG. 14 illustrates one embodiment of a substrate with a plurality of etched holes and a plurality of recesses formed on one surface of the substrate.
  • FIG. 1 illustrates one embodiment of an array of holes 102 (referred to herein individually or collectively as ‘ 102 ’) etched into a silicon wafer/substrate 100 .
  • the substrate 100 may be between about 200 microns to about 650 microns in thickness. In one embodiment, the substrate 100 is 600 microns thick.
  • the holes 102 are etched with Deep Reactive Ion Etching (DRIE) processes.
  • the holes in the silicon substrate 100 may be arranged in any desired pattern by using, for example, a mask fabrication process with electron-beam writing of the mask, such as photolithography masking.
  • a mask is a layer with openings in desired locations to expose an underlying material for etching.
  • a single photolithographic mask provides extremely high precision location positioning.
  • Masks written by electron-beam lithography typically have about 10 nm to 100 nm accuracy in positioning the locations of features in the mask. Thus, the relative position of each fiber in the holes can be accurately controlled.
  • the substrate 100 may have any number of holes 102 etched in any desired pattern.
  • Each hole 102 is sufficiently sized to allow an optical fiber 200 (FIG. 2) to fit through the hole 102 (FIG. 1).
  • each hole is formed to closely match the diameter of an optical fiber, which is typically 125 microns.
  • FIG. 2 illustrates one embodiment of a plurality of optical fibers 200 A- 200 C (referred to herein individually or collectively as ‘fiber 200 ’) inserted in a plurality of holes 102 A- 102 C of a portion of the substrate 100 of FIG. 1.
  • fiber 200 a small number of fibers and holes are shown, but the methods described herein may be applied to a very large number of fibers and holes.
  • a fiber (core plus cladding) 200 is typically about 125 microns in diameter.
  • the core of a fiber 200 is typically about 9 microns in diameter, but the core is conventionally not easily separable from the cladding of the fiber 200 because both the core and the cladding are typically made out of glass.
  • the coating or buffer 204 around the fiber 200 typically comprises plastic and may be separated from the fiber 200 .
  • the diameter of the buffer 204 is typically between 250 microns and 900 microns.
  • each hole 102 in FIG. 2 provides a 5-micron space between an exterior surface (e.g., cylindrical) of a fiber 200 and the hole 102 .
  • the hole 102 is about 135 microns in diameter to provides a 5-micron space between an exterior surface (e.g., cylindrical) of a fiber 200 with a 25 micron diameter and the hole 102 .
  • a fiber 200 is 125 microns in diameter, and each hole 102 is 130 microns in diameter, there is a 2.5-micron clearance on each side for the fiber 200 to pass through the hole 102 .
  • a fiber 200 is 125 microns in diameter
  • each hole 102 is 127 microns in diameter
  • each hole 102 is substantially cylindrical in shape. In other embodiments, each hole 102 may be non-cylindrical, such as a triangle, a rectangle or a pentagon.
  • the optical fibers 200 A- 200 C in FIG. 2 are stripped (removing their buffer coating 204 A- 204 C and exposing the bare fiber 200 A- 200 C), a small amount of glue 206 A- 206 C is applied to the fiber coatings 204 A- 204 C, and the bare fibers 200 A- 200 C are slipped into the holes 102 A- 102 C in the silicon wafer 100 .
  • glue there are many types of glue that can be used, such as a thermal cure epoxy, which cures at 120 degrees Celsius from Epotek.
  • FIG. 3 illustrates one embodiment of angling a plurality of holes 304 A- 304 B in a substrate 300 to allow fibers 302 A- 302 B to be positioned and pointed at a specific angle.
  • the holes 304 A- 304 B in FIG. 3 may be formed with any suitable process, such as deep reactive ion etching.
  • Each hole 304 may also contain micro-machined kinematic alignment mechanisms to position the optical fiber at the center of the hole 304 . Micro-machined kinematic alignment mechanisms are described herein and in the U.S. Provisional Application referenced above and incorporated by reference.
  • FIG. 12 illustrates one embodiment of an angled optical fiber array/terminator 1200 .
  • deep reactive ion etching forms a plurality of holes 1204 A- 1204 C in the substrate.
  • a front surface 1208 of the substrate may have a hole 1204 sized to fit an optical fiber 1202 and a locator 1206 at the edge of the slotted hole 1204 to position a fiber 1202 precisely on that surface 1208 .
  • each hole 1204 is sized to fit an optical fiber 1202 in one direction 1210 A but oversized in another direction 1210 B.
  • each slotted hole 1204 allows a fiber 1202 to be inserted at an angle with respect to the substrate surface 1208 .
  • the angled insertion of the fiber arrays 300 , 1200 in FIGS. 3 and 12 provides low back-reflection, which is important when the fiber array 300 or 1200 is used as a termination into free-space (an unguided medium with a different optical index of refraction). Back-reflection may be further reduced by coating the fiber array 300 or 1200 with an anti-reflection coating. Terminating fibers 304 A- 304 B and 1202 A- 1202 C at an angle also allows a ball lens to collimate light, such that the collimated light comes out at an angle with respect to the substrate with low aberrations. If a graded index lens or aspheric lens is used, then it is important to tilt the lens with respect to the fiber array 300 or 1200 in order to provide collimated light with low aberrations.
  • FIGS. 4 A- 4 B illustrate one embodiment of a substrate 400 with a plurality of holes 408 A- 408 B and a plurality of vertical flaps 404 A- 404 F positioned at an equal distance from each other around each hole 408 .
  • FIG. 4B is a top view. Although three flaps 404 A- 404 C, 404 D- 404 F are shown for each hole 408 A, 408 B, there may be less than three or greater than three flaps for each hole 408 A, 408 B, in other embodiments.
  • the flaps 404 A- 404 F may be formed by deep reactive ion etching portions of the silicon wafer 400 .
  • the first set of flaps 404 A- 404 C support a first fiber 402 A equally and center the fiber 402 A within the first hole 408 A.
  • the second set of flaps 404 D- 404 F support a second fiber 402 B equally and center the fiber 402 B within the second hole 408 B.
  • the flaps provide kinematic alignment or self-centering of a fiber 402 in a hole 408 , which overcomes the problem of etching non-uniformities in the wafer 400 .
  • each hole 408 may be tapered to allow a fiber 402 to more easily slide into the hole 408 .
  • each hole 408 in FIGS. 4 A- 4 B is not tapered.
  • FIG. 5 illustrates the wafer 202 of FIG. 2 with top ends of the fibers 200 A- 200 C removed, e.g., by cleaving or etching.
  • the structure 500 in FIG. 5 may be referred to as a ‘fiber array,’ a ‘fiber connector’ or a ‘fiber terminator.’
  • a top side 502 of the entire silicon wafer 202 in FIG. 5 and the glued fibers 200 A- 200 C is polished by a lapping and polishing process.
  • the lapping and polishing process may include the use of chemical mechanical polishing (CMP) slurries, or using polishing pads with Alumina grit of various sizes that are lubricated with water.
  • CMP chemical mechanical polishing
  • One of the advantages of the structure 500 in FIG. 5 is that all fibers 200 A- 200 C may be polished simultaneously. Once the ends of the fibers 200 A- 200 C are polished, the wafer 202 in FIG. 5 may be separated into individual components, as shown in FIG. 6.
  • FIG. 6 illustrates one embodiment of a plurality of substrate components 602 A- 602 D removed from a base substrate 604 (as shown by the arrow).
  • the separation may be done by various methods, including but not limited to dicing with a diamond saw.
  • FIG. 7 illustrates one embodiment of a coating 702 formed on one side 502 of the substrate 202 and fibers 200 A- 200 C in FIG. 5.
  • an anti-reflection (AR) coating 702 is applied by depositing films of various materials on the side 502 the silicon wafer 202 where the fiber ends have been polished.
  • the AR coating 702 uses multiple layers of dielectric materials, where the materials and designs may vary. Multiple layer dielectrics form interferometric effects, which are used to eliminate reflection from the surface 502 and provide almost 100% transmission.
  • the coating 702 may comprise a chemically sensitive film for chemical sensors, or a metal coating for total reflection.
  • the coating 702 is a way to make a sensor or to improve the optical characteristics of the fiber/ambient interface 502 .
  • MEMS microelectronic mechanical system
  • FIG. 8 illustrates one embodiment of the substrate 202 in FIG. 5 with a plurality of MEMS components 804 A, 804 B inserted in etched recesses 802 A, 802 B.
  • One advantage of the structure 800 in FIG. 8 is that the optical fibers 200 A- 200 C are aligned to the MEMS components 804 A, 804 B using photolithography masking, which provides very good alignment.
  • a single photolithographic mask may be used when the MEMS recesses 802 A, 802 B and the fiber holes in FIG. 8 are etched during the same etching process, such as deep reactive ion etching.
  • a single photolithographic mask provides extremely high precision location positioning between all components. Masks written by electron-beam lithography typically have about 10 nanometer-100 nm accuracy in positioning the locations of features in the mask.
  • the structure 800 in FIG. 8 may be used in fabricating a high density, MEMS fiber optic switch.
  • FIG. 9 illustrates one embodiment of the substrate 202 in FIG. 5 with alignment notches 908 A, 908 B, which are used to align the fiber array 900 to a lens array 902 .
  • the alignment notches 908 A, 908 B and the fiber holes in FIG. 9 are etched into the silicon wafer 202 during the same etching process, such as deep reactive ion etching.
  • the alignment notches 908 A, 908 B are aligned with respect to the fiber holes in the substrate 202 with lithographic precision.
  • the lens array 902 in FIG. 9 comprises a plurality of lenses 904 A- 904 C and protruding stubs 906 A, 906 B, which are intended to fit into the notches 908 A, 908 B.
  • notches are etched into the lens array 902 and stubs are formed (e.g., by etching the surface of the substrate 202 ) in the fiber array 900 .
  • the array 902 may comprise diffraction gratings, MEMS components, or anything that a user desires to align with the fiber array 902 .
  • the fiber terminators described herein may be used for connecting fibers, such as standard single fiber connectors.
  • the photolithographic alignment techniques described herein may be advantageously used to align two fiber arrays.
  • alignment features are formed to register precisely between the two fiber connectors. For example, one connector may have a protruding feature, while another connector may have a recess feature. On each fiber connector, the alignment features are aligned with the fiber holes with lithographic precision. When the features of two connectors mate, the fibers of one connector are aligned with the fibers of the other connector with an accuracy of about one micron or better. Tight alignment tolerances are desired in order to have a low insertion loss in the connector.
  • one fiber in one fiber array physically contacts a corresponding fiber in another array, such that there is no air gap between the fibers.
  • An air gap produces a variable loss due to the resulting interferometric effects.
  • Two possible implementations of aligned fiber arrays are shown in FIGS. 10 and 11.
  • FIG. 10 illustrates one embodiment of two aligned fiber arrays 1000 , 1010 .
  • the fiber arrays 1000 , 1010 are aligned by visually aligning holes 1002 A, 1002 B in the two wafers 1000 , 1010 or using one or more pins 1004 A, 1004 B that would slide through the holes 1002 A, 1002 B.
  • FIG. 11 illustrates another embodiment of two aligned fiber arrays 1100 , 1102 .
  • Wafer pieces 1104 A, 1104 B are patterned to fit in alignment groves etched into the two fiber wafers 1100 , 1102 .
  • FIG. 13 illustrates a top view of another embodiment of kinematic alignment features between two fiber arrays or wafers.
  • three alignment slots or grooves 1300 A- 1300 C are properly designed and etched into one silicon wafer.
  • three small knobs 1302 A- 1302 C are formed that align into the three grooves 1300 A- 1300 C, which have substantially the same width as the knobs 1302 A- 1302 C but are longer.
  • a plurality of holes are formed in a substrate 400 as in FIGS. 4A and 4B with a process other than deep reactive ion etching, and kinematic alignment flaps 404 A- 404 F are formed in the substrate 400 with a process, such as deep reactive ion etching.
  • FIG. 14 illustrates one embodiment of a fiber termination 1408 with a plurality of etched holes 1410 and a plurality of recesses 1404 formed on one side 1406 of the substrate 1400 .
  • the holes 1410 are etched with one or more processes as described above.
  • the recesses 1404 are formed by removing material from selected parts of the ‘front’ side 1406 of the substrate 1400 .
  • the recesses 1404 may be formed by wet etching, plasma etching, laser ablation, sand blasting or some other suitable method.
  • substrate material is removed everywhere on the front side 1406 of the substrate 1400 except a ring of substrate material around each hole 1410 .
  • the recesses 1404 are formed before a plurality of fibers 1402 are inserted in the holes 1410 .
  • the front side 1406 of the substrate 1400 and the fiber ends are polished.
  • a relatively small amount of substrate material e.g., the rings located around the fibers 1402 is polished with the fiber ends.
  • the substrate 1400 with recesses 1404 allows more uniform polishing of the ends of the fibers 1402 and less wear of the polishing surface.
  • the substrate 1400 with recesses 1404 facilitates the physical connection of two fiber connectors, as shown in FIGS. 10 and 11.
  • the pressure is located near the fiber ends to provide low insertion loss.

Landscapes

  • Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • General Physics & Mathematics (AREA)
  • Optics & Photonics (AREA)
  • Optical Couplings Of Light Guides (AREA)
  • Internal Circuitry In Semiconductor Integrated Circuit Devices (AREA)

Abstract

A high density fiber terminator/connector and methods of making the high density fiber terminator/connector are provided. One method comprises using deep reactive ion etching to etch a plurality of holes in a silicon substrate and placing a fiber in at least one hole.

Description

    CLAIM OF PRIORITY
  • The present application claims priority to U.S. Provision Application No. 60/211,192, entitled “High Density Fiber Termination/Connector,” filed on Jun. 13, 2000, assigned to the Assignee of the present application, and is hereby incorporated by reference in its entirety.[0001]
  • BACKGROUND OF THE INVENTION
  • 1. Field of the Invention [0002]
  • The present invention relates to fiber optic terminators/connectors, and more particularly to a high density fiber terminator/connector. [0003]
  • 2. Description of the Related Art [0004]
  • Common fiber optic terminations/connectors terminate one fiber at a time. There are several connector styles (e.g., FC/PC, LC), but in all cases, a single fiber is inserted and glued in a precision ferrule, which is typically made of ceramic. The end of the ferrule and fiber are polished together to provide a smooth surface or a desired shape. [0005]
  • When multiple fibers are connected together, each fiber is terminated with an FC/PC connector as described, and the fibers are connected together one pair at a time. This process is extremely time-consuming and costly when connecting a large number of fibers together. [0006]
  • State of the art high density fiber connectors use micromachined v-grooves in which the fibers are located in v-shaped channels. This technology results in linear arrays of fibers, where the relative positioning of the fibers is limited by the fabrication precision (or imprecision) of the fiber v-grooves and by a diameter uniformity (or non-uniformity) of the fibers. When v-grooves are stacked to provide two-dimensional arrays of fibers, the relative position accuracy is further reduced and results in increased insertion loss in the connection of two such arrays. [0007]
  • SUMMARY OF THE INVENTION
  • A high density fiber terminator/connector and methods of making the high density fiber terminator/connector are provided in accordance with the present invention. One method uses silicon micro-machining to terminate multiple fibers simultaneously. This simplifies the process and improves the alignment of connecting multiple fibers together or positioning multiple fibers together to free-space optical elements. [0008]
  • One method uses Deep Reactive Ion Etching (DRIE) to make precise holes in a silicon wafer. The holes in the silicon may be arranged in any desired pattern by using, for example, a mask fabrication process with electron-beam writing of the mask, such as photolithography masking. A single photolithographic mask provides extremely high precision location positioning, and the relative position of each fiber in the holes can be accurately controlled. The accuracy in the relative positioning of the fibers ensures that all fibers are simultaneously aligned. Thus, photolithographic masking and deep reactive ion etching enable the fabrication of connectors for a plurality of fibers. Photolithographic masking and deep reactive ion etching also allow multiple fibers to be accurately aligned to free-space optical components. [0009]
  • One aspect of the invention relates to a method of making an optical fiber terminator. The method comprises using deep reactive ion etching to etch a plurality of holes in a silicon substrate, wherein each hole is sized to fit an optical fiber; and placing an optical fiber in at least one hole. [0010]
  • Another aspect of the invention relates to an optical fiber terminator in an optical switch. The optical fiber terminator comprises a silicon substrate with a plurality of holes formed by deep reactive ion etching, wherein each hole is sized to fit an optical fiber. [0011]
  • Another aspect of the invention relates to an optical fiber terminator with holes formed to allow insertion of fibers at an angle with respect to the substrate surface. [0012]
  • Another aspect of the invention relates to a method of making an optical fiber terminator. The method comprises etching a plurality of holes in a silicon substrate, wherein each hole is sized to fit an optical fiber; forming a plurality of flaps in the substrate around each hole, the flaps being configured for kinematic alignment of an optical fiber in each hole; and placing an optical fiber in at least one hole. [0013]
  • Another aspect of the invention relates to an optical fiber terminator, which comprises a silicon substrate. The silicon substrate comprises a plurality of holes etched in the silicon substrate, wherein each hole is sized to fit an optical fiber. The silicon substrate also comprises a plurality of flaps formed in the substrate around each hole. The flaps are configured for kinematic alignment of an optical fiber in each hole.[0014]
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • FIG. 1 illustrates one embodiment of an array of holes etched into a silicon wafer/substrate. [0015]
  • FIG. 2 illustrates one embodiment of a plurality of optical fibers inserted in a plurality of holes of a portion of the substrate of FIG. 1. [0016]
  • FIG. 3 illustrates one embodiment of angling a plurality of holes in a substrate to allow fibers to be positioned and pointed at a specific angle. [0017]
  • FIGS. [0018] 4A-4B illustrate one embodiment of a substrate with a plurality of holes and a plurality of vertical flaps positioned at an equal distance from each other around each hole.
  • FIG. 5 illustrates the wafer of FIG. 2 with top ends of the fibers removed. [0019]
  • FIG. 6 illustrates one embodiment of a plurality of substrate components removed from a base substrate. [0020]
  • FIG. 7 illustrates one embodiment of a coating formed on one side of the substrate and fibers in FIG. 5. [0021]
  • FIG. 8 illustrates one embodiment of the substrate in FIG. 5 with a plurality of MEMS components inserted in etched recesses. [0022]
  • FIG. 9 illustrates one embodiment of the substrate in FIG. 5 with alignment notches, which are used to align the fiber array to a lens array. [0023]
  • FIG. 10 illustrates one embodiment of two aligned fiber arrays. [0024]
  • FIG. 11 illustrates another embodiment of two aligned fiber arrays. [0025]
  • FIG. 12 illustrates one embodiment of an angled fiber array. [0026]
  • FIG. 13 illustrates a top view of another embodiment of kinematic alignment features between two fiber arrays. [0027]
  • FIG. 14 illustrates one embodiment of a substrate with a plurality of etched holes and a plurality of recesses formed on one surface of the substrate.[0028]
  • DETAILED DESCRIPTION
  • FIG. 1 illustrates one embodiment of an array of holes [0029] 102 (referred to herein individually or collectively as ‘102’) etched into a silicon wafer/substrate 100. The substrate 100 may be between about 200 microns to about 650 microns in thickness. In one embodiment, the substrate 100 is 600 microns thick.
  • In one embodiment, the [0030] holes 102 are etched with Deep Reactive Ion Etching (DRIE) processes. The holes in the silicon substrate 100 may be arranged in any desired pattern by using, for example, a mask fabrication process with electron-beam writing of the mask, such as photolithography masking. A mask is a layer with openings in desired locations to expose an underlying material for etching. A single photolithographic mask provides extremely high precision location positioning. Masks written by electron-beam lithography typically have about 10 nm to 100 nm accuracy in positioning the locations of features in the mask. Thus, the relative position of each fiber in the holes can be accurately controlled.
  • The [0031] substrate 100 may have any number of holes 102 etched in any desired pattern. Each hole 102 is sufficiently sized to allow an optical fiber 200 (FIG. 2) to fit through the hole 102 (FIG. 1). In one embodiment, each hole is formed to closely match the diameter of an optical fiber, which is typically 125 microns.
  • FIG. 2 illustrates one embodiment of a plurality of [0032] optical fibers 200A-200C (referred to herein individually or collectively as ‘fiber 200’) inserted in a plurality of holes 102A-102C of a portion of the substrate 100 of FIG. 1. In FIGS. 2-5 and 7-12, a small number of fibers and holes are shown, but the methods described herein may be applied to a very large number of fibers and holes.
  • A fiber (core plus cladding) [0033] 200 is typically about 125 microns in diameter. The core of a fiber 200 is typically about 9 microns in diameter, but the core is conventionally not easily separable from the cladding of the fiber 200 because both the core and the cladding are typically made out of glass. The coating or buffer 204 around the fiber 200 typically comprises plastic and may be separated from the fiber 200. The diameter of the buffer 204 is typically between 250 microns and 900 microns.
  • In one embodiment, each [0034] hole 102 in FIG. 2 provides a 5-micron space between an exterior surface (e.g., cylindrical) of a fiber 200 and the hole 102. Thus, one embodiment of the hole 102 is about 135 microns in diameter to provides a 5-micron space between an exterior surface (e.g., cylindrical) of a fiber 200 with a 25 micron diameter and the hole 102. Alternatively, if a fiber 200 is 125 microns in diameter, and each hole 102 is 130 microns in diameter, there is a 2.5-micron clearance on each side for the fiber 200 to pass through the hole 102. In another embodiment, if a fiber 200 is 125 microns in diameter, and each hole 102 is 127 microns in diameter, there is a 1-micron clearance on each side for the fiber 200 to pass through the hole 102.
  • In one embodiment, each [0035] hole 102 is substantially cylindrical in shape. In other embodiments, each hole 102 may be non-cylindrical, such as a triangle, a rectangle or a pentagon.
  • The [0036] optical fibers 200A-200C in FIG. 2 are stripped (removing their buffer coating 204A-204C and exposing the bare fiber 200A-200C), a small amount of glue 206A-206C is applied to the fiber coatings 204A-204C, and the bare fibers 200A-200C are slipped into the holes 102A-102C in the silicon wafer 100. There are many types of glue that can be used, such as a thermal cure epoxy, which cures at 120 degrees Celsius from Epotek.
  • FIG. 3 illustrates one embodiment of angling a plurality of [0037] holes 304A-304B in a substrate 300 to allow fibers 302A-302B to be positioned and pointed at a specific angle. The holes 304A-304B in FIG. 3 may be formed with any suitable process, such as deep reactive ion etching. Each hole 304 may also contain micro-machined kinematic alignment mechanisms to position the optical fiber at the center of the hole 304. Micro-machined kinematic alignment mechanisms are described herein and in the U.S. Provisional Application referenced above and incorporated by reference.
  • FIG. 12 illustrates one embodiment of an angled optical fiber array/[0038] terminator 1200. In FIG. 12, deep reactive ion etching forms a plurality of holes 1204A-1204C in the substrate. A front surface 1208 of the substrate may have a hole 1204 sized to fit an optical fiber 1202 and a locator 1206 at the edge of the slotted hole 1204 to position a fiber 1202 precisely on that surface 1208. In other words, each hole 1204 is sized to fit an optical fiber 1202 in one direction 1210A but oversized in another direction 1210B. Thus, each slotted hole 1204 allows a fiber 1202 to be inserted at an angle with respect to the substrate surface 1208.
  • The angled insertion of the [0039] fiber arrays 300, 1200 in FIGS. 3 and 12 provides low back-reflection, which is important when the fiber array 300 or 1200 is used as a termination into free-space (an unguided medium with a different optical index of refraction). Back-reflection may be further reduced by coating the fiber array 300 or 1200 with an anti-reflection coating. Terminating fibers 304A-304B and 1202A-1202C at an angle also allows a ball lens to collimate light, such that the collimated light comes out at an angle with respect to the substrate with low aberrations. If a graded index lens or aspheric lens is used, then it is important to tilt the lens with respect to the fiber array 300 or 1200 in order to provide collimated light with low aberrations.
  • In another embodiment, there are no locators [0040] 1206 near the front side, and loading (e.g., with other substrates or devices) is used to precisely position the fibers 1202A-1202C at an angle.
  • FIGS. [0041] 4A-4B illustrate one embodiment of a substrate 400 with a plurality of holes 408A-408B and a plurality of vertical flaps 404A-404F positioned at an equal distance from each other around each hole 408. FIG. 4B is a top view. Although three flaps 404A-404C, 404D-404F are shown for each hole 408A, 408B, there may be less than three or greater than three flaps for each hole 408A, 408B, in other embodiments. The flaps 404A-404F may be formed by deep reactive ion etching portions of the silicon wafer 400. The first set of flaps 404A-404C support a first fiber 402A equally and center the fiber 402A within the first hole 408A. Similarly, the second set of flaps 404D-404F support a second fiber 402B equally and center the fiber 402B within the second hole 408B. The flaps provide kinematic alignment or self-centering of a fiber 402 in a hole 408, which overcomes the problem of etching non-uniformities in the wafer 400.
  • In FIG. 4A, each hole [0042] 408 may be tapered to allow a fiber 402 to more easily slide into the hole 408. In another embodiment, each hole 408 in FIGS. 4A-4B is not tapered.
  • FIG. 5 illustrates the [0043] wafer 202 of FIG. 2 with top ends of the fibers 200A-200C removed, e.g., by cleaving or etching. The structure 500 in FIG. 5 may be referred to as a ‘fiber array,’ a ‘fiber connector’ or a ‘fiber terminator.’ In one embodiment, a top side 502 of the entire silicon wafer 202 in FIG. 5 and the glued fibers 200A-200C is polished by a lapping and polishing process. The lapping and polishing process may include the use of chemical mechanical polishing (CMP) slurries, or using polishing pads with Alumina grit of various sizes that are lubricated with water. Some polishing processes are known in the art, and some recipes are provided by vendors of polishing equipment.
  • One of the advantages of the [0044] structure 500 in FIG. 5 is that all fibers 200A-200C may be polished simultaneously. Once the ends of the fibers 200A-200C are polished, the wafer 202 in FIG. 5 may be separated into individual components, as shown in FIG. 6.
  • FIG. 6 illustrates one embodiment of a plurality of [0045] substrate components 602A-602D removed from a base substrate 604 (as shown by the arrow). The separation may be done by various methods, including but not limited to dicing with a diamond saw.
  • FIG. 7 illustrates one embodiment of a [0046] coating 702 formed on one side 502 of the substrate 202 and fibers 200A-200C in FIG. 5. In one embodiment, before separating the components 602A-602D (FIG. 6) and after polishing, an anti-reflection (AR) coating 702 is applied by depositing films of various materials on the side 502 the silicon wafer 202 where the fiber ends have been polished. In one embodiment, the AR coating 702 uses multiple layers of dielectric materials, where the materials and designs may vary. Multiple layer dielectrics form interferometric effects, which are used to eliminate reflection from the surface 502 and provide almost 100% transmission.
  • In other embodiments, the [0047] coating 702 may comprise a chemically sensitive film for chemical sensors, or a metal coating for total reflection. The coating 702 is a way to make a sensor or to improve the optical characteristics of the fiber/ambient interface 502.
  • The processed substrates described above may be combined with microelectronic mechanical system (MEMS) components, such as small micro-machined movable mirrors and electronics. The MEMS components may be placed in recesses in the [0048] silicon wafer 202, as shown in FIG. 8, to prevent the MEMS components from being damaged during a polishing process.
  • FIG. 8 illustrates one embodiment of the [0049] substrate 202 in FIG. 5 with a plurality of MEMS components 804A, 804B inserted in etched recesses 802A, 802B. One advantage of the structure 800 in FIG. 8 is that the optical fibers 200A-200C are aligned to the MEMS components 804A, 804B using photolithography masking, which provides very good alignment. A single photolithographic mask may be used when the MEMS recesses 802A, 802B and the fiber holes in FIG. 8 are etched during the same etching process, such as deep reactive ion etching. A single photolithographic mask provides extremely high precision location positioning between all components. Masks written by electron-beam lithography typically have about 10 nanometer-100 nm accuracy in positioning the locations of features in the mask. The structure 800 in FIG. 8 may be used in fabricating a high density, MEMS fiber optic switch.
  • FIG. 9 illustrates one embodiment of the [0050] substrate 202 in FIG. 5 with alignment notches 908A, 908B, which are used to align the fiber array 900 to a lens array 902. In one embodiment, the alignment notches 908A, 908B and the fiber holes in FIG. 9 are etched into the silicon wafer 202 during the same etching process, such as deep reactive ion etching. The alignment notches 908A, 908B are aligned with respect to the fiber holes in the substrate 202 with lithographic precision.
  • The [0051] lens array 902 in FIG. 9 comprises a plurality of lenses 904A-904C and protruding stubs 906A, 906B, which are intended to fit into the notches 908A, 908B. In another embodiment, notches are etched into the lens array 902 and stubs are formed (e.g., by etching the surface of the substrate 202) in the fiber array 900. In other embodiments, instead of a lens array 902 with lenses 904A-904C as shown in FIG. 9, the array 902 may comprise diffraction gratings, MEMS components, or anything that a user desires to align with the fiber array 902.
  • The fiber terminators described herein may be used for connecting fibers, such as standard single fiber connectors. In addition, the photolithographic alignment techniques described herein may be advantageously used to align two fiber arrays. In one embodiment, alignment features are formed to register precisely between the two fiber connectors. For example, one connector may have a protruding feature, while another connector may have a recess feature. On each fiber connector, the alignment features are aligned with the fiber holes with lithographic precision. When the features of two connectors mate, the fibers of one connector are aligned with the fibers of the other connector with an accuracy of about one micron or better. Tight alignment tolerances are desired in order to have a low insertion loss in the connector. [0052]
  • In one embodiment, one fiber in one fiber array physically contacts a corresponding fiber in another array, such that there is no air gap between the fibers. An air gap produces a variable loss due to the resulting interferometric effects. Two possible implementations of aligned fiber arrays are shown in FIGS. 10 and 11. [0053]
  • FIG. 10 illustrates one embodiment of two aligned [0054] fiber arrays 1000, 1010. In FIG. 10, the fiber arrays 1000, 1010 are aligned by visually aligning holes 1002A, 1002B in the two wafers 1000, 1010 or using one or more pins 1004A, 1004B that would slide through the holes 1002A, 1002B.
  • FIG. 11 illustrates another embodiment of two aligned [0055] fiber arrays 1100, 1102. Wafer pieces 1104A, 1104B are patterned to fit in alignment groves etched into the two fiber wafers 1100, 1102.
  • FIG. 13 illustrates a top view of another embodiment of kinematic alignment features between two fiber arrays or wafers. In FIG. 13, three alignment slots or [0056] grooves 1300A-1300C are properly designed and etched into one silicon wafer. On another silicon wafer, three small knobs 1302A-1302C are formed that align into the three grooves 1300A-1300C, which have substantially the same width as the knobs 1302A-1302C but are longer.
  • In one embodiment, a plurality of holes are formed in a [0057] substrate 400 as in FIGS. 4A and 4B with a process other than deep reactive ion etching, and kinematic alignment flaps 404A-404F are formed in the substrate 400 with a process, such as deep reactive ion etching.
  • FIG. 14 illustrates one embodiment of a [0058] fiber termination 1408 with a plurality of etched holes 1410 and a plurality of recesses 1404 formed on one side 1406 of the substrate 1400. The holes 1410 are etched with one or more processes as described above. The recesses 1404 are formed by removing material from selected parts of the ‘front’ side 1406 of the substrate 1400. The recesses 1404 may be formed by wet etching, plasma etching, laser ablation, sand blasting or some other suitable method. In one embodiment, substrate material is removed everywhere on the front side 1406 of the substrate 1400 except a ring of substrate material around each hole 1410. In one embodiment, the recesses 1404 are formed before a plurality of fibers 1402 are inserted in the holes 1410.
  • In one embodiment, after the [0059] fibers 1402 are inserted in the holes 1410, the front side 1406 of the substrate 1400 and the fiber ends are polished. With the recesses 1404 on the front side 1406, a relatively small amount of substrate material (e.g., the rings) located around the fibers 1402 is polished with the fiber ends. Thus, the substrate 1400 with recesses 1404 allows more uniform polishing of the ends of the fibers 1402 and less wear of the polishing surface.
  • In addition, the [0060] substrate 1400 with recesses 1404 facilitates the physical connection of two fiber connectors, as shown in FIGS. 10 and 11. When pressure is applied between the two connectors, the pressure is located near the fiber ends to provide low insertion loss.
  • The above-described embodiments of the present invention are merely meant to be illustrative and not limiting. Various changes and modifications may be made without departing from the invention in its broader aspects. The appended claims encompass such changes and modifications within the spirit and scope of the invention. [0061]

Claims (10)

What is claimed is:
1. An optical fiber assembly comprising a substrate with at least one hole and one alignment groove formed in the substrate, the hole configured to receive a tip of a fiber and alignment groove configured to align an object in place.
2. The optical fiber assembly of claim 1, wherein the object is an alignment pin
3. The optical fiber assembly of claim 1, wherein the object is a lens array
4. The optical fiber assembly of claim 1, wherein the object is a diffraction grating
5. The optical fiber assembly of claim 1, wherein the object is a microelectronic mechanical system
6. The optical fiber assembly of claim 1, wherein the object is a second optical fiber assembly
7. The optical fiber assembly of claim 1, wherein the alignment groove has a depth of less than about one-fourth of a total thickness of the substrate.
8. The optical fiber assembly of claim 1, wherein the alignment groove is etched through an entire thickness of the substrate.
9. An optical fiber assembly comprising a substrate with at least one hole and a plurality of flaps in the substrate around a hole, the hole configured to receive a tip of a fiber and the flaps configured to align the fiber in the hole.
10. A method of making an optical fiber assembly, the method comprising:
using deep reactive ion etching to etch at least one hole in a silicon substrate, wherein the hole is sized to fit an optical fiber;
etching an alignment groove in said silicon substrate that is aligned with said hole; and
placing an optical fiber in the hole.
US10/448,561 2000-06-13 2003-05-29 High density fiber terminator/connector Abandoned US20030202769A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US10/448,561 US20030202769A1 (en) 2000-06-13 2003-05-29 High density fiber terminator/connector

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US21119200P 2000-06-13 2000-06-13
US09/855,406 US6595698B2 (en) 2000-06-13 2001-05-15 High density fiber terminator/connector
US10/448,561 US20030202769A1 (en) 2000-06-13 2003-05-29 High density fiber terminator/connector

Related Parent Applications (1)

Application Number Title Priority Date Filing Date
US09/855,406 Continuation US6595698B2 (en) 2000-06-13 2001-05-15 High density fiber terminator/connector

Publications (1)

Publication Number Publication Date
US20030202769A1 true US20030202769A1 (en) 2003-10-30

Family

ID=26905924

Family Applications (2)

Application Number Title Priority Date Filing Date
US09/855,406 Expired - Fee Related US6595698B2 (en) 2000-06-13 2001-05-15 High density fiber terminator/connector
US10/448,561 Abandoned US20030202769A1 (en) 2000-06-13 2003-05-29 High density fiber terminator/connector

Family Applications Before (1)

Application Number Title Priority Date Filing Date
US09/855,406 Expired - Fee Related US6595698B2 (en) 2000-06-13 2001-05-15 High density fiber terminator/connector

Country Status (3)

Country Link
US (2) US6595698B2 (en)
AU (1) AU2001269755A1 (en)
WO (1) WO2001096914A2 (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030063861A1 (en) * 2001-10-01 2003-04-03 Fouquet Julie E. Precisely configuring optical fibers and other optical elements using an apertured wafer positioner
EP1619528A1 (en) * 2004-07-23 2006-01-25 Shinko Electric Industries Co., Ltd. Semiconductor device with an optical waveguide mounting member and the method of manufacturing thereof
US20110103747A1 (en) * 2009-10-30 2011-05-05 Hon Hai Precision Industry Co., Ltd. Optical fiber connector configured with separated seat member and lens member
US20130071069A1 (en) * 2011-09-15 2013-03-21 Hon Hai Precision Industry Co., Ltd. Optical fiber connector
US20130195402A1 (en) * 2011-08-23 2013-08-01 Schleifring Und Apparatebau Gmbh Precision two-dimensional fiber-collimator-array
US20140086533A1 (en) * 2012-09-27 2014-03-27 Ezra GOLD Method for alignment between two optical components
DE112012003394B4 (en) 2011-08-16 2022-08-25 International Business Machines Corporation Photonic integrated circuit device and method for its manufacture, coupling system of a photonic integrated circuit and coupling unit of a photonic chip

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10057127A1 (en) * 2000-11-16 2002-06-06 Schott Glas Method for arranging multiple fibre ends of a bundle of glass, quartz or plastic fibre light waveguides into multiple preset positions, uses fixing device with multiple openings for fibre ends
US6522817B2 (en) * 2000-12-18 2003-02-18 Veritech, Inc. Optical fiber array and method of formation
JP2002350674A (en) * 2001-05-23 2002-12-04 Nippon Sheet Glass Co Ltd Optical module and its manufacturing method
US6827500B2 (en) * 2001-06-29 2004-12-07 Lucent Technologies Inc. Precision two dimensional optical fiber array
US6632026B2 (en) * 2001-08-24 2003-10-14 Nihon Microcoating Co., Ltd. Method of polishing optical fiber connector
US7024090B2 (en) * 2001-09-26 2006-04-04 Shipley Company, L.L.C. Optical fiber array with variable fiber angle alignment and method for the fabrication thereof
DE60213550T2 (en) * 2001-12-19 2006-12-14 Nippon Telegraph And Telephone Corp. fiber optic array
JP2003215388A (en) * 2002-01-25 2003-07-30 Hitachi Metals Ltd Optical fiber assembly with lens and manufacturing method therefor
US6948862B2 (en) * 2002-02-22 2005-09-27 Brown Joe D Apparatus and method for coupling laser energy into small core fibers
US7090411B2 (en) * 2002-02-22 2006-08-15 Brown Joe D Apparatus and method for diffusing laser energy that fails to couple into small core fibers, and for reducing coupling to the cladding of the fiber
US6823127B2 (en) * 2002-09-05 2004-11-23 Intel Corporation Apparatus for holding a fiber array
US6890588B2 (en) * 2002-09-05 2005-05-10 Intel Corporation Method and apparatus for applying a gel
US20070292087A1 (en) * 2006-06-19 2007-12-20 Joe Denton Brown Apparatus and method for diffusing laser energy that fails to couple into small core fibers, and for reducing coupling to the cladding of the fiber
US7548682B2 (en) * 2007-03-26 2009-06-16 Trex Enterprises Corp. Optical fiber array alignment unit
CN101915965B (en) * 2010-08-23 2013-11-06 清华大学 Grating coupler and package structure thereof
WO2013150089A1 (en) 2012-04-04 2013-10-10 Tyco Electronics Raychem Bvba Mechanical alignment device for positioning optical fibers
CN103852822B (en) * 2012-12-04 2016-04-13 上海华虹宏力半导体制造有限公司 The manufacture method of optical fiber align pedestal array
US9766420B2 (en) 2013-03-15 2017-09-19 Joe Denton Brown Apparatus and method for absorbing laser energy that fails to couple into the core of a laser fiber, and for absorbing the energy that has been transmitted to the cladding of the laser
US20150118770A1 (en) * 2013-10-28 2015-04-30 Avago Technologies General Ip (Singapore) Pte. Ltd. Wafer-level packages having voids for opto-electronic devices
US9541717B2 (en) 2015-01-30 2017-01-10 Avago Technologies General IP (Singapore) Pta. Ltd. Optoelectronic assembly incorporating an optical fiber alignment structure
CN113056691B (en) * 2018-10-31 2023-07-21 安捷伦科技有限公司 Optical coupler and modular optical device including the same

Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5294790A (en) * 1991-10-09 1994-03-15 Olympus Optical Co., Ltd. Probe unit for near-field optical scanning microscope
US5346583A (en) * 1993-09-02 1994-09-13 At&T Bell Laboratories Optical fiber alignment techniques
US5355429A (en) * 1992-12-30 1994-10-11 Minnesota Mining And Manufacturing Company Optical fiber strain relief apparatus
US5550942A (en) * 1994-07-18 1996-08-27 Sheem; Sang K. Micromachined holes for optical fiber connection
US5566262A (en) * 1993-05-14 1996-10-15 The Furukawa Electric Co., Ltd. Optical fiber array and a method of producing the same
US5769698A (en) * 1997-02-13 1998-06-23 Nuvisions International, Inc. Polishing disc for holding connector-mounted optical fibers
US5892870A (en) * 1995-11-16 1999-04-06 Fiber Connections Inc. Fibre optic cable connector
US6078714A (en) * 1998-07-30 2000-06-20 The Boeing Company Fiber optic bundle interface cooling system
US6215114B1 (en) * 1997-09-25 2001-04-10 Canon Kk Optical probe for detecting or irradiating light and near-field optical microscope having such probe and manufacturing method of such probe
US20010010745A1 (en) * 2000-01-13 2001-08-02 Lowry Brian C. Contoured large screen display
US6328482B1 (en) * 1998-06-08 2001-12-11 Benjamin Bin Jian Multilayer optical fiber coupler
US6396995B1 (en) * 1999-05-20 2002-05-28 Illumina, Inc. Method and apparatus for retaining and presenting at least one microsphere array to solutions and/or to optical imaging systems
US20020191944A1 (en) * 1999-12-15 2002-12-19 Moore David Frank Microlamp
US6621976B2 (en) * 1999-11-05 2003-09-16 Digital Optics Corp. Integration of array on non-rod shaped optical elements with array of fibers in a structure and associated methods

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3751810T2 (en) 1986-11-15 1996-09-26 Sumitomo Electric Industries Process for the production of an optical connector
US5394498A (en) 1993-11-05 1995-02-28 At&T Corp. Optical fiber array and process of manufacture
JPH08327486A (en) 1995-05-30 1996-12-13 Mitsubishi Cable Ind Ltd Manufacture of fiber-optic sensor
JPH10111426A (en) 1996-10-04 1998-04-28 Yokogawa Electric Corp Optical fiber coupler
US5907650A (en) 1997-06-26 1999-05-25 Fiberguide Industries, Inc. High precision optical fiber array connector and method
KR100248054B1 (en) 1997-08-14 2000-03-15 윤종용 Fiber array module using the soldering process fabrication method thereof

Patent Citations (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5294790A (en) * 1991-10-09 1994-03-15 Olympus Optical Co., Ltd. Probe unit for near-field optical scanning microscope
US5355429A (en) * 1992-12-30 1994-10-11 Minnesota Mining And Manufacturing Company Optical fiber strain relief apparatus
US5566262A (en) * 1993-05-14 1996-10-15 The Furukawa Electric Co., Ltd. Optical fiber array and a method of producing the same
US5346583A (en) * 1993-09-02 1994-09-13 At&T Bell Laboratories Optical fiber alignment techniques
US5550942A (en) * 1994-07-18 1996-08-27 Sheem; Sang K. Micromachined holes for optical fiber connection
US5892870A (en) * 1995-11-16 1999-04-06 Fiber Connections Inc. Fibre optic cable connector
US5769698A (en) * 1997-02-13 1998-06-23 Nuvisions International, Inc. Polishing disc for holding connector-mounted optical fibers
US6215114B1 (en) * 1997-09-25 2001-04-10 Canon Kk Optical probe for detecting or irradiating light and near-field optical microscope having such probe and manufacturing method of such probe
US6328482B1 (en) * 1998-06-08 2001-12-11 Benjamin Bin Jian Multilayer optical fiber coupler
US6078714A (en) * 1998-07-30 2000-06-20 The Boeing Company Fiber optic bundle interface cooling system
US6396995B1 (en) * 1999-05-20 2002-05-28 Illumina, Inc. Method and apparatus for retaining and presenting at least one microsphere array to solutions and/or to optical imaging systems
US6621976B2 (en) * 1999-11-05 2003-09-16 Digital Optics Corp. Integration of array on non-rod shaped optical elements with array of fibers in a structure and associated methods
US20020191944A1 (en) * 1999-12-15 2002-12-19 Moore David Frank Microlamp
US20010010745A1 (en) * 2000-01-13 2001-08-02 Lowry Brian C. Contoured large screen display

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030063861A1 (en) * 2001-10-01 2003-04-03 Fouquet Julie E. Precisely configuring optical fibers and other optical elements using an apertured wafer positioner
US6766085B2 (en) * 2001-10-01 2004-07-20 Agilent Technologies, Inc. Precisely configuring optical fibers and other optical elements using an apertured wafer positioner
EP1619528A1 (en) * 2004-07-23 2006-01-25 Shinko Electric Industries Co., Ltd. Semiconductor device with an optical waveguide mounting member and the method of manufacturing thereof
US20060018590A1 (en) * 2004-07-23 2006-01-26 Kei Murayama Optical waveguide mounting member, substrate, semiconductor device, method of manufacturing optical waveguide mounting member, and method of manufacturing substrate
US7251391B2 (en) 2004-07-23 2007-07-31 Shinko Electric Industries Co., Ltd. Optical waveguide mounting member, substrate, semiconductor device, method of manufacturing optical waveguide mounting member, and method of manufacturing substrate
US8235601B2 (en) * 2009-10-30 2012-08-07 Hon Hai Precision Ind. Co., Ltd. Optical fiber connector configured with separated seat member and lens member
US20110103747A1 (en) * 2009-10-30 2011-05-05 Hon Hai Precision Industry Co., Ltd. Optical fiber connector configured with separated seat member and lens member
DE112012003394B4 (en) 2011-08-16 2022-08-25 International Business Machines Corporation Photonic integrated circuit device and method for its manufacture, coupling system of a photonic integrated circuit and coupling unit of a photonic chip
US20130195402A1 (en) * 2011-08-23 2013-08-01 Schleifring Und Apparatebau Gmbh Precision two-dimensional fiber-collimator-array
US9500809B2 (en) * 2011-08-23 2016-11-22 Schleifring Und Apparatebau Gmbh Precision two-dimensional fiber-collimator-array
US20130071069A1 (en) * 2011-09-15 2013-03-21 Hon Hai Precision Industry Co., Ltd. Optical fiber connector
US8636423B2 (en) * 2011-09-15 2014-01-28 Hon Hai Precision Industry Co., Ltd. Optical fiber connector with positioning members
US20140086533A1 (en) * 2012-09-27 2014-03-27 Ezra GOLD Method for alignment between two optical components

Also Published As

Publication number Publication date
US20010051028A1 (en) 2001-12-13
US6595698B2 (en) 2003-07-22
AU2001269755A1 (en) 2001-12-24
WO2001096914A3 (en) 2003-05-30
WO2001096914A2 (en) 2001-12-20

Similar Documents

Publication Publication Date Title
US6595698B2 (en) High density fiber terminator/connector
US10983288B2 (en) Microfabrication method for optical components
US6928226B2 (en) Fiber and lens grippers, optical devices and methods of manufacture
US6945701B2 (en) Multi-piece fiber optic component and manufacturing technique
US6629780B2 (en) High-precision female format multifiber connector
US20040028344A1 (en) High-precision female format multifiber connector
US20040120682A1 (en) Securing optical elements and optical devices
EP0974077B1 (en) Method of forming optical rods including three-dimensional patterns on end faces thereof
US6773166B2 (en) Multi-piece fiber optic component and manufacturing technique
US7077577B2 (en) Multi-piece fiber optic component and manufacturing technique
US6950583B2 (en) Two-dimensional optical element array, two dimensional waveguide apparatus and methods for manufacturing the same
US20030174943A1 (en) Optical devices and methods of manufacture
US6899465B2 (en) Multi-piece fiber optic component and manufacturing technique
US20020172491A1 (en) Angled fiber termination and methods of making the same
US11333835B2 (en) Microfabrication method for optical components
WO2002061479A1 (en) Optical fiber array, and circuit connection method using the optical fiber array
WO2005114284A1 (en) Optical coupling element and method of manufacturing the optical coupling element
WO1992006396A1 (en) Optical fibre connector
JPH0777633A (en) Optical coupling device

Legal Events

Date Code Title Description
STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION