Abstract:
Faraday rotator or isolator with mode stripping ferrules and collimators having fiber pigtailed mode stripping components. An example is a compact Faraday Isolator module employing mode stripping ferrules and mode stripping collimators at the input and/or at the output of a fiber pigtailed Faraday Isolator. Two basic isolator types are a Polarization Independent Faraday isolator and a Polarization Maintaining Faraday isolator. The device is substantially immune to damage due to back-reflection, thermal lensing, energy leakage and absorption. Mode stripped optical energy propagating in the reverse direction is diverted onto a heat absorbing and heat sinking structure, as for example at the input of a compact birefringent wedge-based PI isolator. Alternatively, the optical energy propagating in the reverse direction is angularly refracted away from the forward incident beam path and is coupled into the energy dispersive cladding of the input fiber or the ferrule itself.

Description:
CROSS-REFERENCES TO RELATED APPLICATIONS 
       [0001]    NOT APPLICABLE 
       STATEMENT AS TO RIGHTS TO INVENTIONS MADE UNDER FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT 
       [0002]    NOT APPLICABLE 
       REFERENCE TO A “SEQUENCE LISTING,” A TABLE, OR A COMPUTER PROGRAM LISTING APPENDIX SUBMITTED ON A COMPACT DISK 
       [0003]    NOT APPLICABLE 
       BACKGROUND OF THE INVENTION 
       [0004]    This invention relates to Faraday rotators and particularly Faraday isolators for use with high power lasers. Faraday isolators capable of withstanding high power are required to decouple high power laser sources from reflective targets. Reflections can damage the laser and/or cause it to operate erratically. Lasers used in industrial metalworking applications are particularly prone to reflections from metal work-pieces. For example, metal targets can couple nearly 100% of the incident radiation back into industrial 1 μm laser sources. 
         [0005]    Optical fiber is particularly useful for delivering high power laser radiation in industrial environments. It is sealed from dust and other contaminants. It is flexible, durable and lightweight. Fiber lasers are particularly efficient laser sources for high power industrial use. A fiber laser can be readily coupled to an optical fiber. It is therefore desirable to mate optical fiber to high power Faraday isolators. 
         [0006]    Laser radiation guided within optical fiber is converted into a free space beam when used with a Faraday isolator. This is often achieved by allowing laser radiation emanating from the core of an optical fiber termination to diverge to the desired size and then collimating this radiation into a beam with a lens. Such a combination of elements is called a fiber collimator. The free space beam out of a first fiber collimator is then transmitted through a Faraday isolator where it may be further directed onto a target directly or it may be re-coupled back into a second fiber collimator for fiber beam delivery. Faraday isolators used with one or more fiber collimators are often described as fiber pigtailed Faraday isolators. 
         [0007]    Faraday isolators which are fiber pigtailed on the input and output have been widely used for low power applications, such as fiber optic telecommunications. In such devices radiation transmitted in the forward direction which does not couple into the core of the output fiber is of such low power that it cannot damage anything in the fiber collimator structure. With high power lasers however, the optical radiation (e.g., IR light) which does not couple into the core of the output collimator either couples into the surrounding cladding layer, from which it ultimately diverges and readily burns the optical fiber polymer protective coating layer, thereby destroying the fiber, or it destroys the fiber collimator if it strikes any adhesives which hold the fiber in alignment. This is a practical problem for fiber pigtailed high power Faraday isolators because Faraday isolators are used at wavelengths near an absorption peak where there is always a residual absorption. This is done because Faraday Rotation greatly increases near an absorption, allowing the Faraday isolator to be smaller and less expensive. This residual absorption leads to a temperature gradient across the beam profile within the Faraday optical material, the magnitude of which increases with increasing laser power. This thermal profile leads to two thermal effects within the Faraday optic: thermal lensing and thermal birefringence. For substantially round laser beams, the thermal gradient is parabolic and acts, to first order, as a spherical lens. Increasing the beam size through the Faraday optic can reduce this thermal lensing, but it does so at the expense of making the device bulkier. The thermal lens changes the beam parameters such that optical radiation from a first fiber collimator does not completely couple into the core of a second fiber collimator at all laser operating powers. Thermal birefringence changes polarization states emanating from a first (input) fiber collimator as they propagate through the Faraday isolator. These changed polarization states will also not couple efficiently into the core of a second (output) fiber collimator. Therefore, a structure is desired which does not lead to damage in the presence of thermal effects in a high power fiber pigtailed Faraday isolator. 
         [0008]    There are two types of Faraday isolators used with lasers: Polarization Maintaining (“PM”) isolators and Polarization Insensitive (“PI”) isolators. PM isolators are used with laser sources which have output radiation that is polarized. They require linear polarizers at the input and output joining a 45° Faraday Rotator. Fiber pigtailed PM isolators have been used with PM fiber which maintains the launched linear polarization into, and out of, the linear polarizers of the PM Faraday isolator. For low power operation the linear polarizers can be absorptive type polarizers such as Corning Polarcor™ polarizer (Corning Glass Works of Corning, N.Y.) or scattering/mode stripping fiber types exemplified by Corning Single Polarization Fiber or Crystal Fibre LMA PZ 20 Large Mode Area Polarizing Fiber (Crystal Fibre of Birkerod, Denmark). Polarcor is a thin (typically 0.5 mm) glass plate polarizer that absorbs any polarization component orthogonal to the polarization transmission axis. Corning Single Polarization Fiber, for example, rejects any component of radiation polarized orthogonal to the transmission axis into the cladding where it is ultimately stripped in the polymer protective coating. Typically lengths of one hundred centimeters or more are required to ensure highly linear polarization. Because it can be fusion spliced to commonly used PM fiber, this structure is of a form that is convenient for robust, compact, low power isolators. 
         [0009]    However, these types of polarizers function by absorbing or scattering the undesired polarization component. Thus, they are readily prone to failure if the same designs are employed for high power applications. In contrast, for high power operation, the linear polarizers are typically polarizing beam-splitter cubes or Brewster-angle thin film polarizers. Any polarization component orthogonal to the transmission axis of such polarizers is angularly rejected away from the beam path. Because the rejected polarization means that energy is directed away from the beam path, such polarizers are located outside of the magnet body so that the rejected radiation can be directed onto a beam dump. This design has in the past required that the size of the Faraday isolator be even larger than for low power applications. A robust, compact, fiber pigtailed Polarization Maintaining Faraday isolator suitable for use with high power lasers is desired. 
         [0010]    Polarization Insensitive Faraday isolators are useful with lasers sources which are unpolarized or randomly polarized. There are two common ways to construct PI isolators. The first approach, as for example disclosed in U.S. Pat. No. 4,178,073, is the use of a birefringent crystal beam displacer to split a laser beam into two distinct beams of orthogonal polarization. In operation the device transmits the beams first through 45° of non-reciprocal Faraday rotation and then through 45° of reciprocal optical rotation (using a quartz rotator or waveplate), and finally recombines the two beams in a second beam displacer. A disadvantage of this approach is that the effective aperture size of the Faraday isolator is typically doubled in order to transmit both orthogonally polarized beams. The result is that an already bulky magnetic encasement must be even larger. Furthermore, common birefringent beam displacers have lengths which are approximately ten times as large as the laser beam diameter. For high power laser application where it is desired to increase the laser beam size to reduce thermal lensing, the indicated size of such beam displacers is very large and difficult to fabricate with high optical quality. Even so, such bulky designs have found wide usage in industrial settings with fiber pigtailing because any reflected power back into the isolator is blocked by physical beam blocks rather than being coupled back into the input fiber collimator where damage could occur. 
         [0011]    The second basic approach, which is used to achieve Polarization Independent Faraday Isolation as disclosed in U.S. Pat. No. 4,548,478, is to use birefringent wedges. In a common design, laser light from an input fiber collimator is directed through an input birefringent wedge. The orthogonally polarized birefringent axes define two different refractive indices which refract the two polarizations into slightly different angles. The 45° of Faraday rotation then rotates the polarization axis into that of a second, output birefringent wedge if the second wedge also has its birefringent axis rotated 45° to the input wedge polarization axis. In such a PI isolator, if a second wedge is also oriented at the output in a flipped mirror image to the input wedge about a reflection axis through the middle of the Faraday isolator, then the orthogonally polarized beams exit the output wedge in parallel with one another, but displaced by a small amount, with low transmission loss. With such an approach any reflected light back into the Faraday isolator is given an additional, non-reciprocal, 45° of Faraday rotation such that the backward propagating polarization states are rotated 90° at the input birefringent wedge. The input wedge then refracts the two backward propagating polarization states away from the input beam path by a small angle (on the order of 1-2°). 
         [0012]    Low power fiber pigtailed isolators used for telecom applications in the wavelength range of 1.5 μm typically use highly efficient, low absorption Faraday rotators such as Bismuth Iron Garnet (“BIG”) that can achieve 45° of Faraday rotation in a few millimeters or less. Because the Faraday rotation occurs in such a short length, the small angular deviation through the “BIG” optic after the first birefringent wedge (on the order of 4°) does not require the aperture size of the Faraday isolator to significantly increase beyond the beam size. For this reason birefringent wedge based PI isolator designs are more compact and less expensive than beam displacer based PI isolator designs at telecom wavelengths. Fiber pigtailed PI isolators using birefringent wedges have been the dominant basic form used at low powers. 
         [0013]    However, at typical high power laser wavelengths, 1 μm for example, Terbium Gallium Garnet (“TGG”) is a common Faraday optic material. TGG is a much less efficient Faraday optic material than BIG, which cannot be used at such wavelengths due to a strong absorption. For high magnetic fields, on the order of 10,000 gauss, approximately 2 cm of TGG is required for 45° rotation at 1065 nm. In this case, the small angular deviation in birefringent wedge-based PI isolator designs through the approximately 2 cm TGG optic requires the magnet aperture size to be increased. This significantly increases the size of the overall package. It is further desired to have the original input beam path restored after traversing all optics to simplify alignment and maximize coupling efficiency from fiber to fiber. Additionally, in numerous instances it is desired to have a fiber pigtailed input and a free space output beam. In such usage, it is desired to have the two polarization components of the PI isolator perfectly overlapped at the output in order to achieve minimum focused spot size at the workpiece. Hosokawa in U.S. Pat. No. 5,408,354 discloses the use of a birefringent crystal plane plate beam displacer to bring the two polarization component beams out of first and second birefringent elements to converge the two polarization components back into coincidence. Although the output beam path as disclosed is parallel to the input beam path, it is however displaced from the input beam axis—which causes the magnet aperture size to increase. All of the factors listed above increase the magnet aperture size of birefringent wedge based designs when used with high power Faraday optic materials. This diminishes the potential size and cost benefits which birefringent wedge based PI isolator designs have over a bulky beam displacer based approach. A birefringent wedge based fiber pigtailed PI isolator design for high power applications which maintains the beam path through the Faraday isolator and does not require the magnet aperture size to increase is desired. 
         [0014]    In fiber pigtailed PI isolators in lower power applications, the isolated power directed into the cladding layer and stripped by the polymer coating is well below the threshold for material damage. However at average power levels as low as 10 W, such isolated power can damage the protective polymer coating of the input fiber. Thus, fiber pigtailed birefringent wedge based PI isolators have not been considered suitable for high-power applications. 
         [0015]    What is needed is a compact Faraday isolator for high power applications, and in particular an inherently small PI Faraday isolator, such as a fiber pigtailed Faraday isolator that does not require an enlarged clear aperture and resists internal damage at high power. 
       SUMMARY OF THE INVENTION 
       [0016]    According to the invention, mode stripping fiber ferrules and collimators are combined in a compact Faraday isolator module. The Faraday isolator module employs mode stripping ferrules and/or mode stripping collimators at the input and at the output of a fiber pigtailed Faraday isolator. Mode stripping ferrules are fiber terminations which safely remove radiation in cladding modes, as well as other radiation that cannot be guided by the fiber core away from the fiber, before such radiation can damage any protective coating or jacket surrounding the optical fiber. For use at high power, mode stripping ferrules usually have a section of undoped fiber (an “endcap”) to allow radiation emanating from, or entering into, the fiber core to be of larger beam size so as not to cause surface damage at the ferrule/air interface. The ferrule endface may be angled and is usually anti-reflection coated. Mode stripping collimators are either mode stripping ferrules mated to discrete lenses to form a collimated beam or mode stripping ferrules with a lens formed directly onto the end of the endcap of the ferrule. Mode stripping ferrules and collimators are capable therefore of safely removing optical energy launched into the cladding due to thermal lensing/birefringence before it can damage the fiber. The resulting fiber pigtailed Faraday isolator is suitable for high power applications, being substantially immune to damage due to back-reflection, thermal lensing, thermal birefringence, energy leakage and absorption. 
         [0017]    Two basic isolator types can be fabricated according to the invention: a Polarization Maintaining (PM) Faraday isolator and a Polarization Independent (PI) Faraday isolator. In particular embodiments, mode stripped laser power is directed onto a heat absorbing and heat sinking strain relief structure, as for example at the input of a compact birefringent wedge based PI isolator. In operation of such a device, optical energy propagating in the reverse or isolation direction is angularly refracted away from the forward incident beam path and is coupled into the cladding of the input fiber or the ferrule itself. Alternatively, the optical energy is intentionally reflected and/or scattered away from the fiber onto, for example, an absorbing heat sink. 
         [0018]    An advantage of the invention is the realization of compact Polarization Maintaining Faraday isolators that are also low cost and robust. In addition to stripping any cladding modes due to thermal effects, the mode stripping elements, namely ferrules/collimators, strip the polarization scattered into the cladding by the single polarization fiber. The length of the mode stripping ferrule is chosen such that the rejected polarization power is safely below the threshold for material damage in the fiber polymer protective coating. 
         [0019]    Beyond the examples of a mode stripping ferrules described herein, there are other suitable ferrule designs, as for example described in U.S. patent application Ser. No. 11/338,429 filed Jan. 23, 2006, entitled Monolithic Mode Stripping Ferrule, and assigned to the same assignee as the present application. The content of that disclosure is incorporated herein by reference for all purposes. 
         [0020]    A further aspect of the present invention is the arrangement by proper tilting of the surfaces of the birefringent wedges relative to the Faraday optic such that the original beam path and the initial beam parameters of a laser beam are restored so it is along a reasonably straight and narrow path through a passage in the magnet package, after the beam has propagated through the wedges, Faraday optic and a final beam displacer. This aspect of the invention allows the magnet package to be compact so as to be consistent with the compact optical structure enabled by mode stripping collimators. 
         [0021]    One advantage of the present invention is that use of a mode stripping ferrule/collimator on the output of a Faraday isolator enables consistent output beam focusing properties at high average power. The focusing beam parameters of the beam exiting the output fiber are dictated by the wave-guiding properties of the fiber itself, independent of changes in average laser power or any variable thermal lensing present in the optical elements within the Faraday isolator. 
         [0022]    In an embodiment of the invention, at least one detector or thermal sensor is mounted in the collimator fiber strain relief cover to quantitatively monitor the magnitude of radiation scattered from the mode stripping collimators, if desired. Such monitoring could be used, for example, to quantify backward propagating radiation that is scattered by the input collimator for various system feedback purposes. 
         [0023]    The invention is not limited to fiber pigtailed Faraday isolators. Other fiber pigtailed Faraday devices, such as circulators, rotators and Faraday mirrors suitable for high power applications, are contemplated by the invention. 
         [0024]    The invention will be better understood upon reference to the following detailed description in connection with the accompanying drawings. 
     
    
     
       BRIEF DESCRIPTION OF THE DRAWINGS 
         [0025]      FIG. 1  is a side cross-sectional view of a first embodiment of a high power fiber pigtailed Polarization Insensitive Faraday isolator according to the invention which is suitable for use at 1060 nm optical frequency. 
           [0026]      FIG. 2  is a side cross-sectional view of a second embodiment of a high power fiber pigtailed Polarization Maintaining Faraday isolator suitable for use at 1550 nm and including selected enhancement features. 
           [0027]      FIG. 3  is a side cross-sectional view of a third embodiment according to the invention, and in particular of a high power fiber pigtailed Faraday mirror suitable for use at 1550 nm. 
       
    
    
     DETAILED DESCRIPTION OF THE INVENTION 
       [0028]    Reference is now made in detail to specific embodiments representative of the present invention to illustrate the practice of the invention as contemplated by the inventors. Additional features are described in connection with each embodiment. Alternate embodiments will be apparent to those of ordinary skill in the art in light of these descriptions. 
         [0029]      FIG. 1  is a side cross-sectional view of a Polarization Independent Faraday isolator module according to the invention, wherein monolithic fused silica mode stripping ferrules  10  and  15  are employed. Suitable examples of such ferrules  10  and  15  are described in the disclosure of the above referenced commonly-owned patent application incorporated herein by reference. Input silica fiber  31 , monolithic ferrule  10 , fused silica sleeve  11  and silica aspheric lens  12  together form a substantially stable and compact mode stripping input fiber collimator assembly. Similarly, an output pigtailed collimator assembly is formed by fiber  32 , ferrule  15 , sleeve  14  and lens  13 . In both assemblies, the ferrule  10 ,  15  and optical surfaces of lenses  21 ,  22  are anti-reflection coated at the operating wavelength, herein for example 1060 nm. Non-magnetic, rigid optics holder  16  is made of a metal chosen to have a high thermal conductivity and a coefficient of thermal expansion that is substantially the same as that of an anti-reflection coated Terbium Gallium Garnet (“TGG”) Faraday optical element  18 , which is the core of the Polarization Independent Faraday isolator. Anti-reflection coated birefringent crystal wedges  17  and  19  are provided, typically made of Vanadate, a commercially available crystal. Other materials that are suitable in many instances are calcite, lithium niobate and rutile. The anti-reflection coatings on TGG optic  18  and wedges  17  and  19  are optimized to ensure that the wedged surfaces have no significant polarization-dependent loss. A beam displacer  20  is also in the optical path, typically also formed from Vanadate and also anti-reflection coated. Bonds  21  and  22  may use, for example, a high hardness, high glass transition temperature UV-activated heat cured adhesive or laser-fused transparent glass powder. An adhesive  23  is provided which is thermally conductive, soft and resilient to ensure that the bonded optical structure is decoupled from any stresses imparted by the surrounding magnetic structure. The magnet structure includes a permanent magnetic circuit  28 , magnet housing tube  27  and endplates  25  and  26 . 
         [0030]    In operation, thermally conductive adhesive  23  transfers heat from any absorbed power in the TGG rotating optic  18  through the metal optics holder  16  into a high thermal conductivity heat transfer tube  24 . Conductive covers  29  and  30  encircling the ferrules  10  and  15  and mounted to the endplates  25  and  26  absorb heat scattered by mode stripping ferrules  10  and  15  and conduct this heat to endplates  25  and  26 . Covers  29  and  30  may be made, for example, from clear anodized aluminum cups bolted to the endplates  25  and  26  and having orifices  33 ,  34  for the fibers  31 ,  32 . Adhesive at orifices  33  and  34  strain relieves optical fibers  31  and  32  to covers  29  and  30 . Laser light propagating in the forward, transmission direction which does not couple into the core of output fiber  32 , for example due to thermal lensing in TGG rotating optic  18 , is scattered or reflected away from the fiber by ferrule  15 . Laser optical energy propagating in the reverse, isolation direction, is angularly directed into the cladding of the input fiber or into the ferrule  10  itself, where it is scattered and also reflected away from the fiber. The input face of birefringent wedge  17  and output face of birefringent wedge  19  are at a small tilt to ensure no residual reflection from these surfaces couples into either optical fiber core. The remaining tilted faces of the birefringent wedges  17  and  19 , and TGG rotating optic  18 , are selected according to the thickness/length and refractive index of these materials such that forward propagating rays travel on the same beam path as the incident beam path after exiting beam displacer  20 . For optical fibers, such as Corning HI1060, and a 950 μm collimated beam diameter, an isolator constructed according to this preferred embodiment is useable with power levels in excess of 25 W. Further applicability for applications where the focusing properties of the output beam must not change is guaranteed by the wave-guiding properties of the small (approximately 6 μm) core of the output fiber. Any changes in the beam parameters due to thermal lensing of optical elements within the Faraday isolator will result in that component of the output missing the core of the output fiber, thereby being removed in the mode stripping output ferrule. 
         [0031]    An alternative embodiment of the present invention, a high-power fiber-pigtailed Polarization Maintaining Faraday isolator (designed to operate at for example 1550 nm), is illustrated in the side cross-sectional view of  FIG. 2 . Suitable examples of input monolithic collimator  40  and output monolithic collimator  41  are described in the disclosure of the above-referenced commonly owned patent application incorporated herein by reference. Preferably, a lens is formed directly on the ferrule optical surface at  59  and  60 . Input PM fiber  57  is fusion spliced to a suitable length of input Corning SP 1550 single-polarization fiber  42 . For 30 dB extinction, the length of SP1550 fiber requires a length of one meter. Faraday optic element  45  is disposed in the beam path within the magnet structure. The material of the Faraday optic element  45  is, for example, Mitsubishi “P-Type” low absorption Bismuth-substituted Iron Garnet (BIG) having a specified absorption of less than 0.05 dB. Faraday optic  45  is tilted (by approximately 1°) to ensure that residual reflections do not couple into either fiber, and it is bonded to optic holder  44 . This results in only a small (approximately 5 μm) displacement of the collimated beam from the initial beam path out of collimator  40 . Thus the displacement does not significantly reduce coupling to output collimator  41  if it is kept centered on the original beam path. The optic holder is typically a non-magnetic metal with high thermal conductivity and a coefficient of thermal expansion matched to that of the Faraday optic  45 . An encircling permanent magnet  46  with a central passage of minimal size operates to saturate the magnetization of Faraday optic  45  so that its optical properties are activated. Housing  47 , cover  48  and heat transfer tube  49  form a housing assembly that encloses the Faraday optic  45 , magnet  46  and optic holder  44 . In operation, a soft, resilient, high thermal conductivity adhesive bond at interface  50  transfers heat from the optic holder  44  to the heat transfer tube  49 , where the heat is further conducted to the housing assembly. Bonds at orifices  53  and  54  secure and strain relieve optical fibers  42  and  43  to covers  51  and  52  which are secured to housing  47  and cover  48 . Short flexible tubes  55  and  56  protect the fiber  42  and  43  from sharp bends by restraining the bend radius. For 30 dB isolation output (optional), type SP 1550 single-polarization fiber  43  is of the same 1-meter length as input single polarization fiber  42 . Fiber  43  is fusion spliced to the Polarization Maintaining fiber  58 . The polarization axis of output monolithic collimator  41  and output single polarization fiber  43  is rotated 45° with respect to the polarization axis of input monolithic collimator  40  and fiber  42  to account for the 45° Faraday rotation in Faraday optic  45  prior to bonding the collimators  40  and  41  to the optics holder  44  with adhesive at surfaces  59  and  60 . The polarization of backward propagating radiation entering the lens face of collimator  40  is 90° to the polarization axis of the collimator  40 . Hence, this light (optical energy) is rejected into the cladding of fiber  42  within the mode stripping collimator  40 , where it is scattered and reflected onto cover  51 . A device built according to this embodiment can achieve isolation in excess of 30 dB with in excess of 15 W of incident power. The mode stripping collimators  40  and  41  should be 5 cm long in order to reduce rejected polarization power levels safely below 10 W under all operating conditions in order to not destroy the polymer protective coating. The beam focusing parameters are dictated by output PM fiber  58 , rather than by any thermal lensing in Faraday optic  45 . Backward propagating radiation into mode stripping collimator  40  is scattered toward photodetector  61 , which generates a signal proportional to the magnitude of the backward propagating radiation as displayed on meter  62 . 
         [0032]      FIG. 3  is exemplary of alternative embodiments of the present invention. A side cross-sectional view of a high-power fiber-pigtailed Faraday mirror according to the invention is shown (designed to operate at for example 1060 nm), wherein a monolithic fused-silica mode stripping ferrule  70  is employed. Suitable examples of such ferrules are described in the disclosure of the above referenced commonly owned patent application incorporated herein by reference. Silica fiber  73 , monolithic ferrule  70 , fused silica sleeve  71  and fused silica lens  72  together form a mode stripping fiber collimator assembly. The Faraday optic is a transparent polycrystalline ceramic Terbium Aluminum Garnet (“TAG”) rod  75 . The TAG ceramic rod  75  is anti-reflection coated on the optical surface adjacent to the lens  72 . The other surface of the TAG rod  75  is given a high reflectance coating at the operating wavelength of 1060 nm. TAG rod  75  is mounted in conductive metal mount/endplate  74  and surrounded by magnetic circuit  79 . This mount is threaded on the periphery to mate to a heat-sinking strain relief cover  76 . Adhesive  77  secures the fiber collimator assembly lens  72  to a matching spherical surface machined into mount/endplate  74 . Adhesive  78  secures fiber  73  to strain relief cover  76 . Fiber pigtailed Faraday mirrors are commonly used between fiber amplifiers or within a double pass fiber amplifier to flip polarization states upon 90 degree reflection in the Faraday mirrors. Polarization flipping between amplifier stages or within a double pass amplifier can help remove any undesirable polarization distortions in a fiber amplifier system. As disclosed here, a fiber pigtailed Faraday mirror can be used with very high power fiber lasers and fiber amplifiers where polarization effects are important. 
         [0033]    The invention has now been explained with respect to specific exemplary embodiments. Other embodiments will be apparent to those of ordinary skill in the art upon reference to these descriptions. For example the foregoing description also applies to structures not requiring a magnet assembly, such as a device wherein there is inherent polarization rotation applied to the incident beam. It is therefore not intended that this invention be limited, except as indicated by the appended claims.