Tunable filter with core mode blocker

Abstract
An optic apparatus includes an optical fiber with a cladding surrounding a core and a core-mode blocker included in at least a portion of an interactive region of the optical fiber. A mode coupler is coupled to the optical fiber and couples a first mode to a different spatial mode in a forward direction of the optical fiber.
Description




BACKGROUND OF THE INVENTION




1. Field of the Invention




This invention relates generally to an acousto-optic wavelength tunable bandpass filter, and more particularly to an acousto-optic wavelength tunable bandpass filter that includes a core mode blocker.




2. Description of Related Art




In modern telecommunication systems, many operations with digital signals are performed on an optical layer. For example, digital signals are optically amplified, multiplexed and demultiplexed. In long fiber transmission lines, the amplification function is performed by Erbium Doped Fiber Amplifiers (EDFA's). The amplifier is able to compensate for power loss related to signal absorption, but it is unable to correct the signal distortion caused by linear dispersion, 4-wave mixing, polarization distortion and other propagation effects, and to get rid of noise accumulation along the transmission line. For these reasons, after the cascade of multiple amplifiers the optical signal has to be regenerated every few hundred kilometers. In practice, the regeneration is performed with electronic repeaters using optical-to-electronic conversion. However to decrease system cost and improve its reliability it is desirable to develop a system and a method of regeneration, or signal refreshing, without optical to electronic conversion. An optical repeater that amplifies and reshapes an input pulse without converting the pulse into the electrical domain is disclosed, for example, in the U.S. Pat. No. 4,971,417, Radiation-Hardened Optical Repeater”. The repeater comprises an optical gain device and an optical thresholding material producing the output signal when the intensity of the signal exceeds a threshold. The optical thresholding material such as polydiacetylene thereby performs a pulse shaping function. The nonlinear parameters of polydiacetylene are still under investigation, and its ability to function in an optically thresholding device has to be confirmed.




Another function vital to the telecommunication systems currently performed electronically is signal switching. The switching function is next to be performed on the optical level, especially in the Wavelength Division Multiplexing (WDM) systems. There are two types of optical switches currently under consideration. First, there are wavelength insensitive fiber-to-fiber switches. These switches (mechanical, thermo and electro-optical etc.) are dedicated to redirect the traffic from one optical fiber to another, and will be primarily used for network restoration and reconfiguration. For these purposes, the switching time of about 1 msec (typical for most of these switches) is adequate; however the existing switches do not satisfy the requirements for low cost, reliability and low insertion loss. Second, there are wavelength sensitive switches for WDM systems. In dense WDM systems having a small channel separation, the optical switching is seen as a wavelength sensitive procedure. A small fraction of the traffic carried by specific wavelength should be dropped and added at the intermediate communication node, with the rest of the traffic redirected to different fibers without optical to electronic conversion. This functionality promises significant cost saving in the future networks. Existing wavelength sensitive optical switches are usually bulky, power-consuming and introduce significant loss related to fiber-to-chip mode conversion. Mechanical switches interrupt the traffic stream during the switching time. Acousto-optic tunable filters, made in bulk optic or integrated optic forms, (AOTFs) where the WDM channels are split off by coherent interaction of the acoustic and optical fields though fast, less than about 1 microsecond, are polarization and temperature dependent. Furthermore, the best AOTF consumes several watts of RF power, has spectral resolution about 3 nm between the adjacent channels (which is not adequate for current WDM requirements), and introduces over 5 dB loss because of fiber-to-chip mode conversions.




Another wavelength-sensitive optical switch may be implemented with a tunable Fabry Perot filter (TFPF). When the filter is aligned to a specific wavelength, it is transparent to the incoming optical power. Though the filter mirrors are almost 100% reflective no power is reflected back from the filter. With the wavelength changed or the filter detuned (for example, by tilting the back mirror), the filter becomes almost totally reflective. With the optical circulator in front of the filter, the reflected power may be redirected from the incident port. The most advanced TFPF with mirrors built into the fiber and PZT alignment actuators have only 0.8 dB loss. The disadvantage of these filters is a need for active feedback and a reference element for frequency stability.




A VOA is in opto-mechanical device capable of producing a desired reduction in the strength of a signal transmitted through a optical fiber. Ideally, the VOA should produce a continuously variable signal attenuation while introducing a normal or suitable insertion loss and exhibiting a desired optical return loss. If the VOA causes excessive reflectance back toward the transmitter, its purpose will be defeated.




Although fixed band-rejection filters are readily available using Bragg or long-period gratings impressed into the core of an optical fiber there are no simple, adjustable all-fiber bandpass filters. Such filters would vary the amplitude of signals within a fixed wavelength range. Although a variable transmission bandpass filter of sorts can be made by varying the center wavelength of a Bragg or long-period grating, as one channel is attenuated another channel is unavoidably strengthened.




Accordingly, there is a need for a bandpass filter that changes its amplitude transmission over a fixed wavelength spectrum. There is a further need for a bandpass filter with variable transmission over a fixed wavelength range, and which blocks all other wavelengths.




SUMMARY OF THE INVENTION




Accordingly, an object of the present invention is to provide an acousto-optic wavelength tunable bandpass filter.




Another object of the present invention is to provide an acousto-optic wavelength tunable bandpass filter that is widely tunable.




Still another object of the present invention is to provide a bandpass filter that has an adjustable transmission.




A further object of the present invention is to provide a bandpass filter with variable transmission over a fixed wavelength range, and which blocks all other wavelengths




These and other objects of the present invention are achieved in an optic apparatus that includes an optical fiber with a cladding surrounding a core and a core-mode blocker included in at least a portion of an interactive region of the optical fiber. A mode coupler is coupled to the optical fiber and couples a first mode to a different spatial mode in a forward direction of the optical fiber.




In another embodiment of the present invention, an optic apparatus includes an optical fiber with a cladding surrounding a core and a core-mode blocker included in at least a portion of an interactive region of the optical fiber. A mode coupler is coupled to optical fiber and couples a first mode to a different spatial mode in a forward direction of the optical fiber. A Faraday mirror coupled to the optical fiber.











BRIEF DESCRIPTION OF THE FIGURES




FIG.


1


(


a


) is a schematic diagram of one embodiment of an AOTF of the present invention.




FIG.


1


(


b


) is a cross-sectional view of the optical fiber of the

FIG. 1

AOTF.





FIG. 2

is a cross-sectional view of one embodiment of an acoustic wave propagation member that can be used with the AOTF of FIG.


1


.




FIG.


3


(


a


) is a cross-sectional view illustrating one embodiment of an interface created between an optical fiber and a channel formed in an acoustic wave propagation member of the

FIG. 1

AOTF.




FIG.


3


(


b


) is a cross-sectional view illustrating an embodiment of an interface between an optical fiber and a channel formed in an acoustic wave propagation member of the

FIG. 1

AOTF where a bonding material is used.





FIG. 4

is a schematic diagram of one embodiment of an AOTF of the present invention with an acoustic damper.





FIG. 5

is a cross-sectional view of one embodiment of an index profile of an optical fiber, useful with the AOTF of

FIG. 1

, that has a doubling cladding.





FIG. 6

is a cross-sectional view of an optical fiber with sections that have different diameters.





FIG. 7

is a cross-sectional view of an optical fiber with a tapered section.





FIG. 8

is a perspective view of one embodiment of an AOTF of the present invention that includes a heatsink and two mounts.





FIG. 9

is a perspective view of one embodiment of an AOTF of the present invention with a filter housing.





FIG. 10

is a block diagram of an optical communication system with one or more AOTF's of the present invention.





FIG. 11

is a schematic view showing the structure of an acousto-optic tunable filter according to one embodiment of the present invention.





FIG. 12

is a graph showing the coupling and transmittance of the filter of FIG.


1


.





FIG. 13

is a graph showing the transmittance of the filter of FIG.


11


.





FIG. 14

is a graph showing the center wavelength of filter of

FIG. 1

as a function of the frequency applied to the acoustic wave generator.




FIGS.


15


(


a


)-(


d


) are graphs illustrating the transmissions of the filter of

FIG. 11

when multiple frequencies are applied to the acoustic wave generator.




FIGS.


16


(


a


)-(


b


) are graphs showing the transmittance characteristics of the filter of

FIG. 11

when varying an electric signal with a three frequency component applied to the filter.




FIGS.


17


(


a


)-(


d


) are graphs for comparing the mode converting characteristic of the filter according to an embodiment of the present invention with that of a conventional wavelength filter.




FIG.


18


(


a


) illustrate one embodiment of a transmission spectrum of the

FIG. 11

filter.




FIG.


18


(


b


) illustrates the measured and the calculated center wavelengths of the notches as a function of acoustic frequency of an embodiment of the

FIG. 11

filter.





FIG. 19

illustrates two examples of configurable spectral profiles with spectral tilt from the

FIG. 11

filter.




FIG.


20


(


a


) is a filter assembly that includes two filters of

FIG. 11

that are in series.




FIG.


20


(


b


) is a schematic diagram of a dual-stage EDFA with a filter of FIG.


20


(


a


).




FIG.


21


(


a


) is a graph of gain profiles of an EDFA with the filter of FIG.


20


(


a


).




FIG.


21


(


b


) is a graph illustrating filter profiles that produced the flat gain profiles shown in FIG.


21


(


a


).




FIG.


21


(


c


) is a graph illustrating filter profiles of the FIG.


20


(


a


) filter assembly.




FIGS.


22


(


a


) and


22


(


b


) are graphs illustrating the polarization dependence of one embodiment of the filter of the present invention.





FIG. 23

illustrates one embodiment of the present invention from

FIG. 4

that has a reduction with a lower polarization dependent loss.




FIGS.


24


(


a


) and


24


(


b


) are graphs illustrating the polarization dependent loss profile of one embodiment of the invention, from

FIG. 4

, when the filter is operated to produce 10-dB attenuation at 1550 nm.





FIG. 25

illustrates an embodiment of the invention with two of the filters of FIG.


1


.





FIG. 26

is a graph illustrating the effects of a backward acoustic reflection at the damper of one embodiment of the present invention from FIG.


4


.




FIG.


27


(


a


) is a graph illustrating, in one embodiment of

FIG. 4

, the modulation depth at 10-dB attenuation level at both first- and second-harmonics of the acoustic frequency. FIG.


27


(


b


) is a graph illustrating the modulation depth of first- and second-harmonics components from FIG.


27


(


a


).





FIG. 28

is a schematic diagram of one embodiment of a VOA assembly of the present invention with a feedback loop.





FIG. 29

is a schematic diagram of another embodiment of a VOA of the present invention with a demultiplexer and a multiplexer.





FIG. 30

is a schematic diagram of an embodiment of a channel equalizer of the present invention using a single router.





FIG. 31

is a schematic diagram of another embodiment of a channel equalizer of the present invention using multiple routers.





FIG. 32

is a schematic diagram of an embodiment of the present invention with a second acoustic wave generator.





FIG. 33

is a schematic diagram of an embodiment of the present invention with a feedback loop coupled to the second acoustic generator of the

FIG. 32

device.





FIG. 34

is a schematic diagram of an embodiment of the present invention that includes an acoustic damper with a tapered proximal end.





FIG. 35

is a schematic diagram of an embodiment of the present invention with an acoustic damper and a second acoustic wave generator.




FIG.


36


(


a


) is a schematic diagram of an embodiment of the present invention that includes a code mode blocker in a fiber that is coupled to a mode coupler.




FIG.


36


(


b


) is a schematic diagram of two single mode optical fibers etched with HF to create a code mode blocker of the present invention.




FIG.


36


(


c


) is a schematic diagram of two single mode optical fibers etched and about to be spliced together to form the code mode blocker of the present invention.




FIG.


36


(


d


) is a schematic diagram of the two single mode optical fibers of FIG.


36


(


b


) spliced together to create a code mode blocker.




FIGS.


37


(


a


)-


37


(


d


) illustrate the spectra at the core mode and the cladding mode at positions “A”, “B”, “C”, and “D” of the FIG.


36


(


d


) filter.





FIG. 38

illustrates the measured transmission spectrum of the FIG.


36


(


d


) filter.





FIG. 39

shows the variation of the transmitted wavelength of the FIG.


36


(


d


) filter according to the acoustic frequency.





FIG. 40

illustrates one embodiment of the present invention that includes at least one long period grating.











DETAILED DESCRIPTION





FIG. 1

illustrates one embodiment of an AOTF (hereafter filter


10


) of the present invention. An optical fiber


12


has a longitudinal axis, a core


14


and a cladding


16


in a surrounding relationship to core


14


. Optical fiber


12


can be a birefringent or non-birefringent single mode optical fiber and a multi-mode fiber. Optical fiber


12


can have, multiple modes traveling within the fiber such as core to core, core to cladding and polarization to polarization, multiple cladding modes and a single core mode guided along core


14


, support core to cladding modes and multiple cladding modes. Optical fiber


12


provides fundamental and cladding mode propagation along a selected length of optical fiber


12


. Alternatively, optical fiber


12


is a birefringent single mode fiber that does not have multiple cladding modes and a single core mode. In one embodiment, optical fiber


12


is tensioned. Sufficient tensioning can be applied in order to reduce losses in a flexure wave propagated in optical fiber


12


.




The core of optical fiber


12


is substantially circular-symmetric. The circular symmetry ensures that the refractive index of the core mode is essentially insensitive to the state of optical polarization. In contrast, in hi-birefringent single mode fibers the effective refractive index of the core mode is substantially different between two principal polarization states. The effective refractive index difference between polarization modes in high birefringence single mode fibers is generally greater than 10


−4


. A highly elliptical core and stress-inducing members in the cladding region are two main techniques to induce large birefringence. In non-birefringent fibers, the effective index difference between polarization states is generally smaller than 10


−5


.




An acoustic wave propagation member


18


has a distal end


20


that is coupled to optical fiber


12


. Acoustic wave propagation member


18


propagates an acoustic wave from a proximal end


22


to distal end


20


and launches a flexural wave in optical fiber


12


. The flexural wave creates a periodic microbend structure in optical fiber


12


. The periodic microbend induces an antisymmetric refractive index change in the fiber and, thereby, couples light in the fiber from different modes traveling within optical fiber


12


such as a core mode to cladding modes. For efficient mode coupling, the period of the microbending, or the acoustic wavelength, should match the beatlength between the coupled modes. The beatlength is defined by the optical wavelength divided by the effective refractive index difference between the two modes.




Acoustic wave propagation member


18


can be mechanically coupled to the optical fiber and minimizes acoustic coupling losses in between the optical fiber and the acoustic wave propagation member. In one embodiment, acoustic wave propagation member


18


is coupled to optical fiber


12


in a manner to create a lower order mode flexure wave in optical fiber


12


. In another embodiment, acoustic wave propagation member


18


is coupled to the optical fiber to match a generation of modes carried by optical fiber


12


.




Acoustic wave propagation member


18


can have a variety of different geometric configurations but is preferably elongated. In various embodiments, acoustic wave propagation member


18


is tapered proximal end


22


to distal end


20


and can be conical. Generally, acoustic wave propagation member


18


has a longitudinal axis that is parallel to a longitudinal axis of optical fiber


12


.




At least one acoustic wave generator


24


is coupled to proximal end


22


of acoustic wave propagation member. Acoustic wave generator


24


can be a shear transducer.




Acoustic wave generator


24


produces multiple acoustic signals with individual controllable strengths and frequencies. Each of the acoustic signals can provide a coupling between different modes traveling within the fiber. Acoustic wave generator


24


can produce multiple acoustic signals with individual controllable strengths and frequencies. Each of the acoustic signals provides a coupling between different modes traveling within optical fiber


12


. A wavelength of an optical signal coupled to cladding


16


from core


14


is changed by varying the frequency of a signal applied the acoustic wave generator


24


.




Acoustic wave generator


24


can be made at least partially of a piezoelectric material whose physical size is changed in response to an applied electric voltage. Suitable piezoelectric materials include but are not limited to quartz, lithium niobate and PZT, a composite of lead, zinconate and titanate. Other suitable materials include but are not limited to zinc monoxide. Acoustic wave generator


24


can have a mechanical resonance at a frequency in the range of 1-20 MHz and be coupled to an RF signal generator.




Referring now to

FIG. 2

, one embodiment of acoustic wave propagation member


18


has an interior with an optical fiber receiving channel


26


. Channel


26


can be a capillary channel with an outer diameter slightly greater than the outer diameter of the fiber used and typically in the range of 80˜150 microns. The length of the capillary channel is preferably in the range of 5˜15 mm. The interior of acoustic wave propagation member


18


can be solid. Additionally, acoustic wave propagation member


18


can be a unitary structure.




Optical fiber


12


is coupled to acoustic wave propagation member


18


. As illustrated in FIG.


3


(


a


), the dimensions of channel


26


and an outer diameter of optical fiber


12


are sufficiently matched to place the two in a contacting relationship at their interface. In this embodiment, the relative sizes of optical fiber


12


and channel


26


need only be substantially the same at the interface. Further, in this embodiment, the difference in the diameter of optical fiber


12


and channel


26


are in the range of 1˜10 microns




In another embodiment, illustrated in FIG.


3


(


b


), a coupling member


28


is positioned between optical fiber


12


and channel


26


at the interface. Suitable coupling members


28


including but are not limited to bonding materials, epoxy, glass solder, metal solder and the like.




The interface between channel


26


and optical fiber


12


is mechanically rigid for efficient transduction of the acoustic wave from the acoustic wave propagation member


18


to the optical fiber


12


.




Preferably, the interface between optical fiber


12


and channel


26


is sufficiently rigid to minimize back reflections of acoustic waves from optical fiber


12


to acoustic wave propagation member


18


.




In the embodiments of FIGS.


3


(


a


) and


3


(


b


), acoustic wave propagation member


18


is a horn that delivers the vibration motion of acoustic wave generator


24


to optical fiber


12


. The conical shape of acoustic wave propagation member


18


, as well as its focusing effect, provides magnification of the acoustic amplitude at distal end


20


, which is a sharp tip. Acoustic wave propagation member


18


can be made from a glass capillary, such as fused silica, a cylindrical rod with a central hole, and the like.




In one embodiment, a glass capillary is machined to form a cone and a flat bottom of the cone was bonded to a PZT acoustic wave generator


24


. Optical fiber


12


was bonded to channel


26


. Preferably, distal end


20


of acoustic wave generator


18


is as sharp as possible to minimize reflection of acoustic waves and to maximize acoustic transmission. Additionally, the exterior surface of acoustic wave generator


18


is smooth. In another embodiment, acoustic wave generator


18


is a horn with a diameter that decreases exponentially from proximal end


22


to distal end


20


.




As illustrated in

FIG. 4

, filter


10


can also include an acoustic damper


30


that is coupled to optical fiber


12


. Acoustic damper


30


includes a jacket


32


that is positioned in a surrounding relationship to optical fiber


12


. Acoustic damper


30


absorbs incoming acoustic waves and minimizes reflections of the acoustic wave. The reflected acoustic wave causes an intensity modulation of the optical signal passing through the filter by generating frequency sidebands in the optical signal. The intensity modulation is a problem in most applications. A proximal end


34


of the acoustic damper


30


can be tapered. Acoustic damper


30


can be made of a variety of materials. In one embodiment, acoustic damper


30


is made of a soft material that has a low acoustic impedance so that minimizes the reflection of the acoustic wave. Jacket


32


itself is a satisfactory damper and in another embodiment jacket


32


takes the place of acoustic damper


30


. Optionally, jacket


32


is removed from that portion of optical fiber


12


in a first region


36


and that portion of optical fiber


12


that is bonded to acoustic wave generator


24


.




First region


36


is where there is a coupling between any two or more modes within the fiber by the acoustic wave. Examples of coupling between two fiber modes includes, core to core, core to cladding and polarization to polarization. This coupling is changed by varying the frequency of a signal applied to acoustic wave generator


24


. In one embodiment, first region


36


extends from distal end


20


to at least a proximal portion within acoustic damper


30


. In another embodiment, first region


36


extends from distal end


20


and terminates at a proximal end of acoustic damper


30


. In one embodiment, the length of optical fiber


12


in first region


36


is less than 1 meter, and preferably less than 20 cm. The nonuniformity of the fiber reduces the coupling efficiency and also causes large spectral sidebands in the transmission spectrum of the filter. Another problem of the long length is due to the mode instability. Both the polarization states of the core and cladding modes and the orientation of the symmetry axis of an antisymmetric cladding mode are not preserved as the light propagates over a long length greater than 1 m. This modal instability also reduces the coupling efficiency and causes large spectral sidebands. Preferably, the outer diameter of optical fiber


12


, with jacket


32


, is in the range of 60-150 microns.




The profile of the refractive index of the cross section of optical fiber


12


influences its filtering characteristics. One embodiment of optical fiber


12


, illustrated in

FIG. 5

, has a first and second cladding


16


′ and


16


″ with core


14


that has the highest refractive index at the center. First cladding


16


′ has an intermediate index and second cladding


16


″ has the lowest index. Most of the optical energy of several lowest-order cladding modes is confined both only in core


14


and first cladding


16


′. The optical energy falls exponentially from the boundary between first and second claddings


16


′ and


16


″, respectively.




Optical fields are negligible at the interface between second cladding


16


″ and the surrounding air, the birefringence in the cladding modes, due to polarization-induced charges, is much smaller than in conventional step-index fibers where second cladding


16


″ does not exist. The outer diameter of first cladding


16


′ is preferably smaller than that of second cladding


16


″, and can be smaller by at least 5 microns. In one specific embodiment, core


14


is 8.5 microns, first cladding


16


′ has an outer diameter of 100 microns and second cladding


16


″ has an outer diameter of 125 microns. Preferably, the index difference between core


14


and first cladding


16


′ is about 0.45%, and the index difference between first and second claddings


16


′ and


16


″ is about 0.45%.




In another embodiment, the outer diameter of first cladding


16


′ is sufficiently small so that only one or a few cladding modes can be confined in first cladding


16


′. One specific example of such an optical fiber


12


has a core


14


diameter of 4.5 microns, first cladding


16


′ of 10 microns and second cladding


16


″ of 80 microns, with the index difference between steps of about 0.45% each.




The optical and acoustic properties of optical fiber


12


can be changed by a variety of different methods including but not limited to, (i) fiber tapering, (ii) ultraviolet light exposure, (iii) thermal stress annealing and (iv) fiber etching.




One method of tapering optical fiber


12


is achieved by heating and pulling it. A illustration of tapered optical fiber


12


is illustrated in FIG.


6


. As shown, a uniform section


38


of narrower diameter is created and can be prepared by a variety of methods including but not limited to use of a traveling torch. Propagation constants of optical modes can be greatly changed by the diameter change of optical fiber


12


. The pulling process changes the diameter of core


14


and cladding


16


and also changes the relative core


14


size due to dopant diffusion. Additionally, the internal stress distribution is modified by stress annealing. Tapering optical fiber


12


also changes the acoustic velocity.




When certain doping materials of optical fiber


12


are exposed to ultraviolet light their refractive indices are changed. In one embodiment, Ge is used as a doping material in core


14


to increase the index higher than a pure SiO


2


cladding


16


. When a Ge-doped optical fiber


12


is exposed to ultraviolet light the index of core


14


can be changed as much as 0.1%. This process also modifies the internal stress field and in turn modifies the refractive index profile depending on the optical polarization state. As a result, the birefringence is changed and the amount of changes depends on optical modes. This results in changes of not only the filtered wavelength at a given acoustic frequency or vice versa but also the polarization dependence of the filter. Therefore, the UV exposure can be an effective way of trimming the operating acoustic frequency for a given filtering wavelength as well as the polarization dependence that should preferably be as small as possible in most applications.




Optical fiber


12


can be heated to a temperature of 800 to 1,300° C. or higher to change the internal stresses inside optical fiber


12


. This results in modification of the refractive index profile. The heat treatment is another way of controlling the operating acoustic frequency for a given filtering wavelength as well as the polarization dependence.




The propagation velocity of the acoustic wave can be changed by chemically etching cladding


16


of optical fiber


12


. In this case, the size of core


14


remains constant unless cladding is completely etched. Therefore, the optical property of core mode largely remains the same, however, that of a cladding mode is altered by a different cladding diameter. Appropriate etchants include but are not limited to hydro fluoride (HF) acid and BOE.




The phase matching of optical fiber


12


can be chirped. As illustrated in

FIG. 6

, a section


40


of optical fiber can have an outer diameter that changes along its longitudinal length. With section


40


, both the phase matching condition and the coupling strength are varied along its z-axis


42


and the phase matching conditions for different wavelengths satisfied at different positions along the axis. The coupling then can take place over a wide wavelength range. By controlling the outer diameter as a function of its longitudinal axis


42


, one can design various transmission spectrum of the filter. For example, uniform attenuation over a broad wavelength range is possible by an appropriate diameter control.




Chirping can also be achieved when the refractive index of core


14


is gradually changed along z-axis


42


. In one embodiment, the refractive index of core


14


is changed by exposing core


14


to ultraviolet light with an exposure time or intensity as a function of position along the longitudinal axis. As a result, the phase matching condition is varied along z-axis


42


. Therefore, various shapes of transmission spectrum of the filter can be obtained by controlling the variation of the refractive index as a function of the longitudinal axis


42


.




As illustrated in

FIG. 8

a heatsink


44


can be included to cool acoustic wave generator. In one embodiment, heatsink


44


has a proximal face


46


and a distal face


48


that is coupled to the acoustic wave generator


24


. Preferably, acoustic wave generator


24


is bonded to distal face


48


by using a low-temperature-melting metal-alloy solder including but not limited to a combination of 95% zinc and 5% tin and indium-based solder materials. Other bonding material includes heat curable silver epoxy. The bonding material should preferably provide good heat and electrical conduction. Heatsink


44


provides a mount for the acoustic wave generator


24


. Heatsink can be made of a variety of materials including but not limited to aluminum, but preferably is made of a material with a high heat conductivity and a low acoustic impedance.




Acoustic reflections at proximal face can be advantageous if controlled. By introducing some amount of reflection, and choosing a right thickness of heatsink


44


, the RF response spectrum of acoustic wave generator


24


can be modified so the overall launching efficiency of the acoustic wave in optical fiber can be less dependent on the RF frequency.




In this case, the reflectivity and size of heatsink


44


is selected to provide a launching efficiency of the flexural wave into optical fiber


12


almost independent of an RF frequency applied to acoustic wave generator


24


. The thickness of heatsink


44


is selected to provide a travel time of an acoustic wave from distal face


48


to proximal face


46


, and from proximal face


46


to distal face


48


that substantially matches a travel time of the acoustic wave traveling through acoustic wave propagation member


24


from its proximal end to its distal end, and from its distal end to its proximal end. The heat sink material or the material for the attachment to the proximal face


46


is selected to provide the amount of back reflection from the heat sink that substantially matches the amount of back reflection from the acoustic wave propagation member. In various embodiments, the proximal and distal faces,


46


,


48


of heatsink


44


have either rectangular or circular shapes with the following dimensions: 10×10 mm


2


for the rectangular shape and diameter of 10 mm for the cylindrical shaped heat sink.




However, acoustic back reflections due to proximal face


46


are preferably avoided. Acoustic reflections from the heat sink back to the acoustic wave generator are reduced by angling proximal face


46


at an angle greater than 45 degree or by roughing the face. The acoustic wave coming from the acoustic generator toward the angled proximal face


46


is reflected away from the acoustic generator, reducing the acoustic back reflection to the acoustic wave generator. The roughed face also reduces the acoustic reflection by scattering the acoustic wave to random directions. Preferably, the side faces of the heat sink are also roughened or grooved to scatter the acoustic wave and thereby to avoid the acoustic back reflection. Another method to reduce the back reflection is to attach an acoustic damping material at the proximal face


46


. Suitable materials that reduce back reflections include soft polymers, silicone, and the like that can be applied to proximal face


46


.




Referring again to

FIG. 8

, an acoustic damper mount


50


supports acoustic damper


30


. Acoustic damper mount


50


can be made of a variety of materials including but not limited to silica, invar, and the like. A filter mount


52


supports heatsink


44


and acoustic damper mount


50


. In one embodiment, filter mount is a plate-like structure. Preferably, filter mount


52


and optical fiber


12


have substantially the same thermal expansion coefficients. Filter mount


52


and fiber


12


can be made of the same materials.




Filter mount


52


and optical fiber


12


can have different thermal expansion coefficients and be made of different materials. In one embodiment, filter mount


52


has a lower thermal expansion coefficient than optical fiber


12


. Optical fiber


12


is tensioned when mounted and bonded to the filter mount


52


. The initial strain on optical fiber


12


is released when the temperate increases because the length of filter mount


52


is increased less than optical fiber


12


. On the other hand, when the temperature decreases optical fiber


12


is stretched further. When the amount of strain change according to temperature change is appropriately chosen by selecting proper material for mount the


52


, the filtering wavelength of filter


10


can be made almost independent of temperature. Without such mounting arrangement, the center wavelength of the filter increases with temperature. Additionally, first region


36


of is sufficiently tensioned to compensate for changes in temperature of first region


36


and filter mount


52


.




In another embodiment, illustrated in

FIG. 9

, a filter housing


54


encloses first region


36


. Filter housing


54


can be made of a variety of materials, including but not limited to silica, invar and the like. Filter housing


54


eliminates the need for a separate filter mount


52


. Filter housing


54


extends from distal face


48


of heatsink


44


to acoustic damper


30


or to a jacketed portion


32


of optical fiber


12


. Acoustic wave propagation member


18


, acoustic wave generator


24


and the acoustic damper


30


can be totally or at least partially positioned in an interior of filter housing


54


.




In one embodiment, filter housing


54


and optical fiber


12


are made of materials with substantially similar thermal expansion coefficients. A suitable material is silica. Other materials are also suitable and include invar. Filter housing


54


and optical fiber


12


can have different thermal expansion coefficients and be made of different materials. In one embodiment, filter housing


54


has a lower thermal expansion coefficient than optical fiber


12


.




In one embodiment, first region


36


is sufficiently tensioned sufficiently to compensate for changes in temperature of first region


36


and filter housing


54


.




As illustrated in

FIG. 10

, filter


10


can be a component or subassembly of an optical communication system


56


that includes a transmitter


58


and a receiver


60


. Transmission


58


can include a power amplifier with filter


10


and receiver


60


can also include a pre amplifier that includes filter


10


. Additionally, optical communication system


56


may also have one or more line amplifiers that include filters


10


.




Referring now to

FIG. 11

, if an electric signal


57


with constant frequency “f” is applied to acoustic wave generator


24


, a flexural acoustic wave having the same frequency “f” is generated. The flexural acoustic wave is transferred to optical fiber


12


and propagates along optical fiber


12


, finally absorbed in acoustic damper


30


. The flexural acoustic wave propagating along optical fiber


12


produces periodic microbending along the fiber, resulting in the periodic change of effective refractive index which the optical wave propagating along optical fiber


12


experiences. The signal light propagating along optical fiber


12


in a core mode can be converted to a cladding mode by the change of effective refractive index in optical fiber


12


.




When signal light is introduced into filter


10


part of the signal light is converted to a cladding mode due to the effect of the acoustic wave and the remainder of the signal light propagates as a core mode while the signal light propagates along first region


36


. The signal light converted to a cladding mode cannot propagate any longer in optical fiber


12


with jacket


32


because the light is partly absorbed in optical fiber


12


or partly leaks from optical fiber


12


. A variety of mode selecting means, including a mode conversion means between core modes and cladding modes, can be incorporated in filter


10


. For example, the long-period grating described in the article “Long-period fiber-grating based gain equalizers” by A. M. Vengsarkar et al. in Optics Letters, Vol. 21, No. 5, p. 336, 1996 can be used as the mode selecting means. As another example, a mode coupler, which converts one or more cladding modes of one fiber to core modes of the same fiber or another fiber, can also be used.




A flexural acoustic wave generated by acoustic wave propagation member


18


propagates along first region


36


. The acoustic wave creates antisymmetric microbends that travel along first region


36


, introducing a periodic refractive-index perturbation along optical fiber


12


. The perturbation produces coupling of an input symmetric fundamental mode to an antisymmetric cladding mode when the phase-matching condition is satisfied in that the acoustic wavelength is the same as the beat length between the two modes. The coupled light in the cladding mode is attenuated in jacket


32


. For a given acoustic frequency, the coupling between the fundamental mode and one of the cladding modes takes place for a particular optical wavelength, because the beat length has considerable wavelength dispersion. Therefore, filter


10


can be operated as an optical notch filter. A center wavelength and the rejection efficiency are tunable by adjustment of the frequency and the voltage of RF signal applied to acoustic wave propagation member


18


, respectively.




The coupling amount converted to a different fiber mode is dependent on the wavelength of the input signal light. FIG.


12


(


a


) shows the coupling amounts as functions of wavelength when flexural acoustic waves at the same frequency but with different amplitudes are induced in optical fiber


12


. As shown in FIG.


12


(


a


), the coupling amounts are symmetrical with same specific wavelength line (λ


c


), i.e.,. center wavelength line, however they show different results


62


and


64


due to the amplitude difference of the flexural acoustic waves. Therefore, the transmittance of the output light which has passed through filter


12


is different depending on the wavelength of the input light. Filter


12


can act as a notch filter which filters out input light with specific wavelength as shown in FIG.


12


(


b


).




FIG.


12


(


b


) is a graph showing the transmittances as a function of wavelength when flexural acoustic waves with different amplitudes are induced in optical fiber


12


. The respective transmittances have same center wavelength as does the coupling amount, but different transmittance characteristic


64


and


66


depending on the amplitude difference of the flexural acoustic waves can be shown.




The center wavelength λ


c


, of filter


10


satisfies the following equation.






β


co


(λ)−β


cl


(λ)=2 π/λ


a








In the above equation, β


co


(λ) and β


cl


(λ) are propagation constants of core mode and cladding mode in optical fiber


12


which are respectively dependent on the wavelength, and λ


a


represents the wavelength of the flexural acoustic waves.




Accordingly, if the frequency of the electric signal applied to acoustic wave generator


24


varies, the wavelength of the acoustic wave generated in optical fiber


12


also varies, which results in the center wavelength change of filter


10


. In addition, since the transmission is dependent on the amplitude of the flexural acoustic wave, the transmission of signal light can be adjusted by varying the amplitude of the electric signal which is applied to acoustic wave generator


24


.





FIG. 13

is a graph showing the transmittance of filter


10


in one embodiment when different electric signal frequencies are applied. As shown in

FIG. 13

, each center wavelength (i.e., wavelength showing maximum attenuation) of filter


10


for different electric signals was 1530 nm, 1550 nm and 1570 nm. Therefore the center wavelength of filter


10


, according to the embodiment, is changed by varying the frequency of the electric signal which is applied to acoustic wave generator


24


.




As described above, since there are a plurality of cladding modes in first region


36


the core mode can be coupled to several cladding modes.

FIG. 14

is a graph showing the center wavelength of filter


10


according to the embodiment of the invention as a function of the frequency applied to the flexural acoustic wave generator. In

FIG. 14

, straight lines


71


,


72


and


73


represent the center wavelength of filter


10


resulting from the coupling of a core mode with three different cladding modes.




Referring to

FIG. 14

, there are three applied frequencies for any one optical wavelength in this case. Therefore the input signal light is converted to a plurality of cladding modes by applying multi-frequency electric signal to acoustic wave generator


24


. Moreover, it means transmission characteristics of filter


10


can be electrically controlled by adjusting the amplitude and each frequency component of the electric signal.




As shown in FIG.


15


(


a


), the respective transmission features


74


,


75


and


76


of filter


10


can be provided by applied electric signals with different frequencies f


1


, f


2


and f


3


. In this example, assuming that f


1


couples the core mode of input signal light to a cladding mode (cladding mode A), f


2


couples the core mode to other cladding mode (cladding mode B) and f


3


couples the core mode to another cladding mode different from A or B (cladding mode C, the transmission feature is shown in FIG.


15


(


b


) as a curve


77


when electric signal with three frequency components fl, f


2


and S is applied to acoustic wave generator


24


.




As shown in FIG.


5


(


c


), if filter


10


has transmission feature curves


78


,


79


and


80


corresponding to respective frequencies f


1


′, f


2


′ and f


3


′ and electric signal having three frequency components f


1


′, f


2


′ and f


3


′ is applied to the flexural acoustic wave generator, the transmission feature of filter


10


is shown as a curve


81


of FIG.


5


(


d


).




FIGS.


16


(


a


) and


16


(


b


) are graphs showing the transmittance of filter


10


according to an embodiment of the present invention, when varying electric signal having three frequency components is applied to filter


10


. When varying electric signal having a plurality of frequency components is applied to acoustic wave generator


24


various shapes of transmittance curves


82


,


83


and


84


can be obtained.




Since conventional tunable wavelength filters utilize the coupling of only two modes, the difference between a plurality of applied frequencies naturally becomes small to obtain wide wavelength band filtering feature by applying a plurality of frequencies. In this case, as described under the article “Interchannel Interference in multiwavelength operation of integrated acousto-optical filters and switches” by F. Tian and H. Herman in Journal of Light wave technology 1995, Vol. 13, n 6, pp. 1146-1154, when signal light input to a filter is simultaneously converted into same (polarization) mode by various applied frequency components, the output signal light may undesirably be modulated with frequency corresponding to the difference between the applied frequency components. However, with filter


10


the above problem can be circumvented, because the respective frequency components convert the mode of input light into different cladding modes in filter


10


.




In one embodiment, the filtering feature shown in FIG.


17


(


a


) was obtained by applying adjacent frequencies 2.239 MHz and 2.220 MHz to reproduce the result of a conventional method. The applied two frequencies were such that convert the mode of input light into the same cladding mode. Under the condition, narrow wavelength-band signal light with a center wavelength of 1547 nm was input to filter


10


to measure output light. Referring to the measurement result shown in FIG.


17


(


b


), there is an undesirable modulated signal with frequency corresponding to the difference of the two applied frequencies.




In another embodiment, when adjacent frequencies 2.239 MHz and 2.220 MHz were applied to acoustic wave generator


24


, according to the embodiment of the invention, the two frequency components convert the mode of input light into mutually different cladding modes. FIG.


17


(


c


) shows the measurement result when the same signal light as the above experiment was input to filter


10


and output light was measured. However, an undesirable modulated signal, which appeared in a conventional filter, practically disappeared as shown in FIG.


17


(


d


).




In optical communications or optical fiber sensor systems, wavelength filters are required that has a wide tuning range and are capable of electrically controlling its filtering feature.




FIG.


18


(


a


) illustrates one embodiment of a transmission spectrum of filter


10


with a 15.5-cm-long interaction length for a broadband unpolarized input light from a LED. A conventional communication fiber was used with a nominal core diameter of 8.5 μm, a cladding outer diameter of 125 μm and a normalized index difference of 0.37%. The frequency of the applied RF signal was 2.33 MHz, and the corresponding acoustic wavelength was estimated to be ˜650 μm. The three notches shown in FIG.


8


(


a


) are from the coupling to three different cladding modes with the same beat length at the corresponding wavelengths. The coupled cladding modes were the LP


11




(cl)


, the LP


12




(cl)


, and the LP


13




(cl)


modes, which was confirmed from far-field radiation patterns. The center of each coupling wavelength was tunable over >100 nm by tuning the acoustic frequency.




FIG.


18


(


b


) shows the measured and the calculated center wavelengths of the notches as a function of acoustic frequency. The fiber parameters used in the calculation for best fit with the experimental results are a core diameter of 8.82 μm, a cladding outer diameter of 125 μm, and a normalized index difference of 0.324%, in reasonable agreement with the experimental fiber parameters.




Referring again to FIG.


8


(


a


), coupling light of a given wavelength from the fundamental mode to different cladding modes requires acoustic frequencies that are separated from each other by a few hundred kilohertz. This separation is large enough to provide a wide wavelength-tuning range of almost 50 nm for each coupling mode pair without significant overlap with each other, thereby practically eliminating the coherent cross talk that is present in conventional counterparts. The tuning range is sufficient to cover the bandwidth of typical EDFA's. In one embodiment, filter


10


provides for a combination of independent tunable notch filters built into one device, and the number of involved cladding modes corresponds to the number of filters. The multifrequency acoustic signals can be generated by a single transducer, and the spectral profile of filter


10


is determined by the frequencies and amplitudes of the multiple acoustic signals.





FIG. 19

shows two examples of the configurable spectral profiles with spectral tilt, which can be used to recover the gain flatness in an EDFA with a gain tilt caused by signal saturation. In one embodiment, three cladding modes [LP


11




(cl)


, the LP


12




(cl)


, and the LP


13




(cl)


] were used and three RF signals were simultaneously applied with different voltages and frequencies adjusted for the particular profile. The 3-dB bandwidth of the individual notch was ˜6 nm with a 10-cm-long interaction length.




A complex filter profile is required to flatten an uneven EDFA gain, which exhibits large peaks with different widths around 1530 and 1560 nm. The combination of three Gaussian shaped passive filters can produce a flat gain over a 30-nm wavelength range.




As illustrated in FIG.


20


(


a


), a filter assembly of the present invention can include first and second filters


10


′ and


10


″ in series. Each filter


10


′ and


10


″ is driven by three radio frequency (RF) signals at different frequencies and amplitudes that produce acousto-optic mode conversion from the fundamental mode to different cladding modes. This approach eliminates the detrimental coherent crosstalk present in LiNbO


3


-based AOTF's. The 3-dB bandwidths of the first filter


10


′ were 3.3, 4.1, and 4.9 nm for the couplings to the cladding modes LP


12




(cl)


, the LP


13




(cl)


, and LP


14




(cl)


, respectively. For second filter″, they were 8, 8.6, and 14.5 nm for the couplings to the cladding modes, LP


11




(cl)


, the LP


12




(cl)


, and the LP


13




(cl)


respectively.




The minimum separations of notches produced by single RF driving frequency were ˜50 nm for first filter


10


′ and ˜150 nm for second filter


10


″, respectively, so that only one notch for each driving frequency falls into the gain-flattening range (35 nm). The large difference between filters


10


′ and


10


″ was due to the difference in optical fiber


12


outer diameters. The polarization splitting in the center wavelength of the notches as 0.2 nm for first filter


10


′ and ˜1.5 nm for second filter


10


″. The relatively large polarization dependence in second filter


10


″ is due mainly due to the unwanted core elliptically and residual thermal stress in optical fiber


12


, that can be reduced to a negligible level by using a proper optical fiber. First and second filters


10


′ and


10


″ were used for the control of the EDFA gain shape around the wavelengths of 1530 and 1555 nm, respectively. The background loss of the gain flattening AOTF was less than 0.5 dB, which was mainly due to splicing of different single-mode fibers used in the two AOTF's


1010


. Adjusting the frequencies and voltages of the applied RF signals provided control of the positions and depths of the notches with great flexibility. The RF's were in the range between 1 and 3 MHz.




FIG.


20


(


b


) shows a schematic of a dual-stage EDFA employing gain flattening filter


10


along with a test setup. A 10-m-long EDF pumped by a 980-nm laser diode and a 24-m-long EDF pumped by a 1480-nm laser diode were used as the first and the second stage amplifiers, respectively. The peak absorption coefficients of both EDF's were ˜2.5 dB/m at 1530 nm. Filter


10


was inserted between the two stages along with an isolator. Total insertion loss of filter


10


and the isolator was less than 0.9 dB. Six synthesizers and two RF power amplifiers were used to drive filter


10


.




Gain profiles of the EDFA were measured using a saturating signal at the wavelength of 1547.4 nm and a broad-band light-emitting diode (LED) probing signal. The saturating signal from a distributed feedback (DFB) laser diode was launched into the EDFA after passing through a Fabry-Perot filter (optical bandwidth: 3 GHz, extinction ratio: 27 dB) to suppress the sidelobes of the laser diode. The total power of the probe signal in 1520-1570-mn range was 27 dBm, which is much smaller than that of the input saturating signal ranging from 13 to 7 dBm.




FIG.


21


(


a


) shows gain profiles before and after the gain flattening for two different saturating signal powers of 13 and 7 dBm when the second-stage pump power was 42 mW. The gain excursions before flattening were larger than 5 dB. By adjusting the filter profile, flat gain profiles within 0.7 dB were obtained over 35 nm for both cases. The flat gain region is shifted slightly toward the shorter wavelength for higher gain level, which is due to the intrinsic gain characteristics of the EDF. FIG.


21


(


b


) shows filter profiles that produced the flat gain profiles shown in FIG.


21


(


a


), where Profile


1


and Profile


2


are for the cases of saturating tones of 13 and 7 dBm, respectively. For the measurements, EDFI was used as an ASE source, while the second pump diode (1480 nm) was turned off. The ASE signal leaked out of the second WDM coupler was monitored and the signals obtained when the filter was on and off were compared to yield the filter response. The attenuation coefficients for Profile


1


and Profile


2


at the saturating signal wavelength were 5.0 and 4.9 dB, respectively, and the average attenuation over the 35-nm range (1528-1563 nm) was 5 dB in both cases. The total RF electrical power consumption of the filter was less than 500 mW. Profile


2


could be obtained from Profile


1


by adjusting mainly the depths of notches, although fine adjustments of center wavelengths of notches within 0.5-nm range slightly improved the gain flatness. FIG.


21


(


c


) shows the filter profiles of first filter


10


′ and second filter


10


″ used to form Profile


1


, and also the locations of center wavelengths of six notches. By adjusting first and second filters


10


′ and


10


″ spectral profiles electronically gain flatness of <0.7 dB over 35-nm wavelength range were obtained at various levels of gain as well as input signal and pump power.




One important characteristic of filter


10


is polarization dependence. The shape of filter


10


can be dependent on the polarization state of input light. The polarization dependence originates from fiber birefringence. Fiber birefringence causes the effective propagation constant of a mode to be different between two eigen polarization states. Since the magnitude of birefringence is different from mode to mode, the fiber birefringence causes the beat length between two coupled modes to be different between the eigen polarization states, and, therefore, results in splitting of center wavelength of filter


10


for a given acoustic frequency.




FIG.


22


(


a


) illustrates the polarization dependence. Curve


90


represents the filter profile for light in one eigen polarization state, and filter profile


92


is when the input is in the other eigen state. The center wavelengths are split because of the birefringence. Moreover, since the field overlap between two coupled modes is also polarization dependent due to the birefringence, the attenuation depth can be different between filter profiles


90


and


92


.




A critical feature due to the polarization dependence is the polarization dependent loss (PDL) which is defined as the difference of the magnitude of attenuation between two eigen polarization states. Since polarization dependent loss is an absolute value, it increases with the attenuation depth. FIG.


22


(


b


) shows polarization dependent loss profile


93


associated with filter profiles


90


and


92


. In WDM communication system applications, the polarization dependent loss should be minimized. Most applications require the polarization dependent loss to be less than 0.1 dB. However, acousto-optic tunable filter


10


has exhibited a typical polarization dependent loss as large as 2 dB at 10-dB attenuation level. This is due to the large birefringence of the antisymmetric cladding modes.





FIG. 23

shows one possible configuration that can reduce the inherent polarization dependent loss of filter


10


. In

FIG. 23

, double-pass filter


100


consists of a 3-port circulator with input-, middle-, and output-port fibers,


12


′,


12


″ and


12


″′, respectively, and Faraday rotating mirror (FRM)


104


. The middle-port fiber


12


″ is connected to acousto-optic tunable filter


10


and Faraday rotating mirror


104


. When light comes in through input-port fiber


12


′, it is directed to filter


10


, through circulator


102


, and then refracted by Faraday rotating mirror


104


. Faraday rotating mirror


104


acts as a conjugate mirror with respect to optical polarization states. So, if the light pass through filter


10


in a specific polarization state, then on the way back after reflection it pass through filter


10


in its orthogonal polarization state. Since the light pass through filter


10


twice but in mutually orthogonal states, the total attenuation after the double pass becomes polarization-insensitive. Another benefit of the double pass configuration is that, since the filtering takes place twice in filter


10


, the drive RF power applied to filter


10


to obtain a certain attenuation depth is reduced half compared to single-pass configuration as in FIG.


4


. For instance, when filter


10


is operated at an attenuation depth of 5 dB, the overall attenuation depth of double-pass filter


100


becomes 10 dB.




Another embodiment of a device configuration for low polarization dependence is shown in FIG.


24


. In this embodiment, dual filter


110


consists of filters


10


′ and


10


″ in tandem and connected through mid fiber section


112


. Filters


10


′ and


10


″ are preferably operated at the same RF frequency. The birefringence of mid fiber section


112


is adjusted such that it acts as a half-wave plate aligned with 45-degree angle with respect to the eigen polarization axes of filters


10


′ and


10


″. In other words, the light passing through filter


10


′ in one eigen polarization state enters filter


10


″ in the other eigen polarization state. If the polarization dependent loss is the same loss for filters


10


′ and


10


″, the overall attenuation after passing through filters


10


′ and


10


″ becomes polarization-insensitive. If filters


10


′ and


10


″ are not identical in terms of polarization dependent loss, the double filter


110


would exhibit residual polarization dependent loss that should be, however, smaller than the polarization dependent loss of individual filters,


10


′ or


10


″. Therefore, it is desirable that filters


10


′ and


10


″ are identical devices. Since the filtering takes place by two filters, the drive powers to individual filters are reduced, compared to using a single filter alone, to achieve the same attenuation depth.




In one embodiment, illustrated in

FIG. 23

, circulator


102


based on magneto-optic crystal has overall insertion loss and polarization dependent loss of 1.5 dB and 0.5 dB, respectively. Faraday rotating mirror


104


has insertion loss and polarization dependent loss of 0.5 dB and 0.5 dB, respectively. Curve


120


in FIG.


24


(


a


) shows the polarization dependent loss profile in one embodiment when filter


10


was operated to produce 10-dB attenuation at 1550 nm. The filter profile in this instance is shown by curve


124


in FIG.


24


(


b


). Optical fiber


12


used in the filter was a conventional communication-grade single mode fiber. When the filter was used in the double-pass configuration, the overall polarization dependent loss was reduced greatly as shown by curve


121


in FIG.


24


(


a


).




The polarization dependent loss was reduced down to less than 0.2 dB. The total insertion loss of double-pass filter was 3 dB, mainly due to the circulator and splices. In this embodiment, the drive power to filter


10


required to produce total 10-dB attenuation at 1550 nm, as shown by filter profile


125


in FIG.


24


(


b


), was decreased compared to the single-pass filter experiment.




In another embodiment, illustrated in

FIG. 25

, two filters were fabricated with a conventional circular-core single mode fiber. Each filter was operated with 5-dB attenuation at the same center wavelength, 1550 nm. The overall dual filter profile is shown by curve


126


in FIG.


24


(


b


). In these filters, the eigen polarization states are linear and their axes are parallel and orthogonal to the direction of the flexural acoustic wave vibration or the acoustic polarization axis. This is generally true with filters made of a circular-core fiber where the dominant birefringence axes are determined by the lobe orientation of the cladding mode, which is the same as the acoustic polarization axis. Linear axis orthogonal to acoustic polarization is the slow axis, and its orthogonal axis is the fast axis. In this embodiment, a polarization controller was used in mid fiber section


112


and controlled to minimize the overall polarization dependent loss of dual filter


110


.




The loss profile is shown by curve


122


in FIG.


24


(


a


). The total filter profile is shown by curve


126


in FIG.


24


(


b


). The residual polarization dependent loss as large as 0.6 dB is primarily due to different polarization dependent loss of filters


10


′ and


10


″, and could be reduced greatly if identical two filters were used.




Another important characteristic of filter


10


is the intensity modulation of an optical signal passing through the filter. One reason which gives rise to the intensity modulation of the output signal is static coupling between different modes traveling within the fiber either by microbending of fiber


12


or imperfect splices, if present. Another reason is an acoustic wave propagating backward in first region


36


by an acoustic reflection at imperfect acoustic damper


30


and fiber jacket


32


.

FIG. 26

shows an example of output signal


139


suffering from the intensity modulation by backward acoustic reflection at acoustic damper


30


. In this case, the major modulation frequency is equal to twice the acoustic frequency. The modulation depth is defined by the ratio of peak-to-peak AC voltage amplitude, V


AC


to DC voltage, V


DC


. By static mode coupling, the major modulation frequency is equal to the acoustic frequency. When both static mode coupling and backward acoustic wave are present, the intensity of the output is modulated at frequencies of both first- and second-harmonics of the acoustic frequency. The modulation depth, when smaller than 20%, is, approximately, linearly proportional to the amount of attenuation in dB scale. In most WDM communication system applications, the modulation depth is generally required to be less than 3% at 10-dB attenuation level.




In one embodiment, illustrated in

FIG. 4

, filter


10


was fabricated by using a conventional single-mode fiber. The modulation depth at 10-dB attenuation level was about 10% at both first- and second-harmonics of the acoustic frequency, as shown by curves


140


and


141


in FIG.


27


(


a


), respectively. The same filter was used as filter


10


in another embodiment, illustrated in FIG.


23


. The RF drive power to the filter was controlled to produce 10-dB attenuation depth. In the first embodiment of double-pass filter


100


, the length of fiber section


106


was selected such that the round-trip travel time of fiber section


106


is equal to a quarter of the period of the acoustic wave. In this case, the second-harmonics component of the intensity modulation can be compensated out. Curves


142


and


143


in FIG.


27


(


a


) show the modulation depth of first- and second-harmonics components, respectively. The second-harmonics was eliminated almost completely. The first-harmonics was also reduced a little, which may be attributed to imperfect length matching of fiber section


106


. In the second embodiment of double-pass filter


100


, the length of fiber section


106


was such that the optical round-trip travel time of fiber section


106


is equal to a half of the period of the acoustic wave. In this case, the first-harmonics component of the intensity modulation can be reduced. Curves


147


and


148


in FIG.


27


(


b


) show the modulation depth of first- and second-harmonics components, respectively. The first-harmonics was eliminated almost completely.




Reduction of intensity modulation can also be achieved by dual filter


110


where the length of mid fiber section


112


is selected properly. For example, if the first-harmonic modulation component is to be compensated, the length of mid fiber section


112


is such that the optical travel time from one end of section


112


to the other end is equal to a half of the period of the acoustic wave.




Referring now to

FIG. 28

, one embodiment of the present invention is a tunable VOA assembly


150


that includes a tunable VOA


152


, coupled to a tap coupler


154


, a detector


156


and an attenuator control circuit


158


that creates a local loop. A network loop is created by coupling attenuator control circuit


158


to network components in order to receive network commands. Attenuator


152


can be a liquid crystal attenuator, a MEMS device, an acoustic-optic device, a Fabry Perot device, a mechanical sliding attenuator, a magneto-optic device and the like.




Tap coupler


154


can be a fused directional coupler, a bulk optic filter, a grating positioned in a fiber, and the like. Detector


156


can be any photodetector well known to those skilled in the art.




VOA


152


couples light from a fundamental core mode of an optical fiber to a higher-order mode such as a higher order core mode or a cladding mode. The configuration of VOA


152


is preferably the same as AOTF


10


. The amount of coupling is determined by the amplitude of the acoustic wave. Transmission in the fundamental core mode is controlled by the voltage of an RF signal applied to the transducer.




Optical tap coupler


154


, optical power detector


156


, and an attenuator control circuit


158


provide a feedback loop to VOA


152


. Additionally, the feedback signal can come from other system elements, not shown, that are coupled with VOA system


150


. Control circuit


158


can include a decision circuit and an RF generator. Control circuit


158


compares the output signal power determined from the detector output with a target value required by a system operator. Control circuit


158


controls the voltage of the RF signal that goes to the transducer of VOA


152


so that the optical signal power approaches the target value.




VOA assembly


150


is suitable with single or multiple wavelength channels and/or bands, depending on the wavelength bandwidth of the AO coupling and the channel and/or band spacing. VOA assembly


150


provides broadband operation, spectral attenuation and broadband tilt adjustment. VOA assembly


150


can provide approximate flat spectral attenuation or it can provide a tilt adjustment by moving the match to one side or the other. This can require network feedback from a spectral monitor. Further, two VOA assemblies


150


can be in series, with one providing tile and the other overall attenuation.




Referring now to

FIG. 29

, a channel equalizer


159


is illustrated. When used for a single wavelength channel, VOA


152


is likely to be positioned in an optical node incorporating a demultiplexer


160


, such as an arrayed wave-guide grating (AWG) router. For example, VOA


152


can be used to equalize the powers of multiple channels and/or bands including, in particular, added channels and bands. In this case, the RF frequency for each VOA


152


is set differently according to the attenuation desired for each channel and/or band VOA


152


is to deal with. Polarization dependence of each VOA


152


is largely tolerated due to the feedback operation as long as the feedback speed is faster than the polarization fluctuations. For example, the characteristic time of SOP fluctuation in a real communication system can be on the order of a millisecond.




Demultiplexer


160


is configured to receive a plurality of different WDM channels and separate the different signals (channels) into different fibers, one fiber for each wavelength channel and/or bands. Each separate wavelength is individually attenuated with a VOA


152


. This provides individual control for each wavelength. Some of the wavelengths can be dropped and not passed to VOA's


152


. New wavelengths can be added after demultiplexer


160


. VOA's


152


provide gain flattening and also permit adding and dropping of channels and/or bands. VOA's


152


provide spectral flattening and adjust the powers so the recombined signals all have a predetermined power.




In the

FIG. 29

embodiment, a first series of VOA's


152


is positioned between the drop and add and a second series of VOA's


152


positioned after the add. A multiplexer


162


is positioned downstream from the second series of VOA's


152


. A monitor


164


is coupled to the output. Monitor


164


can provide a feedback signal that is used to adjust VOA's


152


. The embodiment of

FIG. 29

provides broadband operation, spectral attenuation, channel by channel spectral attenuation and broadband tilt adjustment.




Referring now to

FIG. 30

, one embodiment of an optical cross-connect apparatus


166


is provided. Optical cross-connect apparatus


166


provides channel routing, switching and leveling between two inputs with multiple wavelengths and two outputs of multiple wavelengths. Optical cross-connect apparatus


166


includes demultiplexer


160


, multiplexer


162


, a demultiplexer


168


and a multiplexer


170


and coupled to optical cross connect


172


which includes any number of devices to redirect wavelengths, including but not limited to mirrors and the like. Optical cross connect


172


can be made using MEMS mirrors, bubble switch technology, with liquid crystals and the like. A plurality of VOA's


152


are each coupled to an optical fiber and positioned between optical cross connect


172


and multiplexers


162


and


170


. VOA's


152


are included to individually adjust the power of individual wavelengths and achieve leveling and/or spectral grooming.




Optionally included is a monitor


174


which can be a spectral monitor and the like that monitors the spectral output. A system command device


176


is coupled to monitor


174


to receive network commands and create a feedback loop. These network commands can, (i) come from the end of the link after electrical detection and bit error rate measurements, (ii) come from spectral monitors located throughout the network and (iii) can be IP signals or proprietary signals to the local control electronics/processor. A second monitor


178


is provided at the second output. The embodiment illustrated in

FIG. 30

also provides broadband operation, spectral attenuation and channel by channel broadband spectral adjustment.




Referring now to

FIG. 31

, another embodiment of an optical cross-connect apparatus


180


includes two or more optical cross connects


172


and


182


. At least two demultiplexers


160


and


184


are provided at the input carrying WDM signals. At least two multiplexers


162


and


184


are at the output. The wavelengths are split into two groups. All of the even wavelengths are in one group and the odd wavelengths in the other group. One group is directed to optical cross connect


172


and the other group is directed to optical cross connect


182


. Thereafter, multiplexers


162


and


184


combine the different wavelengths which are directed to the different output fibers. A plurality of VOA's


152


are coupled to optical cross connects


172


and


182


. Spectral monitors


174


couple the output fibers with VOA's


152


. Amplifiers


186


can be coupled to the optical fibers carrying the WDM signals. It will be appreciated that the embodiment of

FIG. 31

can be extended to any desired number of optical cross connects, demultiplexers and multiplexers.





FIG. 32

illustrates another embodiment of the present invention. In this embodiment filter


210


includes optical fiber


212


with first region


214


and second region


216


. There is more coupling of the optical signal between modes traveling within the optical fiber in first region


214


than in second region


216


. First acoustic wave generator


218


is coupled to optical fiber


212


. First acoustic wave generator


218


produces a first acoustic wave that travels in a first direction


220


in first region


214


. In response to propagation of the first acoustic wave in first region


214


, a backward-propagating wave is created and travels in an opposite direction


222


to the first acoustic wave. A first acoustic wave propagation member


226


is coupled to optical fiber


212


. A second acoustic wave generator


228


is coupled to optical fiber


212


at second region


216


. Second acoustic wave generator


228


produces a second acoustic wave that reduces a magnitude of the backward propagating acoustic wave.




Optical fiber


212


can include a cladding and a core. An optical signal is coupled to the cladding from the core in first region


214


. A frequency of the first acoustic wave is preferably the same as the frequency of the second acoustic wave. The second acoustic wave is out of phase with the backward propagating acoustic wave. The second acoustic wave is preferably 90 to 270 degrees out of phase with the backward propagating acoustic wave, more preferably about 180 degrees out of phase.




The second acoustic wave reduces a power of the back reflection in a range of 20 to 30 db or less, more preferably 30 to 40 db or less, more preferably 40 to 50 db or less and still more preferably 50 to 60 db or less.




First acoustic wave generator


218


can produce multiple acoustic signals with individual controllable strengths and frequencies. Each of these acoustic signals provides a coupling between different modes traveling within the fiber. A wavelength of an optical signal coupled to a cladding from a core of optical fiber


212


is changed by varying the frequency of a signal applied to first acoustic wave generator


218


. An amount of an optical signal coupled to a cladding from a core of optical fiber


212


is changed by varying the amplitude of a signal applied to first acoustic wave generator


218


.




Referring now to

FIG. 33

, a feedback loop


230


is coupled to a feedback and processing unit


231


which is coupled to one or more second acoustic generators


228


. By looking at the various second harmonic signals, feedback signals can be calculated at feedback and processing unit


231


and sent to each second acoustic generator


228


to remove substantially all of the second harmonic intensity modulation.




As illustrated in

FIG. 34

, filter


210


can also include an acoustic damper


232


coupled to non-interaction region


216


. In this embodiment, acoustic damper


232


has a proximal end


233


with a sufficient taper configuration that reduces a power of the backward-propagating wave in a range of 20 to 30 dB or less, preferably 30 to 40 dB or less, more preferably 40 to 50 dB or less and still more preferably 50 to 60 dB or less.




Referring now to

FIG. 35

, second acoustic wave generator


228


is coupled to acoustic damper


232


. In this embodiment, acoustic damper


232


need not have the selected tapered configuration. Second acoustic wave generator


228


produces the second acoustic wave that reduces the magnitude of the backward propagating acoustic wave. Additionally, acoustic damper


232


can have the tapered configuration in order to help reduce the magnitude of the backward propagating acoustic wave.




In another embodiment of the present invention, illustrated in FIG.


36


(


a


), a filter


310


includes optical fiber


312


with a cladding


316


surrounding a core


314


and a core-mode blocker


317


included in at least a portion of first region


336


of optical fiber


312


. A mode coupler


318


is coupled to optical fiber


312


. A mode coupler


318


couples a first mode to a different spatial mode in a forward direction of optical fiber


312


. A second mode coupler can be included. Mode coupler


318


can be an acoustic wave propagation member such as an acoustic grating, a UV grating, a bending grating, a stress induced grating and the like.




Core-mode blocker


317


absorbs or scatters a first mode in core


314


and passes other spatial modes that travel in fiber


312


including but not limited to core to cladding, cladding to core, polarization to polarization, multiple cladding modes, and the like.




Core-mode blocker


317


can be integrally formed as a portion of optical fiber


312


. In various embodiments, core-mode blocker


317


can be, voids in optical fiber


312


, a region of core


314


that has been damaged by high intensity light, a region of core


314


that has been damaged by etching a portion of core


314


followed by resplicing, a region of core


314


that has been damaged by UV light or a region of optical fiber


312


that has been spliced with an absorbing core region, positioning a reflector over the core region and the like.




Optionally, core-mode blocker


317


can include a fiber Bragg grating or a grating that scatters core light into cladding


316


. Additionally, the scattered light can also be reflected back into the core and an isolator minimizes the reflected light from going back into filter


310


. In various embodiments, core mode blocker


317


can have lengths of 5 cm or less, 2 cm or less, 1 cm or less and 5 mm or less. core-mode blocker has a length of 5 cm or less.




Additionally, in various embodiments, core mode blocker


317


provides an attenuation of at least 50 dB, 40 dB, 30 dB, 20 dB or at least 10 dB.




FIG.


36


(


b


) illustrates one method for making filter


310


with a two single mode fibers (“SMF”) etched in HF. The cores are etched more than the claddings in FIG.


36


(


c


). The SMF pair made by this process are then spliced (FIG.


36


(


d


)) and a bubble with an approximate size of 10 μm is made at the splicing point. The cladding mode undergoes a small loss at core mode blocker


317


as compared to the fundamental mode LP01 in the guided modes of optical fiber


312


.




FIGS.


37


(


a


)-(


d


) illustrate the spectra at the core mode and the cladding mode at positions “A”, “B”, “C”, and “D” of filter


310


illustrated in FIG.


36


(


d


). The solid line represents the core mode and the dot line represents the cladding mode.




Light which does not satisfy the phase matching condition is propagated as the core mode in length L with the large loss illustrated in FIGS.


37


(


b


) and


37


(


c


). The cladding mode at the C position propagates length L and is re-coupled into the core mode by the acoustic wave in filter


317


. FIG.


37


(


d


) illustrates that filter


317


with core mode blocker


317


operates as a bandpass filter. If the frequency of an electric signal supplied at acoustic wave generator


324


is changed, the acoustic wavelength is changed in the phase matching condition. Wavelengths transmitted with filter


310


are thus tunable.





FIG. 38

illustrates the measured transmission spectrum of filter


310


. By way of illustration, but without limitation to specific numbers, the acoustic frequency driven to acoustic wave generator


324


was 1.56 MHz and the 3 dB bandwidth ˜3.8 nm at 18 cm-interaction length.





FIG. 39

shows the variation of the transmitted wavelength of filter


310


according to the acoustic frequency. The extinction at filter


310


is the transmission ratio between the transmission wavelength and the non-transmission wavelength and is the difference between those in a log scale. With filter


310


the extinction is mainly dependent on the core mode loss at core mode blocker


317


. Large extinction can be created by cascading core mode blockers


317


.




As shown in

FIG. 40

, one embodiment of the present invention includes at least one long period grating


411


which is used to couple between forward propagating modes. Long period grating


411


can have a length in the range of 10 microns to 10 cm. Long period grating


411


can be impressed into the core of optical fiber


412


to phase-match the transfer of light between core and other spatial modes. As the length of long-period grating


411


increases, the intensity of light remaining in the fiber core varies periodically. It will be appreciated that other gratings including but not limited to UV induced gratings, bending induced gratings and the like, can also be utilized. A mode coupler


418


is also coupled to optical fiber


412


.




In this embodiment, light that is coupled from the core mode to the cladding mode and then returned to the core mode by long period grating


411


. Light that propagates in the core mode of filter


410


is coupled to the cladding mode by long period grating


411


.




In one embodiment, filter


410


has two identical long-period gratings


411


of equal length with core mode blocker


417


between the two gratings. For resonant wavelengths the first long-period grating


411


couples light out of the core into the cladding. All non-resonant wavelengths encounter core mode blocker


417


and are extinguished. However, the resonant wave-lengths travel around core mode blocker through the cladding and are then transferred back into the core by second long-period grating


411


.




In the region between two long-period gratings


411


a core mode blocker


417


is created so that only light that is detected by both gratings


411


passes through filter


410


. The cladding then acts as a bypass around core mode blocker


417


, but only for those wavelengths that are resonant with both long-period gratings


411


. By perturbing the cladding of fiber


412


in the region between the long period gratings


411


the amplitude of light transmitted through the filter


410


can be modulated.




The foregoing description of a preferred embodiment of the invention has been presented for purposes of illustration and description. It is not intended to be exhaustive or to limit the invention to the precise forms disclosed. Obviously, many modifications and variations will be apparent to practitioners skilled in this art. It is intended that the scope of the invention be defined by the following claims and their equivalents.



Claims
  • 1. An optic apparatus, comprising:an optical fiber with a cladding surrounding a core, and an interactive region having a core-mode blocker; and a mode coupler affixed to the optical fiber that couples a first mode to a different spatial mode in a forward direction of the optical fiber, the interaction region being a region of the optical fiber where an optical signal that propagates through the optical fiber interacts with an acoustic wave from the mode coupler.
  • 2. The apparatus of claim 1, further comprising:a second mode coupler affixed to the optical fiber, the second mode coupler configured to couple the second mode back to the first mode.
  • 3. The apparatus of claim 1, wherein the mode coupler is selected from an acoustic grating, a UV grating, a bending grating and a stress induced grating.
  • 4. The apparatus of claim 1, wherein the mode coupler includes an acoustic wave generator affixed to optical fiber that produces the acoustic wave traveling in the forward direction, and an acoustic wave propagation member affixed to the optical fiber.
  • 5. The apparatus of claim 1, wherein the core-mode blocker absorbs or scatters the first mode and passes other spatial modes that travel in the fiber.
  • 6. The apparatus of claim 1, wherein the core-mode blocker passes light in the cladding and the acoustic wave, and absorbs or scatters light in the core.
  • 7. The apparatus of claim 1, wherein the core-mode blocker includes voids.
  • 8. The apparatus of claim 1, wherein the core-mode blocker is a region of the core that has been damaged by high intensity light.
  • 9. The apparatus of claim 1, wherein the core-mode blocker is a region of the core that has been damaged by etching a portion of the core and then resplicing.
  • 10. The apparatus of claim 1, wherein the core-mode blocker is a region of the core that has been damaged by UV light.
  • 11. The apparatus of claim 1, wherein the core-mode blocker is a region of the optical fiber that has been spliced with an absorbing core region.
  • 12. The apparatus of claim 1, wherein the core-mode blocker includes a fiber Bragg grating.
  • 13. The apparatus of claim 1, wherein the first mode is a core mode and the different spatial mode is a cladding mode.
  • 14. The apparatus of claim 1, wherein the first mode is a cladding mode and the different spatial mode is a core mode.
  • 15. The apparatus of claim 1, wherein the core-mode blocker includes a grating that scatters or absorbs core light into the cladding.
  • 16. The apparatus of claim 1, wherein the core-mode blocker has a length of 5 cm or less.
  • 17. The apparatus of claim 1, wherein the core-mode blocker has a length of 2 cm or less.
  • 18. The apparatus of claim 1, wherein the core-mode blocker has a length of 1 cm or less.
  • 19. The apparatus of claim 1, wherein the core-mode blocker has a length of 5 mm or less.
  • 20. The apparatus of claim 1, wherein the core-mode blocker is integrally formed as a portion of the optical fiber.
  • 21. The apparatus of claim 1, wherein the core-mode blocker provides an attenuation of at least 50 dB.
  • 22. The apparatus of claim 1, wherein the core-mode blocker provides an attenuation of at least 40 dB.
  • 23. The apparatus of claim 1, wherein the core-mode blocker provides an attenuation of at least 30 dB.
  • 24. The apparatus of claim 1, wherein the core-mode blocker provides an attenuation of at least 20 dB.
  • 25. The apparatus of claim 1, wherein the core-mode blocker provides an attenuation of at least 10 dB.
  • 26. The apparatus of claim 1, wherein a portion of the optical signal is coupled to the cladding from the core in the interactive region.
  • 27. The apparatus of claim 1, wherein the mode coupler includes an acoustic wave generator that produces multiple acoustic signals with individual controllable strengths and frequencies, each of the acoustic signals providing a coupling between different spatial modes traveling within the fiber.
  • 28. The apparatus of claim 1, wherein the mode coupler includes a temperature controlled grating that is temperature tunable.
  • 29. The apparatus of claim 1, wherein the mode coupler includes a stress induced grating that is temperature tunable.
  • 30. The apparatus of claim 1, wherein the mode coupler includes an acoustic wave generator that produces longitudinal waves.
  • 31. The apparatus of claim 1, wherein the mode coupler includes an acoustic wave generator that produces torsional waves.
  • 32. The apparatus of claim 1, wherein the mode coupler includes an acoustic wave generator that produces transverse waves.
  • 33. The apparatus of claim 1, wherein the mode coupler includes an acoustic wave generator and a wavelength of an optical signal coupled between two different modes traveling within the optical fiber is changed by varying the frequency of a signal applied to the acoustic wave generator.
  • 34. The apparatus of claim 1, wherein the mode coupler includes an acoustic wave generator and an amount of an optical signal coupled between two different modes traveling within the optical fiber is changed by varying the amplitude of a signal applied to the acoustic wave generator.
  • 35. An optic apparatus, comprising:an optical fiber with a cladding surrounding a core and an interactive region having a core-mode blocker; and a mode coupler affixed to the optical fiber that couples a first mode to a different spatial mode in a forward direction of the optical fiber, the interaction region being a region of the optical fiber in which an optical signal that propagates through the optical fiber interacts with acoustic waves from the mode coupler; and a Faraday mirror affixed to the optical fiber.
  • 36. The apparatus of claim 35, further comprising:a circulator, wherein the mode coupler is positioned between the circulator and the Faraday mirror.
  • 37. The apparatus of claim 35, further comprising:a second mode coupler affixed to the optical fiber, the second mode coupler configured to couple the second mode back to the first mode.
  • 38. The apparatus of claim 35, wherein the mode coupler is selected from an acoustic grating, a UV grating, a bending grating and a stress induced grating.
  • 39. The apparatus of claim 35, wherein the mode coupler includes an acoustic wave generator affixed to optical fiber that produces an acoustic wave traveling in the forward direction, and an acoustic wave propagation member affixed to the optical fiber.
  • 40. The apparatus of claim 35, wherein the core-mode blocker absorbs or scatters the first mode and passes other spatial modes that travel in the fiber.
  • 41. The apparatus of claim 35, wherein the core-mode blocker passes light in the cladding and the acoustic wave, and absorbs or scatters light in the core.
  • 42. The apparatus of claim 35, wherein the core-mode blocker includes voids.
  • 43. The apparatus of claim 35, wherein the core-mode blocker is a region of the core that has been damaged by high intensity light.
  • 44. The apparatus of claim 35, wherein the core-mode blocker is a region of the core that has been damaged by etching a portion of the core and then resplicing.
  • 45. The apparatus of claim 35, wherein the core-mode blocker is a region of the core that has been damaged by UV light.
  • 46. The apparatus of claim 35, wherein the core-mode blocker is a region of the optical fiber that has been spliced with an absorbing core region.
  • 47. The apparatus of claim 35, wherein the core-mode blocker includes a fiber Bragg grating.
  • 48. The apparatus of claim 35, wherein the first mode is a core mode and the different spatial mode is a cladding mode.
  • 49. The apparatus of claim 35, wherein the first mode is a cladding mode and the different spatial mode is a core mode.
  • 50. The apparatus of claim 35, wherein the core-mode blocker includes a grating that scatters or absorbs core light into the cladding.
  • 51. The apparatus of claim 35, wherein the core-mode blocker has a length of 5 cm or less.
  • 52. The apparatus of claim 35, wherein the core-mode blocker has a length of 2 cm or less.
  • 53. The apparatus of claim 35, wherein the core-mode blocker has a length of 1 cm or less.
  • 54. The apparatus of claim 35, wherein the core-mode blocker has a length of 5 mm or less.
  • 55. The apparatus of claim 35, wherein the core-mode blocker is integrally formed as a portion of the optical fiber.
  • 56. The apparatus of claim 35, wherein the core-mode blocker provides an attenuation of at least 50 dB.
  • 57. The apparatus of claim 35, wherein the core-mode blocker provides an attenuation of at least 40 dB.
  • 58. The apparatus of claim 35, wherein the core-mode blocker provides an attenuation of at least 30 dB.
  • 59. The apparatus of claim 35, wherein the core-mode blocker provides an attenuation of at least 20 dB.
  • 60. The apparatus of claim 35, wherein the core-mode blocker provides an attenuation of at least 10 dB.
  • 61. The apparatus of claim 35, wherein a portion of the optical signal is coupled to the cladding from the core in the interactive region.
  • 62. The apparatus of claim 35, wherein the mode coupler includes an acoustic wave generator that produces multiple acoustic signals with individual controllable strengths and frequencies, each of the acoustic signals providing a coupling between different spatial modes traveling within the fiber.
  • 63. The apparatus of claim 35, wherein the mode coupler includes a temperature controlled grating that is temperature tunable.
  • 64. The apparatus of claim 35, wherein the mode coupler includes a stress induced grating that is temperature tunable.
  • 65. The apparatus of claim 35, wherein the mode coupler includes an acoustic wave generator that produces longitudinal waves.
  • 66. The apparatus of claim 35, wherein the mode coupler includes an acoustic wave generator that produces torsional waves.
  • 67. The apparatus of claim 35, wherein the mode coupler includes an acoustic wave generator that produces transverse waves.
  • 68. The apparatus of claim 35, wherein the mode coupler includes an acoustic wave generator and a wavelength of an optical signal coupled between two different modes traveling within the optical fiber is changed by varying the frequency of a signal applied to the acoustic wave generator.
  • 69. The apparatus of claim 35, wherein the mode coupler includes an acoustic wave generator and an amount of an optical signal coupled between two different modes traveling within the optical fiber is changed by varying the amplitude of a signal applied to the acoustic wave generator.
Priority Claims (1)
Number Date Country Kind
97-24796 Jun 1997 KR
CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a continuation-in-part of Ser. No. 09/729,661 filed Dec. 4, 2000, pending, which is a continuation-in-part of Ser. No. 09/666,763 filed Sep. 21, 2000, pending, which application is a continuation-in-part of and claims the benefit of priority from Provisional Patent Application Ser. No. 60/206,767, filed May 23, 2000, Ser. No. 09/666,763 pending, also being a continuation in part of Ser. No. 09/571,092 filed May 15, 2000, now U.S. Pat. No. 6,253,002, which is a continuation of Ser. No. 09/425,099 filed Oct. 22, 1999, now U.S. Pat. No. 6,233,379, which is a continuation-in-part of Ser. No. 09/022,413 filed Feb. 12, 1998, now U.S. Pat. No. 6,021,237, which claims priority to KR 97-24796 filed Jun. 6, 1997, all of which applications are fully incorporated herein by reference.

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6266462 Kim et al. Jul 2001 B1
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Provisional Applications (1)
Number Date Country
60/206767 May 2000 US
Continuations (2)
Number Date Country
Parent 09/729661 Dec 2000 US
Child 09/765971 US
Parent 09/425099 Oct 1999 US
Child 09/571092 US
Continuation in Parts (3)
Number Date Country
Parent 09/666763 Sep 2000 US
Child 09/729661 US
Parent 09/571092 May 2000 US
Child 09/666763 US
Parent 09/022413 Feb 1998 US
Child 09/425099 US