CA1264582A - Molecular bonded fiber optic couplers and method of fabrication - Google Patents
Molecular bonded fiber optic couplers and method of fabricationInfo
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- CA1264582A CA1264582A CA000519622A CA519622A CA1264582A CA 1264582 A CA1264582 A CA 1264582A CA 000519622 A CA000519622 A CA 000519622A CA 519622 A CA519622 A CA 519622A CA 1264582 A CA1264582 A CA 1264582A
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Abstract
MOLECULAR BONDED FIBER OPTIC COUPLERS
AND METHOD OF FABRICATION
Abstract of the Disclosure A fiber optic coupler is formed by heating juxtaposed optically flat surfaces formed on two lengths of optical fiber to the glass transition temperature. The fibers bond together while preserving the molecular composition of the fibers at bonded region. Depending upon the depth to which the fibers are lapped to form the optically flat surfaces, the coupler may be either an evanescent field coupler or a core intercept coupler. The fibers may be mounted on curved substrates and then lapped to form the optically flat surfaces. The optical throughput of a fiber may be monitored during assembly of a coupler to permit adjustment of the positions of the optically flat surfaces to produce a desired coupling efficiency. The fibers may then be bonded together by application of energy from a suitable coherent light source such as a CO2 laser.
AND METHOD OF FABRICATION
Abstract of the Disclosure A fiber optic coupler is formed by heating juxtaposed optically flat surfaces formed on two lengths of optical fiber to the glass transition temperature. The fibers bond together while preserving the molecular composition of the fibers at bonded region. Depending upon the depth to which the fibers are lapped to form the optically flat surfaces, the coupler may be either an evanescent field coupler or a core intercept coupler. The fibers may be mounted on curved substrates and then lapped to form the optically flat surfaces. The optical throughput of a fiber may be monitored during assembly of a coupler to permit adjustment of the positions of the optically flat surfaces to produce a desired coupling efficiency. The fibers may then be bonded together by application of energy from a suitable coherent light source such as a CO2 laser.
Description
4S8z MOLEt::ULAR BOhlDE~D FIBEP~ OPTIC COUPLERS
~ack~ro~L~d of the Inv~nIiqn This invention relates generally to rne~hods and apparatus for 5 bonding optical fibers ltog~ther. Mor~ particularly, this invention relates to methods and apparatus for forming fiber optic couplers. Still more particularly, this invention relates to methods and apparatus for forming a coherent molecular bond between two optical fibers.
Sorne familiarity with the propagation characteristics of light 10 within an optical fiber will facilitate an understanding of both the present invention and the prior art. Therefore, a brief discussion of fiber optic waveguides, normal modes of propagation of light in such waveguides and polarization of light is presented.
The behavior of an optical wave at an interface between two 1~ dielectric materials depends upon the refractive indices of the two materials. If the refractive indices of the two dielectrics are identical, then the wave propagates across the interface without experiencing any change. In the general case of different refractive indices, however, there will be a reflected wave, which remains in the medium 20 in which the wave was first propagating, and a refracted wave, which propagates beyoncl the dielectric interface into the second material with a change in direction relative to the incident wave. The relative intensities of the reflected and rcfract0d waves depend upon the angle of incidence and the difference between the refractive indices of the two
~ack~ro~L~d of the Inv~nIiqn This invention relates generally to rne~hods and apparatus for 5 bonding optical fibers ltog~ther. Mor~ particularly, this invention relates to methods and apparatus for forming fiber optic couplers. Still more particularly, this invention relates to methods and apparatus for forming a coherent molecular bond between two optical fibers.
Sorne familiarity with the propagation characteristics of light 10 within an optical fiber will facilitate an understanding of both the present invention and the prior art. Therefore, a brief discussion of fiber optic waveguides, normal modes of propagation of light in such waveguides and polarization of light is presented.
The behavior of an optical wave at an interface between two 1~ dielectric materials depends upon the refractive indices of the two materials. If the refractive indices of the two dielectrics are identical, then the wave propagates across the interface without experiencing any change. In the general case of different refractive indices, however, there will be a reflected wave, which remains in the medium 20 in which the wave was first propagating, and a refracted wave, which propagates beyoncl the dielectric interface into the second material with a change in direction relative to the incident wave. The relative intensities of the reflected and rcfract0d waves depend upon the angle of incidence and the difference between the refractive indices of the two
2~ materials. If an optical wave ori~inally propagating in ~he higher index material strikes the interface at an angle of incidence greater than or equal to a critical angle, there will be nc refracted wave propagated across the interface; and essentially all of the wave will be totally internally reflected back into the high index region. An exponentially 30 decaying evanescent wave associated with the incident wav~ extends a small distance beyond the interface.
Optical fiber has an elongated generally cylindrical core of higher re7ractive index and a cladding of lower refractive index surrounding the core. Optical fiber use the principle of total internal reflection to confine the energy associated with an optical wave to the core. The diameter of the core is so small that a light beam propagating in the core strikes the core only at angles greater than the critical angle.
Therefore, a light beam follows an essentially zig-zag path in the core 5 as it moves between points on the core-cladding interface.
It is well-known that a light wave may be represented by a time-varying electromagnetic field comprising orthogonal electric and magnetic field vectors having a frequency equal to the fraquency of the light wave. An electromagnetic wave propagating through a guiding 10 structure can be described by a set of normal modes. The normal modes are the permissible distributions of the electric and magnetic fields within the ~uiding structure, for example, a ~iber optic waveguide.
The field distributions are directly related to the distribution of energy within the structure. The normal modes ar~ generally represented by 15 mathematical functions that describe the field components in the wave in terms of the frequency and spatial distribution in the guiding structure. The specific functions that d~scribe the normal modes of a waveguide depend upon the geometry of the waveguide. ~or an optical fiber, where the guided wave is confined to a structure having a 2Q circular cross section of fixed dimensions, only fields having certain frequencies and spatial distributions will propagate without ssvere attenuation. The waves having field components that propagate unattenuat~d are the normal modes. A single mode ~ib~r will guide only one energy distribution, and a multimode fiber will simultaneously 2~ guide a plurality of energy distributions. The primary characteristic that determines the number of modes a fiber will guide is the ratio of the diameter of the fiber core to the wavelength of the light propagated by the fiber.
In describing the normal modesg it is convenient to refer to the 30 direction of the electric and magnetic ~ields relative to the direction of propagation of the wave. If only the electric field vector is perpendicular to the direction of propagation, which is usually called the optic axis, then the wave is said to be a transverss electric (TE) mode. If only ~he magnetic field vector is perpendicular to to the optic axis, the wave is a
Optical fiber has an elongated generally cylindrical core of higher re7ractive index and a cladding of lower refractive index surrounding the core. Optical fiber use the principle of total internal reflection to confine the energy associated with an optical wave to the core. The diameter of the core is so small that a light beam propagating in the core strikes the core only at angles greater than the critical angle.
Therefore, a light beam follows an essentially zig-zag path in the core 5 as it moves between points on the core-cladding interface.
It is well-known that a light wave may be represented by a time-varying electromagnetic field comprising orthogonal electric and magnetic field vectors having a frequency equal to the fraquency of the light wave. An electromagnetic wave propagating through a guiding 10 structure can be described by a set of normal modes. The normal modes are the permissible distributions of the electric and magnetic fields within the ~uiding structure, for example, a ~iber optic waveguide.
The field distributions are directly related to the distribution of energy within the structure. The normal modes ar~ generally represented by 15 mathematical functions that describe the field components in the wave in terms of the frequency and spatial distribution in the guiding structure. The specific functions that d~scribe the normal modes of a waveguide depend upon the geometry of the waveguide. ~or an optical fiber, where the guided wave is confined to a structure having a 2Q circular cross section of fixed dimensions, only fields having certain frequencies and spatial distributions will propagate without ssvere attenuation. The waves having field components that propagate unattenuat~d are the normal modes. A single mode ~ib~r will guide only one energy distribution, and a multimode fiber will simultaneously 2~ guide a plurality of energy distributions. The primary characteristic that determines the number of modes a fiber will guide is the ratio of the diameter of the fiber core to the wavelength of the light propagated by the fiber.
In describing the normal modesg it is convenient to refer to the 30 direction of the electric and magnetic ~ields relative to the direction of propagation of the wave. If only the electric field vector is perpendicular to the direction of propagation, which is usually called the optic axis, then the wave is said to be a transverss electric (TE) mode. If only ~he magnetic field vector is perpendicular to to the optic axis, the wave is a
3~ transverse magnetic (TM) mode. If both the electric and magnetic field lZ6~S8~
vectors are perp0ndicular to the optic axis, then the wave is a transverse electromagnetic (TEM~ mode. Nono of the normal modes require a definite direction of the field components; and in a TE mode, for example, the electric field may be in any direction that is 5 perpendicular to the optic axis.
The direction of the electric field vector in an electromagnetic wave is the polarization of the wave. In general, a wave will have random polarization in which there is a uniform distribution of electric field vectors pointing in all directions permissible for each mode. If all 10 the electric field vectors in a wave point in only one particular direction, the wave is linearly polarizod. If the electric field consists of two orthogonal electric field components of equal magnitude and 4~ out of phase, the electric fieid is circularly polarized because the net electric field is then a vector that rotates around the optic axis at an angular 15 velocity equal to the frequency of the wave. If the hAro linear polarizations have unequal magnitudes and phases that are neither equal nor opposite, the wave has elliptical polarization. In ~eneral, any arbitrary polarization can be represented by either the sum of two orthogonal linear polarizations, two oppositaly directed circular 20 polarizations or two oppositely directed elliptical polarizations having orthogonal semi-major axes.
Propa~ation characteristics such as velocity, for example, of an - optical wave depend upon the polarization of the wave and the index of refraction of the medium through which the light propagates. Certain 2~ materials, including optical fiber, have different refractivs indices for different polarizations. A material that has two refractive indices is said to be birefringent.
The polarization of an optical signal is sometirnes referred to as a mode. A standard single mode optical fiber will propagat0 two waves 30 of the same frequency and spatial distribution that have two different polarizations. A multimode fiber will propagate two polarizations for each propagation mode. Two different polarization components of ~he same normal mode can propa~ate through a birefringent material unchanyed except for a difference in velocity of the two polarizations.
35 Polarization is particularly important in interferometric sensors because ~zsi~s~
vectors are perp0ndicular to the optic axis, then the wave is a transverse electromagnetic (TEM~ mode. Nono of the normal modes require a definite direction of the field components; and in a TE mode, for example, the electric field may be in any direction that is 5 perpendicular to the optic axis.
The direction of the electric field vector in an electromagnetic wave is the polarization of the wave. In general, a wave will have random polarization in which there is a uniform distribution of electric field vectors pointing in all directions permissible for each mode. If all 10 the electric field vectors in a wave point in only one particular direction, the wave is linearly polarizod. If the electric field consists of two orthogonal electric field components of equal magnitude and 4~ out of phase, the electric fieid is circularly polarized because the net electric field is then a vector that rotates around the optic axis at an angular 15 velocity equal to the frequency of the wave. If the hAro linear polarizations have unequal magnitudes and phases that are neither equal nor opposite, the wave has elliptical polarization. In ~eneral, any arbitrary polarization can be represented by either the sum of two orthogonal linear polarizations, two oppositaly directed circular 20 polarizations or two oppositely directed elliptical polarizations having orthogonal semi-major axes.
Propa~ation characteristics such as velocity, for example, of an - optical wave depend upon the polarization of the wave and the index of refraction of the medium through which the light propagates. Certain 2~ materials, including optical fiber, have different refractivs indices for different polarizations. A material that has two refractive indices is said to be birefringent.
The polarization of an optical signal is sometirnes referred to as a mode. A standard single mode optical fiber will propagat0 two waves 30 of the same frequency and spatial distribution that have two different polarizations. A multimode fiber will propagate two polarizations for each propagation mode. Two different polarization components of ~he same normal mode can propa~ate through a birefringent material unchanyed except for a difference in velocity of the two polarizations.
35 Polarization is particularly important in interferometric sensors because ~zsi~s~
-4-only waves having the same polarization will produce the desired interferenca patterns.
An optical coupler joins two fibers for transmitting optical energy from one fiber to the other. Optical couplers are used in many applications of optical fiber, including constructing fiber optic inte~eromet~rs, resonators, sensor arrays and data buses.
Among the parameters that are considered in forming an optical coupler are the polarizations of the waves before and after coupling, the fraction of energy to be coupled from one fiber to the other, the insertion loss of the coupler and whether the fibers guide only a single mode or a multiplicity of rnodes.
Several methods have been employed for joining two fibers to form a coupler for transrnitting optical energy from one fiber to the other.
A first technique for joining two fibers results in the biconical tapered fiber optic coupler. The fibers are placed together, twisted and then heated to near the meiting point to fuse them during application of a force to stretch the fibers. The heating and twisting steps in the ~ormation of the biconical tapered fiber optic coupler result in alteration of the molecular arrangements of the materials comprising the joined fibers. In particular, the heating and twisting alters the distributions of impurities used as dopants to control the refractive indices of the core.
The refractive index of a material depends upon its molecular structure; therefors, forming the biconical tapered flber optic coupler, in general, produces localized changes in tho refractive indices of the fibers. These changes in refractive indices are uncontrollable and cause undesirable, uncontrollable reflections and refraction at the interfaces between the fibers. It is therefore difficult to fabricate biconical tapered fiber optic coupler having coupling efficiencies predetermined for specific applications.
Another technique for joining two fibers includes grinding flat surfaces on facing portions of the fibers and joining them by mechanically fixing the surfaces in juxtaposition with a refractive index matching oil or other material ~hat enhances light transmission between the fibers.
lZ6~S82 These and other prior methods of forming fiber optic couplers have the disadvantage of suffering undesirably high loss of optical signal intensity. These prior fabrication techniques generaily fail to facilitate control of the amount of light transmitted by any particular
An optical coupler joins two fibers for transmitting optical energy from one fiber to the other. Optical couplers are used in many applications of optical fiber, including constructing fiber optic inte~eromet~rs, resonators, sensor arrays and data buses.
Among the parameters that are considered in forming an optical coupler are the polarizations of the waves before and after coupling, the fraction of energy to be coupled from one fiber to the other, the insertion loss of the coupler and whether the fibers guide only a single mode or a multiplicity of rnodes.
Several methods have been employed for joining two fibers to form a coupler for transrnitting optical energy from one fiber to the other.
A first technique for joining two fibers results in the biconical tapered fiber optic coupler. The fibers are placed together, twisted and then heated to near the meiting point to fuse them during application of a force to stretch the fibers. The heating and twisting steps in the ~ormation of the biconical tapered fiber optic coupler result in alteration of the molecular arrangements of the materials comprising the joined fibers. In particular, the heating and twisting alters the distributions of impurities used as dopants to control the refractive indices of the core.
The refractive index of a material depends upon its molecular structure; therefors, forming the biconical tapered flber optic coupler, in general, produces localized changes in tho refractive indices of the fibers. These changes in refractive indices are uncontrollable and cause undesirable, uncontrollable reflections and refraction at the interfaces between the fibers. It is therefore difficult to fabricate biconical tapered fiber optic coupler having coupling efficiencies predetermined for specific applications.
Another technique for joining two fibers includes grinding flat surfaces on facing portions of the fibers and joining them by mechanically fixing the surfaces in juxtaposition with a refractive index matching oil or other material ~hat enhances light transmission between the fibers.
lZ6~S82 These and other prior methods of forming fiber optic couplers have the disadvantage of suffering undesirably high loss of optical signal intensity. These prior fabrication techniques generaily fail to facilitate control of the amount of light transmitted by any particular
5 coupler and also fail to perrnit control of the arnounl of light that will be coupled from one fiber to another. Such problems are caused by the inherent intermolecular inhomogeneities and discontinuities that occur - at the interfaces during prior fabrication processes for joining fibers.
Further, prior fabrication techniques are not conducive to producing the 10 : great numbers of optical couplers required in communieations; data processing and sensor applications.
Many applications of fiber optic couplers require very low signal loss in the coupler and also require couplers having critically selected light transmission and coupling characteristics. Large 15 numbers of such couplers are required for practical applications of optical fibers.
Surnmary of the Invention The present invention provides a method and apparatus for forrning fiber optic couplers that avoid the inharent problems of 20 couplers fabricated according to previous techniques. In the present invention bonding of a pair of optical fibers occurs a~ the molecular level In a critical fashion such that the molecular structure of the glass is coherently homogeneous and uniform across th~ bondsd surfaces, thereby preserving the physical characteristics of light transmission 25 across the coupling junction and avoiding unnecessary luss of signal intensity.
The present invention permits precise control of the amount of light coupl~d between fibars and is suitable for mass production of optical couplers having precisely sel~cted coupling and transmission 30 characteristics.
The present invention provides a fi~er optic coupler for coupling an optical wave between a pair of optical fibers each having a central core surrounded by a cladding, th~ cores and claddihgs having characteristic refractive indices, compr;sing a first planar surface 35 formed on a first optical fiber by removing at least a portion of the ~Z~:i458~
cladding therefrom and a second planar surface formed on a second optical fiber by removing at least a portion of the cladding therefrom, the first and second planar surfaces being juxtaposed to form an interaction region wherein light is to propagate between the fibers. A
coherent molecular bond is formed between the first and second planar surfaces without altering the core and oladding refractive indices across the joined surfaces.
In on0 embodiment of the inv0ntion, ths planar surfaces are formed by removing porRons of the cladding from curved lengths of the optical fibers su~h that evanescent field coupling ~t the interaction region between optical waves guided by a first one of the fibers and the other fiber couples energy between the fibers.
In another embodiment of the invention the planar surfaces are formed by removing portions of the cladding and a portions of the core 1~ from curved lengths of the optical fibers such tha~ juxtaposing the fiber cores forms an intercepting core coupler.
The present invention inclwdes a fiber optic coupler for coupling an optical wave between a pair of optical fibers each having a central core surrounded by a cladding, the cores and claddings having characteristic refractive indices. The coupler according to the invention is formed by the process comprisin~ forming a first planar surface ~ormed on a first optical fiber by removing at teast a portion of the cladding therefrom and forming a second planar surface on a second optical fiber by rernoving at least a portion of the cladding ther~from, the first and second planar sur~aces being juxtaposed to form an interac~ion region wherein light propagates between the fibers; and formin~ a coherent molecular intermolecular bond formed between the first and second planar surfaces without altering the local core and cladding refractive indices.
The coherent molecular bond that joins the fibers to form the coupler may be formed by the process oomprising aligning the planar surfaces relative to one another to provide a predetermined coup~ing efficiency; and applying a controlled amount of energy to the planar surfaces to cause them to bond together, forming a homo~eneous, 3~ coherent intermolecularly bonded s~ructure.
~264S8z The method of the present invention for forming a fiber optic coupler for coupling an optical wave between a pair of optical fibers each having a central core surrounded by a cladding, th~ cores and claddings having characteristic refractive indicas, comprises the steps of: forming a first planar surface formed on a first optical fiber by removing at least a portion of the cladding therefrom; forming a second planar surface formed on a second optical fiber by removing at least a portion of the cladding therefrom, the first and second planar surfaces being juxtaposed to form an interaction region wherein light propagates between the fibers; and forming a coherent molecular bond between the first and second planar surfaces without altering the local core and cladding refractive indices by causing intermolecular inhomogeneities and discontinuities across the joined surfaces.
The step of forming the coherent molecular bond may comprise ihe steps of aligning the planar surfaces relative to one another to provide a predetermined coupling efficiency; and applying a controlled amount of energy to the planar surfaces to cause them to bond together, thereby forming a homogeneous, coherent interrnolecularly bonded structure.
The step of applying energy to the planar surfaces may include focusing a beam of coherent ligh~ thereon. The step of forrning a coherent molecular bond may include heating the fibers to a transition temperature belouv the melting temperature of the fibers.
Br~f l:~escription Qf the Drawings Figure 1 is a cross sectional view of a fiber optic evanescent field coupler formed according to the present invention;
Figure 2 is a cross sectional view of the fiber optic evanescent field coupler taken along lina 2-2 of Figura 1;
Figure 3 is a plan view showing an oval surface on a portion of an optical fiber included in the fiber optic evanescent field coupler of Figures 1 and 2;
Figure 4 is a cross sectional view of an intercepting core coupler formed according to the present invention;
Figure 5 is a cross sectional view taken along line 5-~ of Figure 4;
~l2~458~
Figure 6 is a plan view showing core and cladding planar `~ surfaces on a portion of an optical fiber included in the fiber optic intercep~ing core coupler of Figures 4 and 5;
Figure 7 is a plan view illustrates a system for joining two optical fibers to form either an evanescent field ~iber optic coupler as shown in Figures 1-3 or an intercepting fieW coupler as shown in Figures 4-6;
Figure 8 is an cross sectional view showing alignment of a pair of opticai fibers with a jig and application of ener~y thereto for bonding 10 the ~ibers together to form a fiber optic coupler;
Figure 9 is a plan view of the apparatus of Figure 8; and Figure 10 illustrates formation of an optically fiat surface on an optical fiber to be used in forming a fiber optic coupler.
Desçription of the Prçferred Emb~diment 1~ Evanescent Field Coupler As illustrated in Figure 1, a coupler 20 formed according to the method of the invention includes a pair of optical fibers 22 and 24 mounted together. The fiber 22 has a core 26 and a cladding 28, and the fiber 24 has a cor~ 30 and a cladding 32. As explained 20 subsequently, an oval shaped optically flat surface 34 is formed in the cladding 28 of the fiber 22. Similarly, an oval shaped optically flat surface 36 is formed in the cladding 32 of th0 fiber 22.
The oval surfaces 34 and 36 are juxtaposed. in facing relationship to form an interaction region 42 wherein the evanescent 25 fields of light propagated by each of the fibers 22 and 24 interact with the other fiber. The quality and quantity of light crossing or interacting across the juxtaposed surfaces 34 and 36 are affected by discontinuities, inhomogeneities and other local defects caused in the interaction region by the manner of joining and the type of bond 30 produced between the surfaces 34 and 3B. The essence af the present invention is a coupler and method of fabrication thereof that comprises a bonded surface that is molccularly coherent, homogeneous and continuous across and around the joined sur~aces 34 and 36 ~f the fibers 22 and 24. Accordingly, local irregularities in the refractive indices are avoided, with the resultant interaction region 46 of the ~2~i4~i82 joined region having well behaved refractive indices throughout as expected for a rnolecularly consistent material.
The amount of fiber optic material removed increases gradually from zero at the edges of the oval-shaped planar su~aces 34 and 36 to 5 a maximum amount at the centers thereof. The tapered rernoval of fiber optic material snables the fibers 22 and 24 to eonverge and diverge gradually, which is advantageous for avoiding backward reflection and excessive loss of light energy at the interaction region 42. The gradual curvature of the fibers 22 and 24 prevents sharp bends or other abrupt 10 changes in direction of the fibers 22 and 24 to avoid power loss through mode perturbation.
Light is transferred between the fibers 22 and 24 by evanescent field coupling at the interaction region 42. The core 26 has a refractive index that is greater than that of the cladding 28, and the 1~ diameter of the core 26 is such that light propagating within the core 26 internally reflects at the core-cladding interface. Most of the optical energy guided by the optical fiber 22 is confined to its core 26.
However, solution of the wave equations for the fiber 22 and applying the well-known boundary conditions shows that th~ energy distribution, 20 although primarily in the core 26, includes a portion that extends into the cladding and decays exponentially as the radius from the center of the fiber increases. The exponentially decaying portion of the energy distribution within the fiber 22 is generally called the evanescent field.
If the evanescent field of the optical energy initially propagated by the 2~ fiber 22 extends a sufficient distance into the fiber 24, energy will couple from the fiber 22 into the fiber 24.
It has been found that to ensure proper evanescent field coupling, the amount of material removed from the fibers 22 and 24 must be carefully controlled so that th~ spacing between the cores of 30 the fibers 22 and 24 is within a predetermined critical zone. The evanescent field extends a short distance into the cladding and decreases rapidly in magnitude with distance outside the fiber core.
Thus, sufficient fiber optic material should be removed to permit overlap between the evanescent fields of waves propaga~ed by the ~wo fibers 35 22 and 24. If too little material is removed, the cores will not be ~aZ6 sufficiently close to permit the evanescent f;elds to cause the desired interaction of the guided waves; and therefore, insufficient coupling will result.
Conversely, removal of too much material alters the 5 propagation characteristies of the fibers, resulting in loss of light energy from the fibers due to mode perturbation. However, when the spacing between the cores of the flbers 22 and 24 is within the critical zone, each fiber 22 and 24 receives a significant portion of the evanescent field energy ~rom the other to achieve good coupling without significant 1C energy loss. The critical zone includes the region in which the evanescent fields of the fibers 22 and 24 overlap sufficiently to provide - good evanescen~ field coupling with each core being within the evanescent field of light guided by the o~her core. It is believed that for weakly guided modes, such as the HE11 mode guided by single mode 15 fibers, mode perturbation occurs when the fiber core is exposed.
Therefore, the critical zone is the core spacing that causes the evanescent ~ields to overlap sufficiently to cause coupling without causing substantial mode perturbation induced power loss.
The extent of the critical zone for a particular coupler depends 20 upon a number of factors, such as the physical parameters of th0 fibers and the geometry of the coupler. The critical zono also is affected by the type of bond formed betwe0n the joined fibers. The critical zone rnay be quit0 narrow for a single mode fiber having a step index profile.
The center-to-center spacing of the fibers 22 and 24 is typically less that 25 two to three core diameters.
The fibers 22 and 24 preferably have substantially identical core and cladding diameters, the same raclius of curvature at the interaction zone 42, ~nd the same amount of fiber optic material removed therefrom to form the interaction region 42. The fibers 22 and 30 24 are symmetrical through the interaction region 42 in the planes of the surfaces 34 and 36, respectively, so that the facing planar oval surfaces of the fibers 22 and 24 are coextensive when they are superimposed. The two fibers 22 and 24 therefore have identical propagation ~haracteristics at the interaction region, thereby avoiding 3~ reduction in coupling that is associated with dissimilar propagation ~Z6~5~3Z
characteristics. Each of the optical fibers 22 and 24 has a propagation constant that determines the parameters, such as wavelength, reflection at interfaces and attenuation of waves propagating therein. It is well-known that energy couples between media having substantially identical propagation constants more easily than between media having different propagation constants. There~ore, in forming the coupler 20, it is desirable to minimize variations of the propagation constant a~ the interaction region 42.
The coupler 20 of Figures 1 and 4 includes four ports labeled 20A, 20B, 2ûC and 20D. Ports 20A and 20B, which are on the left and right sides, respectively, of the coupler 20 correspond to the fiber 22;
The ports 20C and 20D, which are on the left and right sides, respectively, of the coupler ~û correspond to the fiber 24. For purposes of explanation it is assumed that an optical signal input is applied to pcrt 2ûA through the fiber 22. The signal passes through the coupler 20 and is output at sither one or both of ports 20B or 20C depending upon the amuunt of coupling between the fibers 22 and 24. The "coupling constant" is defined as the ratio of the coupled power to the total output power.
In the above example, the coupling constant is the ratio of the powsr output at port 20D divided by the sum of the power output at the ports 20~ and 20D. This ratio is sometimes called the "couplin~
efficiencyN, which is typically expressed as a percent. Thsrefor0, when the term "coupling constant~ is used herein, it should be understood that the corresponding coupling efficiency is equal to the coupling constant times 100.
The coupler 20 may be tuned to adjust the coupling constant to any desired value between zero and 1.0 by offsetting the confronting surfaces 34 and 36 to control the dimensions of the region of overlap of the evanescent fields of waves guided by the fibers 22 and 24. Tuning may be accompiished by sliding the substrates 34 and 36 laterally or longitudinally relative to one another during assembly of the coupler 20.
The coupler 20 is highly directional with substantially all of the power applied at one side thereof being output at the ports on the other side. Substantially all of the light applied as an input to sither ports 20A or 20C is delivered to ports 20B and 20D without appreciable contra-directional coupling. The directional charactaristic is symme~rical in that light applied to either ports 20B or 20D is delivsred to ports 20A
and 20B. The coupler 20 is essentially non-discriminatory with respect to polarizations and preserves the polarization of light input thereto.
Light ~ha~ is cross-coupled from one of the fibers 22 and 24 to the other undergoes a phase shift of 1l/2, but light that passes straight through the coupler 20 wlthout being cross-coupled is not shifted in phase. For example, if the coupler 20 has a-coupling constant of 0.5, and an optical signal is input to port 20A, then the outputs at ports 20B
and 20D will be of equal magnitude; but the QUtpUt at port 20D will be shifted in phase by ~/2 relative to the output at port 2ûB.
The coupler 20 is a low loss device, having typical insertion 1~ losses of about 0.1% to 0.2%. The term "insertion loss" as used herein refers to the real scattering losses of light energy passing through the coupler 20. For example, if light energy is input to port 20~; and the light energy output at ports 20B and 20D totals 97% of the input energy, the insertion loss is 3%. The term "coupler transmission~ is defined as one minus the insertion loss and is typically expressed an a decimal fraction.
Intercepting Core Coupler Referring to Figure 4, an intercepting core fiber optic coupler 48 formed according to tho methods of the present inv~ntion includes a pair of optical fibers 50 and 52.
The fiber 50 is polished to remove sufficient fiber optic material to expose a core portion 62 and a cladding portion 64 on the fiber 50.
Similarly, the fiber 52 is polished to remove sufficient fiber optic material to expose a cors portion 66 and a ciadding portion 68 on the fiber 52. The fibers 50 and 52 preferably have identical diameters, and the cora and cladding portions 62 and 64 have dimensions substantially identical to the core and cladding portions 66 and 68, respectively. The dimensions of the core portion 62 the cladding portion 64 are determined by the diameters of the cors and cladding of the fiber 50 and the depth to which fiber op~ic material is removed therefrom. Similarly, the dimensions of the core portion 66 the cladding portion 68 are determined by the diameters of the core and cladding of the fiber 52 and the depth to which fiber optic material is removed therefrom.
The exposed core portions 62 and 66 and the ~ladding portions 64 and 68 are juxtaposed in facing relationship. The ~ibers ~0 and 57 are then bonded together as described subsequently herein.
The coupling efficiency of the ceupler 48 is determined primarily by the depths to which material is removed from the cores of the fibers ~0 and 52 and the relative positions of the flat regions thereon when the fibers are bonded together.
If the fibers 50 and 52 have different diameters, then they vvill ordinariiy be polished to different depths so tha$ the exposed core and cladding portions, respectively, will have essentially the same dimensions. If the fiber 50 has a smaller core diameter than the fiber 52, the coupling efficiency of the coupler 4B depends on which fiber carries the optical wave to the region where the cores intercept. The coupling efficiency will in general be higher when the light is incident upon the coupler 48 from within the fiber having the smaller diameter.
Method of Fabricatien The ensuing description of the processes for fabricating th~
coupiers 20 and 48 begins with a description of the steps used for fabricating the evanescent field coupler ~0. Many identical steps are involved in fabricating the evanescent field coupler 20 and the intercepting core coupler 48. The process for fabricating the intercepting core coupler 48 will point out the similarities and differences between the fabrication methods.
The first step in formation of the coupler 20 is to remove any jacketing material that may bs ~n a length of a few centimeters of the fibers to provida access to the bare cladding thereof. Referring to Figures 7 and 8, the fibers 22 and 24 are then attached to conv~xly curved surfaces of a pair of substrates 70 and 72, respectively, by the use of any suitable adhesivc. The substrates 70 and 72 may be made of any generally rigid material, such as glass, metal or plastic. The radii of curvature of the substrates 70 and 72 preferably are identical and are ~;~6~ ;J
sufficiently large to preclude the risk of fracturing the fibers as they are bent to conform to the curvature.
The central portions of the fib0rs 22 and 24 rnay then be lapped using conventional lapping methods to a predetermined depth to remove cladding material thersfrom and form the planar suriaces 34 and 36, respectively. The planar surfaces 34 and 36 should be sufficiently flat that they $end to adhere to one another when they are placed together with no adhesive or index rnatching oil therebetween.
A lapping technique that has been found to b0 advantageous 10 in forming the planar surfaces 34 and 36 to be optically flat is illustrated in Figure 10. The fiber 22 is shown mounted to the substrate 70, which is connected to a retainer 73 by any suitable means, such as clamping or gluing. The retainer 73 is supported on a shaft 75 that extends from a motor 77, which controls the elevation of tha shaft 77 and retainer 75 1~ relative to an optically flat lapping surface 79. Tha lapping begins with the central portion of the convexly curved fiber 22 being tangent to the lapping surface 79. As the lapping procaeds, the motor 77 lowers the shaft 75, the retainer 73 and the substrate 70 with the fiber 22 attached thereto such that the planar surface 34 is formed by lapping radially 20 inward from the point of initial contact between the fiber 22 and the lapping surface 79.
A preferred rnethod for determining the depth to which the fiber is lapped is to apply an optical signal to one end thereof fronn a laser 81 and to monitor the optical output at the other end with a photodetector 2~ 83. A lapping slurry having a refractive index near that of the fiber 22 is maintained on the lapping surface 79 during the lapping process. As the lapping proceeds, light couples from the fiber 22 into the lapping slurry, thereby reducing the optical throughput of the fiber 22. Tha optical throughput may be correlatsd to the lapping depth. In general, 30 the relation between the opticaJ throughput and lapping depth depends upon the specific type of fiber being lapped. Therefore, it is necessary to perform a series of measurements of the lapping depth as a function of optical throughput to produce a calibration curve for the par~icular fiber being lapped and the lapping slurry used ~herewith.
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As explained previously, care must be taken to avoid removal of too much cladding material from the fibers used to form the evanescent field coupier 20. Using ordinary single mods flber, forming the coupler 20 to have a coupling efficiency of one to two percent 5 requires removal nf about ten percent of the core depth at the center of the oval surfaces.
After the fibers 22 and 24 are mounted on the corresponding substrates 70 and 72 and the oval surfaces are formed using, for example, the rnethods described above, the planar surfaces 34 and 36 10 are placed in juxtaposition as shown in Figures 7-9. A preferred method for holding the surfaces 34 and 36 in the desired positions is to place the substrates 70 and 72 are placed in a jig 82 as shown in Figure 9. The jig- 82 includes a pair of retainers 84 and 86 for holding the substratÆs 70 and 72, respectively, so that they are movable with 1~ respect to one another. The substra~es 70 and 72 are placed in desired positions relative to one another and then the fibers 22 and 24 are bonded together. Ordinarily, the fibers 22 and 24 will be position0d t maximize the coupling of optical signals therebetween.
The coupler 20 may be formed to have a desired coupling 2Q constant. One preferred method for assuring achievernent of a desired coupling constant includes the step of inputting an optical signal frorn a laser 90 into an end 92 of the fiber 22. The intensities of the optical signals emanating from the fibers 22 and 24 after the inpu~ beam has impinged upon the interaction re~ion 42 are monitored using suitable 25 photodetectors 94 and 96, respectively, while the substrates are manipulated to achieve a desired coupling efficieney. The amount of coupling may be varied by moving the substrates 28 in the jig 72 to adjust the amount of overlap of the planar surfacss 30 and 32. The coupling efficiency is Tl = 1 - It/i lC(lt + ~C)-1 ~
where 1l is the coupling efficiency, Ij is the light intensity input to fiber 22, It iS the light transmitted through fiber 22 beyond the interaction region 42 and Ic is the light intensity coupled from fiber 22 to fiber 24.
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After the fibers 22 and 24 have been positioned to provide the desired coupling constant, energy is applied to the interface oF the planar surFaces 30 and 32. As shown in Figure 8, the energy source may be a laser 98. The laser ~8 is p~ferably a CO2 laser, and it should produce an sutput beam that will heat the fibers 22 and 24 to a temperature near the glass transition temperature. The energy source may also be an ultrasonic wave genera~or, an induction heating source or other suitable device for providing the desired amount of heat to the fibers 22 and 24. As shown in Figures 8 and 9, a forc~ F may be applied to compress the fibers 22 and 24 together during the bonding process. Generally it has been found that a compressive force of about a pound facilitates formation of the coherent molecular bond The transition temperatura is below the melting point of the glass from which ~he fibers 22 and 24 are formed. Ths transition temperature depends upon the materials comprising the fibers 22 and 24. Most optical fiber is formed from silicon dioxide with a dopant such as germanium dioxide or boron added thareto to control the refractive index. Such fibers typically have transition temperatures in thc range of 1100 C to 1200 C. The transition temperature should be determined ~o ~xperimentally for the fibers to be joined, and the energy output from the laser 98 should be controlled to assure that the temperature in the bonded region does not excsed the transition temperature. The transition temperaturc of an optical fiber is attained when the fiber begins to soften as the temperature increases.
Applying the outpwt of the laser 98 over the juncture of the surfaces 30 and 32 fuses the fibers 22 and 24 together. It has been found that the above described method forms a junction of the surfaces 30 and 32 that results in a coherent molecular bonded r2gion having the same physical structure and the samc optical characteristics as the bulk material comprising ~ibers 22 and 24.
The processes of forming and joining optically flat surfaces on fiber 22 an~l 24 described herein provide a fiber optic coupler having a bonded surfaoe that is molecularly coherent, homogeneous and continuous across and around ths joined surfaces 34 and 36 of the 3~ fibers 22 and 24. Accordingly, local irregwiarities in the refractive ~z~
indices are avoided, with the resultant interaction region 46 of the joined region having well behaved refractive inclices throughout as expected for a molecularly consistent material. The step of coupling light from the fibers 22 and 24 while they are lapped to form the optically flat surfaces 34 and 36, respectively, permits sufficient control of the lapping depth ~abrication to form the coupler 20 to have a predetermined coupling efficiency.
The primary difference between the steps for fabricating the evanescent field coupler 20 and the intercepting cors coupler 48 is the - depth to which the fibers 22, 24, 50 and 52 are lapped. The amount of coupling depends upon the length of the interaction zone, which is a function of the lapping depth and the radius of curvature of the flber being lapped. It has been found that in general a 3 dB intercepting core coupler should have the fibers lapped to remove 5û% of the core 15 to provide full modal mixing. It is well known from electromagnetic theory that the energy distributions of tha normal modes varies with the radial distance from the center of an optical fiber. The energy in the lower orcler modes tends to be primarily in the ~entral region of the core, whereas the higher order modes tend to have more snergy near 20 the core/cladding interface. Since most of the energy in a multimode fiher is in the lower order modes, good coupling is facilitated by having the central regions of the cores in contact.
Couplers formed according to the absve described method have been cut into sections and examined with high power 25 microscopes and a mireau interferometer. These instruments show that the bond interface has no distortion of the molecular arrangements of the cores or the claddings of the fibers and that the rnolecular structure of the inter~ace is identical to that of the fibers.
, ,
Further, prior fabrication techniques are not conducive to producing the 10 : great numbers of optical couplers required in communieations; data processing and sensor applications.
Many applications of fiber optic couplers require very low signal loss in the coupler and also require couplers having critically selected light transmission and coupling characteristics. Large 15 numbers of such couplers are required for practical applications of optical fibers.
Surnmary of the Invention The present invention provides a method and apparatus for forrning fiber optic couplers that avoid the inharent problems of 20 couplers fabricated according to previous techniques. In the present invention bonding of a pair of optical fibers occurs a~ the molecular level In a critical fashion such that the molecular structure of the glass is coherently homogeneous and uniform across th~ bondsd surfaces, thereby preserving the physical characteristics of light transmission 25 across the coupling junction and avoiding unnecessary luss of signal intensity.
The present invention permits precise control of the amount of light coupl~d between fibars and is suitable for mass production of optical couplers having precisely sel~cted coupling and transmission 30 characteristics.
The present invention provides a fi~er optic coupler for coupling an optical wave between a pair of optical fibers each having a central core surrounded by a cladding, th~ cores and claddihgs having characteristic refractive indices, compr;sing a first planar surface 35 formed on a first optical fiber by removing at least a portion of the ~Z~:i458~
cladding therefrom and a second planar surface formed on a second optical fiber by removing at least a portion of the cladding therefrom, the first and second planar surfaces being juxtaposed to form an interaction region wherein light is to propagate between the fibers. A
coherent molecular bond is formed between the first and second planar surfaces without altering the core and oladding refractive indices across the joined surfaces.
In on0 embodiment of the inv0ntion, ths planar surfaces are formed by removing porRons of the cladding from curved lengths of the optical fibers su~h that evanescent field coupling ~t the interaction region between optical waves guided by a first one of the fibers and the other fiber couples energy between the fibers.
In another embodiment of the invention the planar surfaces are formed by removing portions of the cladding and a portions of the core 1~ from curved lengths of the optical fibers such tha~ juxtaposing the fiber cores forms an intercepting core coupler.
The present invention inclwdes a fiber optic coupler for coupling an optical wave between a pair of optical fibers each having a central core surrounded by a cladding, the cores and claddings having characteristic refractive indices. The coupler according to the invention is formed by the process comprisin~ forming a first planar surface ~ormed on a first optical fiber by removing at teast a portion of the cladding therefrom and forming a second planar surface on a second optical fiber by rernoving at least a portion of the cladding ther~from, the first and second planar sur~aces being juxtaposed to form an interac~ion region wherein light propagates between the fibers; and formin~ a coherent molecular intermolecular bond formed between the first and second planar surfaces without altering the local core and cladding refractive indices.
The coherent molecular bond that joins the fibers to form the coupler may be formed by the process oomprising aligning the planar surfaces relative to one another to provide a predetermined coup~ing efficiency; and applying a controlled amount of energy to the planar surfaces to cause them to bond together, forming a homo~eneous, 3~ coherent intermolecularly bonded s~ructure.
~264S8z The method of the present invention for forming a fiber optic coupler for coupling an optical wave between a pair of optical fibers each having a central core surrounded by a cladding, th~ cores and claddings having characteristic refractive indicas, comprises the steps of: forming a first planar surface formed on a first optical fiber by removing at least a portion of the cladding therefrom; forming a second planar surface formed on a second optical fiber by removing at least a portion of the cladding therefrom, the first and second planar surfaces being juxtaposed to form an interaction region wherein light propagates between the fibers; and forming a coherent molecular bond between the first and second planar surfaces without altering the local core and cladding refractive indices by causing intermolecular inhomogeneities and discontinuities across the joined surfaces.
The step of forming the coherent molecular bond may comprise ihe steps of aligning the planar surfaces relative to one another to provide a predetermined coupling efficiency; and applying a controlled amount of energy to the planar surfaces to cause them to bond together, thereby forming a homogeneous, coherent interrnolecularly bonded structure.
The step of applying energy to the planar surfaces may include focusing a beam of coherent ligh~ thereon. The step of forrning a coherent molecular bond may include heating the fibers to a transition temperature belouv the melting temperature of the fibers.
Br~f l:~escription Qf the Drawings Figure 1 is a cross sectional view of a fiber optic evanescent field coupler formed according to the present invention;
Figure 2 is a cross sectional view of the fiber optic evanescent field coupler taken along lina 2-2 of Figura 1;
Figure 3 is a plan view showing an oval surface on a portion of an optical fiber included in the fiber optic evanescent field coupler of Figures 1 and 2;
Figure 4 is a cross sectional view of an intercepting core coupler formed according to the present invention;
Figure 5 is a cross sectional view taken along line 5-~ of Figure 4;
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Figure 6 is a plan view showing core and cladding planar `~ surfaces on a portion of an optical fiber included in the fiber optic intercep~ing core coupler of Figures 4 and 5;
Figure 7 is a plan view illustrates a system for joining two optical fibers to form either an evanescent field ~iber optic coupler as shown in Figures 1-3 or an intercepting fieW coupler as shown in Figures 4-6;
Figure 8 is an cross sectional view showing alignment of a pair of opticai fibers with a jig and application of ener~y thereto for bonding 10 the ~ibers together to form a fiber optic coupler;
Figure 9 is a plan view of the apparatus of Figure 8; and Figure 10 illustrates formation of an optically fiat surface on an optical fiber to be used in forming a fiber optic coupler.
Desçription of the Prçferred Emb~diment 1~ Evanescent Field Coupler As illustrated in Figure 1, a coupler 20 formed according to the method of the invention includes a pair of optical fibers 22 and 24 mounted together. The fiber 22 has a core 26 and a cladding 28, and the fiber 24 has a cor~ 30 and a cladding 32. As explained 20 subsequently, an oval shaped optically flat surface 34 is formed in the cladding 28 of the fiber 22. Similarly, an oval shaped optically flat surface 36 is formed in the cladding 32 of th0 fiber 22.
The oval surfaces 34 and 36 are juxtaposed. in facing relationship to form an interaction region 42 wherein the evanescent 25 fields of light propagated by each of the fibers 22 and 24 interact with the other fiber. The quality and quantity of light crossing or interacting across the juxtaposed surfaces 34 and 36 are affected by discontinuities, inhomogeneities and other local defects caused in the interaction region by the manner of joining and the type of bond 30 produced between the surfaces 34 and 3B. The essence af the present invention is a coupler and method of fabrication thereof that comprises a bonded surface that is molccularly coherent, homogeneous and continuous across and around the joined sur~aces 34 and 36 ~f the fibers 22 and 24. Accordingly, local irregularities in the refractive indices are avoided, with the resultant interaction region 46 of the ~2~i4~i82 joined region having well behaved refractive indices throughout as expected for a rnolecularly consistent material.
The amount of fiber optic material removed increases gradually from zero at the edges of the oval-shaped planar su~aces 34 and 36 to 5 a maximum amount at the centers thereof. The tapered rernoval of fiber optic material snables the fibers 22 and 24 to eonverge and diverge gradually, which is advantageous for avoiding backward reflection and excessive loss of light energy at the interaction region 42. The gradual curvature of the fibers 22 and 24 prevents sharp bends or other abrupt 10 changes in direction of the fibers 22 and 24 to avoid power loss through mode perturbation.
Light is transferred between the fibers 22 and 24 by evanescent field coupling at the interaction region 42. The core 26 has a refractive index that is greater than that of the cladding 28, and the 1~ diameter of the core 26 is such that light propagating within the core 26 internally reflects at the core-cladding interface. Most of the optical energy guided by the optical fiber 22 is confined to its core 26.
However, solution of the wave equations for the fiber 22 and applying the well-known boundary conditions shows that th~ energy distribution, 20 although primarily in the core 26, includes a portion that extends into the cladding and decays exponentially as the radius from the center of the fiber increases. The exponentially decaying portion of the energy distribution within the fiber 22 is generally called the evanescent field.
If the evanescent field of the optical energy initially propagated by the 2~ fiber 22 extends a sufficient distance into the fiber 24, energy will couple from the fiber 22 into the fiber 24.
It has been found that to ensure proper evanescent field coupling, the amount of material removed from the fibers 22 and 24 must be carefully controlled so that th~ spacing between the cores of 30 the fibers 22 and 24 is within a predetermined critical zone. The evanescent field extends a short distance into the cladding and decreases rapidly in magnitude with distance outside the fiber core.
Thus, sufficient fiber optic material should be removed to permit overlap between the evanescent fields of waves propaga~ed by the ~wo fibers 35 22 and 24. If too little material is removed, the cores will not be ~aZ6 sufficiently close to permit the evanescent f;elds to cause the desired interaction of the guided waves; and therefore, insufficient coupling will result.
Conversely, removal of too much material alters the 5 propagation characteristies of the fibers, resulting in loss of light energy from the fibers due to mode perturbation. However, when the spacing between the cores of the flbers 22 and 24 is within the critical zone, each fiber 22 and 24 receives a significant portion of the evanescent field energy ~rom the other to achieve good coupling without significant 1C energy loss. The critical zone includes the region in which the evanescent fields of the fibers 22 and 24 overlap sufficiently to provide - good evanescen~ field coupling with each core being within the evanescent field of light guided by the o~her core. It is believed that for weakly guided modes, such as the HE11 mode guided by single mode 15 fibers, mode perturbation occurs when the fiber core is exposed.
Therefore, the critical zone is the core spacing that causes the evanescent ~ields to overlap sufficiently to cause coupling without causing substantial mode perturbation induced power loss.
The extent of the critical zone for a particular coupler depends 20 upon a number of factors, such as the physical parameters of th0 fibers and the geometry of the coupler. The critical zono also is affected by the type of bond formed betwe0n the joined fibers. The critical zone rnay be quit0 narrow for a single mode fiber having a step index profile.
The center-to-center spacing of the fibers 22 and 24 is typically less that 25 two to three core diameters.
The fibers 22 and 24 preferably have substantially identical core and cladding diameters, the same raclius of curvature at the interaction zone 42, ~nd the same amount of fiber optic material removed therefrom to form the interaction region 42. The fibers 22 and 30 24 are symmetrical through the interaction region 42 in the planes of the surfaces 34 and 36, respectively, so that the facing planar oval surfaces of the fibers 22 and 24 are coextensive when they are superimposed. The two fibers 22 and 24 therefore have identical propagation ~haracteristics at the interaction region, thereby avoiding 3~ reduction in coupling that is associated with dissimilar propagation ~Z6~5~3Z
characteristics. Each of the optical fibers 22 and 24 has a propagation constant that determines the parameters, such as wavelength, reflection at interfaces and attenuation of waves propagating therein. It is well-known that energy couples between media having substantially identical propagation constants more easily than between media having different propagation constants. There~ore, in forming the coupler 20, it is desirable to minimize variations of the propagation constant a~ the interaction region 42.
The coupler 20 of Figures 1 and 4 includes four ports labeled 20A, 20B, 2ûC and 20D. Ports 20A and 20B, which are on the left and right sides, respectively, of the coupler 20 correspond to the fiber 22;
The ports 20C and 20D, which are on the left and right sides, respectively, of the coupler ~û correspond to the fiber 24. For purposes of explanation it is assumed that an optical signal input is applied to pcrt 2ûA through the fiber 22. The signal passes through the coupler 20 and is output at sither one or both of ports 20B or 20C depending upon the amuunt of coupling between the fibers 22 and 24. The "coupling constant" is defined as the ratio of the coupled power to the total output power.
In the above example, the coupling constant is the ratio of the powsr output at port 20D divided by the sum of the power output at the ports 20~ and 20D. This ratio is sometimes called the "couplin~
efficiencyN, which is typically expressed as a percent. Thsrefor0, when the term "coupling constant~ is used herein, it should be understood that the corresponding coupling efficiency is equal to the coupling constant times 100.
The coupler 20 may be tuned to adjust the coupling constant to any desired value between zero and 1.0 by offsetting the confronting surfaces 34 and 36 to control the dimensions of the region of overlap of the evanescent fields of waves guided by the fibers 22 and 24. Tuning may be accompiished by sliding the substrates 34 and 36 laterally or longitudinally relative to one another during assembly of the coupler 20.
The coupler 20 is highly directional with substantially all of the power applied at one side thereof being output at the ports on the other side. Substantially all of the light applied as an input to sither ports 20A or 20C is delivered to ports 20B and 20D without appreciable contra-directional coupling. The directional charactaristic is symme~rical in that light applied to either ports 20B or 20D is delivsred to ports 20A
and 20B. The coupler 20 is essentially non-discriminatory with respect to polarizations and preserves the polarization of light input thereto.
Light ~ha~ is cross-coupled from one of the fibers 22 and 24 to the other undergoes a phase shift of 1l/2, but light that passes straight through the coupler 20 wlthout being cross-coupled is not shifted in phase. For example, if the coupler 20 has a-coupling constant of 0.5, and an optical signal is input to port 20A, then the outputs at ports 20B
and 20D will be of equal magnitude; but the QUtpUt at port 20D will be shifted in phase by ~/2 relative to the output at port 2ûB.
The coupler 20 is a low loss device, having typical insertion 1~ losses of about 0.1% to 0.2%. The term "insertion loss" as used herein refers to the real scattering losses of light energy passing through the coupler 20. For example, if light energy is input to port 20~; and the light energy output at ports 20B and 20D totals 97% of the input energy, the insertion loss is 3%. The term "coupler transmission~ is defined as one minus the insertion loss and is typically expressed an a decimal fraction.
Intercepting Core Coupler Referring to Figure 4, an intercepting core fiber optic coupler 48 formed according to tho methods of the present inv~ntion includes a pair of optical fibers 50 and 52.
The fiber 50 is polished to remove sufficient fiber optic material to expose a core portion 62 and a cladding portion 64 on the fiber 50.
Similarly, the fiber 52 is polished to remove sufficient fiber optic material to expose a cors portion 66 and a ciadding portion 68 on the fiber 52. The fibers 50 and 52 preferably have identical diameters, and the cora and cladding portions 62 and 64 have dimensions substantially identical to the core and cladding portions 66 and 68, respectively. The dimensions of the core portion 62 the cladding portion 64 are determined by the diameters of the cors and cladding of the fiber 50 and the depth to which fiber op~ic material is removed therefrom. Similarly, the dimensions of the core portion 66 the cladding portion 68 are determined by the diameters of the core and cladding of the fiber 52 and the depth to which fiber optic material is removed therefrom.
The exposed core portions 62 and 66 and the ~ladding portions 64 and 68 are juxtaposed in facing relationship. The ~ibers ~0 and 57 are then bonded together as described subsequently herein.
The coupling efficiency of the ceupler 48 is determined primarily by the depths to which material is removed from the cores of the fibers ~0 and 52 and the relative positions of the flat regions thereon when the fibers are bonded together.
If the fibers 50 and 52 have different diameters, then they vvill ordinariiy be polished to different depths so tha$ the exposed core and cladding portions, respectively, will have essentially the same dimensions. If the fiber 50 has a smaller core diameter than the fiber 52, the coupling efficiency of the coupler 4B depends on which fiber carries the optical wave to the region where the cores intercept. The coupling efficiency will in general be higher when the light is incident upon the coupler 48 from within the fiber having the smaller diameter.
Method of Fabricatien The ensuing description of the processes for fabricating th~
coupiers 20 and 48 begins with a description of the steps used for fabricating the evanescent field coupler ~0. Many identical steps are involved in fabricating the evanescent field coupler 20 and the intercepting core coupler 48. The process for fabricating the intercepting core coupler 48 will point out the similarities and differences between the fabrication methods.
The first step in formation of the coupler 20 is to remove any jacketing material that may bs ~n a length of a few centimeters of the fibers to provida access to the bare cladding thereof. Referring to Figures 7 and 8, the fibers 22 and 24 are then attached to conv~xly curved surfaces of a pair of substrates 70 and 72, respectively, by the use of any suitable adhesivc. The substrates 70 and 72 may be made of any generally rigid material, such as glass, metal or plastic. The radii of curvature of the substrates 70 and 72 preferably are identical and are ~;~6~ ;J
sufficiently large to preclude the risk of fracturing the fibers as they are bent to conform to the curvature.
The central portions of the fib0rs 22 and 24 rnay then be lapped using conventional lapping methods to a predetermined depth to remove cladding material thersfrom and form the planar suriaces 34 and 36, respectively. The planar surfaces 34 and 36 should be sufficiently flat that they $end to adhere to one another when they are placed together with no adhesive or index rnatching oil therebetween.
A lapping technique that has been found to b0 advantageous 10 in forming the planar surfaces 34 and 36 to be optically flat is illustrated in Figure 10. The fiber 22 is shown mounted to the substrate 70, which is connected to a retainer 73 by any suitable means, such as clamping or gluing. The retainer 73 is supported on a shaft 75 that extends from a motor 77, which controls the elevation of tha shaft 77 and retainer 75 1~ relative to an optically flat lapping surface 79. Tha lapping begins with the central portion of the convexly curved fiber 22 being tangent to the lapping surface 79. As the lapping procaeds, the motor 77 lowers the shaft 75, the retainer 73 and the substrate 70 with the fiber 22 attached thereto such that the planar surface 34 is formed by lapping radially 20 inward from the point of initial contact between the fiber 22 and the lapping surface 79.
A preferred rnethod for determining the depth to which the fiber is lapped is to apply an optical signal to one end thereof fronn a laser 81 and to monitor the optical output at the other end with a photodetector 2~ 83. A lapping slurry having a refractive index near that of the fiber 22 is maintained on the lapping surface 79 during the lapping process. As the lapping proceeds, light couples from the fiber 22 into the lapping slurry, thereby reducing the optical throughput of the fiber 22. Tha optical throughput may be correlatsd to the lapping depth. In general, 30 the relation between the opticaJ throughput and lapping depth depends upon the specific type of fiber being lapped. Therefore, it is necessary to perform a series of measurements of the lapping depth as a function of optical throughput to produce a calibration curve for the par~icular fiber being lapped and the lapping slurry used ~herewith.
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As explained previously, care must be taken to avoid removal of too much cladding material from the fibers used to form the evanescent field coupier 20. Using ordinary single mods flber, forming the coupler 20 to have a coupling efficiency of one to two percent 5 requires removal nf about ten percent of the core depth at the center of the oval surfaces.
After the fibers 22 and 24 are mounted on the corresponding substrates 70 and 72 and the oval surfaces are formed using, for example, the rnethods described above, the planar surfaces 34 and 36 10 are placed in juxtaposition as shown in Figures 7-9. A preferred method for holding the surfaces 34 and 36 in the desired positions is to place the substrates 70 and 72 are placed in a jig 82 as shown in Figure 9. The jig- 82 includes a pair of retainers 84 and 86 for holding the substratÆs 70 and 72, respectively, so that they are movable with 1~ respect to one another. The substra~es 70 and 72 are placed in desired positions relative to one another and then the fibers 22 and 24 are bonded together. Ordinarily, the fibers 22 and 24 will be position0d t maximize the coupling of optical signals therebetween.
The coupler 20 may be formed to have a desired coupling 2Q constant. One preferred method for assuring achievernent of a desired coupling constant includes the step of inputting an optical signal frorn a laser 90 into an end 92 of the fiber 22. The intensities of the optical signals emanating from the fibers 22 and 24 after the inpu~ beam has impinged upon the interaction re~ion 42 are monitored using suitable 25 photodetectors 94 and 96, respectively, while the substrates are manipulated to achieve a desired coupling efficieney. The amount of coupling may be varied by moving the substrates 28 in the jig 72 to adjust the amount of overlap of the planar surfacss 30 and 32. The coupling efficiency is Tl = 1 - It/i lC(lt + ~C)-1 ~
where 1l is the coupling efficiency, Ij is the light intensity input to fiber 22, It iS the light transmitted through fiber 22 beyond the interaction region 42 and Ic is the light intensity coupled from fiber 22 to fiber 24.
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After the fibers 22 and 24 have been positioned to provide the desired coupling constant, energy is applied to the interface oF the planar surFaces 30 and 32. As shown in Figure 8, the energy source may be a laser 98. The laser ~8 is p~ferably a CO2 laser, and it should produce an sutput beam that will heat the fibers 22 and 24 to a temperature near the glass transition temperature. The energy source may also be an ultrasonic wave genera~or, an induction heating source or other suitable device for providing the desired amount of heat to the fibers 22 and 24. As shown in Figures 8 and 9, a forc~ F may be applied to compress the fibers 22 and 24 together during the bonding process. Generally it has been found that a compressive force of about a pound facilitates formation of the coherent molecular bond The transition temperatura is below the melting point of the glass from which ~he fibers 22 and 24 are formed. Ths transition temperature depends upon the materials comprising the fibers 22 and 24. Most optical fiber is formed from silicon dioxide with a dopant such as germanium dioxide or boron added thareto to control the refractive index. Such fibers typically have transition temperatures in thc range of 1100 C to 1200 C. The transition temperature should be determined ~o ~xperimentally for the fibers to be joined, and the energy output from the laser 98 should be controlled to assure that the temperature in the bonded region does not excsed the transition temperature. The transition temperaturc of an optical fiber is attained when the fiber begins to soften as the temperature increases.
Applying the outpwt of the laser 98 over the juncture of the surfaces 30 and 32 fuses the fibers 22 and 24 together. It has been found that the above described method forms a junction of the surfaces 30 and 32 that results in a coherent molecular bonded r2gion having the same physical structure and the samc optical characteristics as the bulk material comprising ~ibers 22 and 24.
The processes of forming and joining optically flat surfaces on fiber 22 an~l 24 described herein provide a fiber optic coupler having a bonded surfaoe that is molecularly coherent, homogeneous and continuous across and around ths joined surfaces 34 and 36 of the 3~ fibers 22 and 24. Accordingly, local irregwiarities in the refractive ~z~
indices are avoided, with the resultant interaction region 46 of the joined region having well behaved refractive inclices throughout as expected for a molecularly consistent material. The step of coupling light from the fibers 22 and 24 while they are lapped to form the optically flat surfaces 34 and 36, respectively, permits sufficient control of the lapping depth ~abrication to form the coupler 20 to have a predetermined coupling efficiency.
The primary difference between the steps for fabricating the evanescent field coupler 20 and the intercepting cors coupler 48 is the - depth to which the fibers 22, 24, 50 and 52 are lapped. The amount of coupling depends upon the length of the interaction zone, which is a function of the lapping depth and the radius of curvature of the flber being lapped. It has been found that in general a 3 dB intercepting core coupler should have the fibers lapped to remove 5û% of the core 15 to provide full modal mixing. It is well known from electromagnetic theory that the energy distributions of tha normal modes varies with the radial distance from the center of an optical fiber. The energy in the lower orcler modes tends to be primarily in the ~entral region of the core, whereas the higher order modes tend to have more snergy near 20 the core/cladding interface. Since most of the energy in a multimode fiher is in the lower order modes, good coupling is facilitated by having the central regions of the cores in contact.
Couplers formed according to the absve described method have been cut into sections and examined with high power 25 microscopes and a mireau interferometer. These instruments show that the bond interface has no distortion of the molecular arrangements of the cores or the claddings of the fibers and that the rnolecular structure of the inter~ace is identical to that of the fibers.
, ,
Claims (10)
1. A fiber optic coupler for coupling an optical wave between a pair of optical fibers each having a central core surrounded by a cladding, the cores and claddings having characteristic refractive indices, comprising:
a first planar surface formed on a first optical fiber by removing at least a portion of the cladding therefrom;
a second planar surface formed on a second optical fiber by removing at least a portion of the cladding therefrom, the first and second planar surfaces being juxtaposed to form an interaction region wherein light propagates between the fibers; and a coherent molecular bond formed between the first and second planar surfaces.
a first planar surface formed on a first optical fiber by removing at least a portion of the cladding therefrom;
a second planar surface formed on a second optical fiber by removing at least a portion of the cladding therefrom, the first and second planar surfaces being juxtaposed to form an interaction region wherein light propagates between the fibers; and a coherent molecular bond formed between the first and second planar surfaces.
2. The fiber optic coupler of claim 1 wherein the coherent molecular bond is formed while maintaining the characteristic core and cladding refractive indices constant at the interaction region.
3. The fiber optic coupler of claim 1 wherein the coherent molecular bond is formed by lapping the first and second planar surfaces to be optically flat and bonding them together by application of a controlled amount of energy thereto.
4. The fiber optic coupler of claim 3 wherein a compressive force is applied to the first and second fibers to apply pressure between the first and second planar surfaces as they are bonded together.
5. A method for forming a fiber optic coupler for coupling an optical wave between a pair of optical fibers each having a central core surrounded by a cladding, the cores and claddings having characteristic refractive indices, comprising the steps of:
forming a first planar surface formed on a first optical fiber by removing at least a portion of the cladding therefrom;
forming a second planar surface formed on a second optical fiber by removing at least a portion of the cladding therefrom, the first and second planar surfaces being juxtaposed to form an interaction region wherein light propagates between the fibers; and forming a coherent molecular bond formed between the first and second planar surfaces.
forming a first planar surface formed on a first optical fiber by removing at least a portion of the cladding therefrom;
forming a second planar surface formed on a second optical fiber by removing at least a portion of the cladding therefrom, the first and second planar surfaces being juxtaposed to form an interaction region wherein light propagates between the fibers; and forming a coherent molecular bond formed between the first and second planar surfaces.
6. The method of claim 5 wherein the step of forming the coherent molecular bond comprises the steps of:
aligning the planar surfaces relative to one another to provide a predetermined coupling efficiency; and applying energy to the planar surfaces to bond them together.
aligning the planar surfaces relative to one another to provide a predetermined coupling efficiency; and applying energy to the planar surfaces to bond them together.
7. The method of claim 6 wherein the step of aligning the planar surfaces includes the steps of:
introducing an optical beam into a first end of one of the fibers on one side of the interaction region; and monitoring the optical energy output from an end of at least one of the fibers on the other side of the interaction region.
introducing an optical beam into a first end of one of the fibers on one side of the interaction region; and monitoring the optical energy output from an end of at least one of the fibers on the other side of the interaction region.
8. The method of claim 6 wherein the step of applying energy to the planar surfaces includes focusing a beam of coherent light thereon.
9. The method of claim 6 wherein forming a coherent molecular bond includes heating the fibers to a transition temperature below the melting temperature of the fibers.
10. The method of claim 9, further including the step of applying a compressive force is to the first and second fibers to apply pressure between the first and second planar surfaces as they are bonded together.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US816,982 | 1986-01-07 | ||
| US06/816,982 US4699482A (en) | 1982-06-23 | 1986-01-07 | Opthalmoscopic system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA1264582A true CA1264582A (en) | 1990-01-23 |
Family
ID=25222089
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA000519622A Expired - Lifetime CA1264582A (en) | 1986-01-07 | 1986-10-02 | Molecular bonded fiber optic couplers and method of fabrication |
Country Status (1)
| Country | Link |
|---|---|
| CA (1) | CA1264582A (en) |
-
1986
- 1986-10-02 CA CA000519622A patent/CA1264582A/en not_active Expired - Lifetime
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