Patent Grant
8977095
1. Field
The present specification generally relates to optical fibers and, more specifically, to polarization maintaining optical fibers.
2. Technical Background
Polarization-Maintaining (PM) optical fibers are a class of specialty optical fibers that may be used in a variety of applications including coherent communication systems, navigational controls (gyros), fiber-optic sensors, and, most-recently, in high-brightness fiber lasers.
Conventional PM optical fibers are made by inserting stress-applying-parts adjacent to and external to the core (i.e., the light carrying portion of the optical fiber) in order to induce a non-symmetrical stress field around the core. The stress-applying-parts (SAPs) are generally formed from boron-doped silica glass. The SAPs can have various shapes depending on the methods used for making the fiber. For example, Panda-type PM optical fibers are formed by mechanically drilling a pair of holes around the core of the optical fiber preform and inserting SAPs in the holes prior to drawing the preform into a fiber. The birefringence generated in the PM fibers is due to the anisotropic thermal-stress caused by the mismatch in the coefficient of thermal expansion between the SAPs and the surrounding cladding.
Due to the high absorption of boron doped SAPs, the SAPs must be positioned some distance away from the fiber core in order to avoid high fiber attenuation. Very high boron doping levels (>20% by weight) are generally needed to produce sufficient birefringence in the core. In addition, boron doping in the glass changes the viscosity of the glass significantly, making the glass much softer than the pure silica cladding. As a result, PM fibers with boron doped stress rods are difficult to make and expensive. In the case of multi-core PM fiber or PM fibers with a low cladding diameter, there may be insufficient space in the cladding portion of the optical fiber to accommodate the SAPs.
Accordingly, a need exists for alternative designs for polarization maintaining optical fibers.
According to one embodiment, a polarization maintaining optical fiber may include a cladding portion and a core portion disposed in the cladding portion. The core portion may include a first core region having a first coefficient of thermal expansion CTE1 and a second core region having a second coefficient of thermal expansion CTE2. The first coefficient of thermal expansion CTE1 is not equal to the second coefficient of thermal expansion CTE2. At least one of the first core region and the second core region may be non-circular symmetric with respect to a centerline of the polarization maintaining optical fiber.
In another embodiment, a polarization maintaining optical fiber may include a cladding and a core portion disposed in the cladding. The core portion may include a first core region and a second core region. The second core region comprises at least one down-dopant and at least one up-dopant such that a relative refractive index difference Δcc between the first core region and the second core region is less than 0.1%. A birefringence of the polarization maintaining optical fiber may be greater than 1×10−5 at wavelengths in a range greater than or equal to 800 nm and less than or equal to 1700 nm.
In yet another embodiment, a polarization maintaining optical fiber may include a cladding portion and a core portion disposed in the cladding portion. The core portion may include a first core region having a first coefficient of thermal expansion CTE1 and a second core region having a second coefficient of thermal expansion CTE2. A difference between CTE1 and CTE2 may be greater than or equal to 1×10−7/° C. A birefringence of the polarization maintaining optical fiber may be greater than 1×10−5 at wavelengths in a range greater than or equal to 800 nm and less than or equal to 1700 nm.
Additional features and advantages of the embodiments described herein will be set forth in the detailed description which follows, and in part will be readily apparent to those skilled in the art from that description or recognized by practicing the embodiments described herein, including the detailed description which follows, the claims, as well as the appended drawings.
It is to be understood that both the foregoing general description and the following detailed description describe various embodiments and are intended to provide an overview or framework for understanding the nature and character of the claimed subject matter. The accompanying drawings are included to provide a further understanding of the various embodiments, and are incorporated into and constitute a part of this specification. The drawings illustrate the various embodiments described herein, and together with the description serve to explain the principles and operations of the claimed subject matter.
a)-2(f) depict cross sections of different embodiments of core portions of PM optical fibers;
Reference will now be made in detail to embodiments of polarization maintaining optical fibers, examples of which are illustrated in the accompanying drawings. Whenever possible, the same reference numerals will be used throughout the drawings to refer to the same or like parts. One embodiment of a polarization maintaining optical fiber is schematically depicted in
The phrase “refractive index profile,” as used herein, refers to the relationship between refractive index or relative refractive index and the dimensions of the optical fiber.
The phrase “relative refractive index,” as used herein, is defined as Δ(r) %=100×(n(r)2−nREF2)/2ni2, where ni is an extrema of the refractive index in region i (i.e., the minimum or maximum of the refractive index in region i), unless otherwise specified. The relative refractive index percent is measured at 1550 nm unless otherwise specified. The term nREF is the average refractive index of the common outer cladding, which can be calculated, for example, by taking “N” index measurements (nc1, nc2, . . . ncN) of the common outer cladding (which, in some embodiments, may be undoped silica), and calculating the average refractive index by:
As used herein, the relative refractive index is represented by Δ and its values are given in units of “%,” unless otherwise specified. In cases where the refractive index of a region is less than the reference index nREF, the relative refractive index is negative and is referred to as having a depressed region or depressed-index, and the minimum relative refractive index is calculated at the point at which the relative refractive index is most negative, unless otherwise specified. In cases where the refractive index of a region is greater than the reference index nREF, the relative index percent is positive and the region can be said to be raised or to have a positive index.
The term “birefringence,” as used herein, refers to the effective index difference between orthogonal (i.e., x and y) polarization states of a fundamental mode propagating in the core portion of an optical fiber.
Referring now to
The cladding portion 108 is generally formed from silica-based glass (SiO2) which surrounds and directly contacts the core portion 102. In some embodiments of the PM optical fiber 100 described herein, the cladding portion 108 comprises an overclad portion 110 surrounding the core portion 102 and an outer cladding portion 112 surrounding the overclad portion 110. In these embodiments, the overclad portion 110 of the cladding portion 108 may be formed from silica-based glass which is doped with one or more dopants which decreases the index of refraction of the overclad portion 110, such as boron, fluorine or the like. The outer cladding portion 112 may be formed form un-doped silica-based glass or silica-based glass which includes one or more dopants which decreases the index of refraction of the outer cladding portion 112, such as boron, fluorine or the like. In general, the index of refraction of the cladding portion 108 is less than the index of refraction of the core portion 102 of the PM optical fiber 100.
The optical fibers described herein are polarization maintaining optical fibers. In order to achieve the desired birefringence within the core portion of the optical fiber and thereby maintain the polarization of the propagated light, the core portion 102 of the PM optical fiber 100 is constructed from a first core region 104 with a first coefficient of thermal expansion CTE1 and a second core region 106 with a second coefficient of thermal expansion CTE2 which is not equal to the first coefficient of thermal expansion CTE1. In the embodiments described herein, the absolute value of the difference between the first coefficient of thermal expansion CTE1 of the first core region 104 and the second coefficient of thermal expansion CTE2 of the second core region 106 is greater than or equal to 1×10−7/° C. or even greater than or equal to 1×10−6/° C.
In addition, at least one of the first core region 104 and the second core region 106 is non-circular symmetric with respect to the centerline CL of the PM optical fiber. For reference, the phrase “circular symmetric” generally means that a particular structure is symmetric about any straight line drawn through the center point of the structure. For example, a series of concentric circles are circular symmetric about any line drawn through the center point of the concentric circles. However, a non-circular symmetric structure is not symmetric about every straight line drawn through the center point of the structure. For example, the first core region 104 of the PM optical fiber 100 of
The asymmetry of at least one of the first core region 104 and the second core region 106 with respect to the centerline of the PM optical fiber in combination with the different coefficients of thermal expansion of the first core region 104 and the second core region 106 creates a stress differential within the core portion 102. The stress differential, in turn, creates birefringence between orthogonal polarized modes of light propagating in the core portion 102 of the PM optical fiber. In the embodiments described herein, the PM optical fibers 100 have a birefringence of greater than or equal to 1×10−5 in the wavelength range from about 800 nm to about 1700 nm due to the stress differential caused by the difference in the CTEs and the asymmetry of at least one of the core regions. In some embodiments, the PM optical fibers 100 may have a birefringence of greater than or equal to 1×10−4 of even greater than or equal to 5×10−4 over the wavelength range from about 800 nm to about 1700 nm.
While the core portion 102 of the PM optical fibers 100 described herein is constructed from a first core region 104 and a second core region 106, each having different coefficients of thermal expansion, it should be understood that the refractive index n1 of the first core region 104 and the refractive index n2 of the second core region 106 are substantially the same so as not to disrupt the propagation of light through the entire core portion 102 of the PM optical fibers 100. Preferably the index difference between n1 and n2 is less than 0.0014, more preferably less than 0.0005 or most preferably, less than 0.0001.
More specifically, in the embodiments of the PM optical fibers 100 described herein, the first core region 104 generally has a relative refractive index Δc1 which is less than or equal to 2% relative to the outer cladding portion 112 of the PM optical fiber 100. In some embodiments, the relative refractive index Δc1 of the first core region 104 is greater than or equal to 0.1% and less than or equal to about 2%. In some other embodiments, the relative refractive index Δc1 of the first core region 104 is greater than or equal to 0.3% and less than or equal to about 1%. Similarly, the second core region 106 generally has a relative refractive index Δc2 less than or equal to 2% relative to the outer cladding portion 112 of the PM optical fiber 100. In some embodiments, the relative refractive index Δc2 of the second core region 106 is greater than or equal to 0.1% and less than or equal to about 2%. In some other embodiments, the relative refractive index Δc2 of the second core region 106 is greater than or equal to 0.3% and less than or equal to about 1%.
In some embodiments of the PM optical fibers 100 described herein, the difference in the relative refractive index of the first core region 104 and the relative refractive index of the second core region 106 is minimized so as not to disrupt the propagation of light through the core portion 102 of the PM optical fiber. Specifically, in some embodiments described herein, the relative refractive index difference Δcc=|Δc1−Δc2| and is less than or equal to 0.1%. Preferably, in some embodiments, the relative refractive index difference Δcc is less than or equal to 0.05% or, more preferably, less than or equal to 0.01%. Accordingly, it should be understood that light propagating through the first core region 104 and the second core region 106 travels at essentially the same speed in both regions.
A PM optical fiber 100 having core regions with different CTEs and in which the relative refractive index difference Δcc is minimized, as described above, may be created using several different techniques. In one embodiment, the core regions are doped with different doping materials such that the core regions 104, 106 have different compositions and, therefore, different coefficients of thermal expansion while the relative refractive index difference Δcc between the core regions is minimized. For example, in one embodiment, the first core region 104 may be formed from relatively pure (i.e., undoped) silica glass. In the embodiments described herein, relatively pure silica glass contains less than about 0.1 wt. % of impurities, tramp components, and the like. In this embodiment, the second core region 106 may be co-doped with one or more dopants which increases the index of refraction of silica glass (i.e., up-dopants), such as GeO2, TiO2, ZrO2, Nb2O5 and/or Ta2O5, and one or more dopants which decreases the index of refraction of silica glass (i.e., down-dopants), such as B2O3, fluorine, or the like. The addition of the dopants to the silica glass of the second core region 106 changes the coefficient of thermal expansion CTE2 of the second core region 106 with respect to the coefficient of thermal expansion CTE1 of the first core region 104. However, co-doping the silica glass of the second core region 106 with appropriate amounts of up-dopants and down-dopants results in a net relative refractive index change of about zero in the second core region 106 such that the relative refractive index Δc2 of the second core region 106 is substantially the same as the relative refractive index Δc1 of the first core region 104, thereby minimizing the relative refractive index difference Δcc between the first core region 104 and the second core region 106.
While the aformentioned technique for creating a CTE difference between the first core region 104 and the second core region 106 involves doping the silica glass of the second core region 106 while leaving the silica glass of the first core region 104 un-doped, it should be understood that similar effects can be achieved by co-doping the silica glass of the first core region 104 with up-dopants and down-dopants while leaving the silica glass of the second core region un-doped.
Alternatively, the same effect can be achieved by up-doping or down-doping one of the first core region 104 or the second core region 106 and co-doping the other region such that the coefficients of thermal expansion of the first core region 104 and the second core region 106 are different while the relative refractive index difference Δcc between the first core region 104 and the second core region 106 is minimized. For example, in one embodiment, the first core region 104 may be up-doped by including a dopant which increases the index of refraction of silica glass, such as GeO2 or the like, in the silica glass of the first core region 104. In order to produce the desired difference in the coefficient of thermal expansion between the first core region 104 and the second core region 106, the second core region 106 is co-doped with both an up-dopant and a down-dopant in amounts sufficient to match the change in the index of refraction of the first core region 104 such that the relative refractive index difference Δcc between the first core region 104 and the second core region 106 is minimized while imparting a different coefficient of thermal expansion to the second core region 106.
Accordingly, it should be understood that the desired differential in the coefficients of thermal expansion and minimal relative refractive index difference Δcc can be achieved by co-doping at least one of the first core region and the second core region to thereby achieve a stress differential in the core portion 102 of the PM optical fiber 100.
As noted hereinabove, the asymmetry (i.e., the non-circular symmetry) of at least one of the first core region 104 and the second core region 106 with respect to the centerline of the PM optical fiber 100 assists in achieving the desired birefringence in the PM optical fiber 100 by creating a stress differential within the core portion of the PM optical fiber. The non-circular symmetry of at least one of the first core region 104 and the second core region 106 with respect to the centerline of the PM optical fiber 100 may be achieved in a number of different ways. Referring to
While
Alternatively, one of the core regions of the core portion may comprise a plurality of core region segments which are non-circular symmetric with respect to the centerline CL of the PM optical fiber. For example,
Similarly,
A method of forming a PM optical fiber will now be described in more detail with specific reference to
In one embodiment, the core portion 102, and cladding portion 108 of the PM optical fiber 100 may be formed by an outside-vapor-deposition (OVD) process. The OVD process is a way of making optical fiber through reactions from the desired vapor ingredients (including silica and the other desired dopant precursors) via a pyrolysis process in a CH4+O2 flame to form soot-particles, which are then collected by thermopheretic means onto a glass core cane or rod. The soot-preform is subsequently dried and densified into solid transparent glass in a high temperature furnace, a process commonly referred to as consolidation. The desired core and cladding compositions are achieved by utilizing different amounts of various vapor-phase ingredients for each of the layers in the soot preform fabrication process. For example, the core/cladding perform may be generated first, then consolidated, and the final (consolidated) preform drawn into the optical fiber by known fiber-drawing methods.
Referring now to
Referring now to
Thereafter, a layer of glass soot is deposited around region 206 to form an outer region 208 which generally corresponds to the overclad portion of the PM optical fiber. In the embodiments described herein, outer region 208 may be initially formed by depositing relatively pure silica glass soot around region 206 by outside vapor deposition. The soot is in region 208 is then consolidated in a furnace with a fluorine containing compound, for example with SiF4, CF4 or BF3, such that silica glass in region 208 is down-doped. Thereafter, one or more additional layers of silica glass soot (not shown) may be deposited over region 208 and consolidated to form additional cladding layers. The preform may then be drawn into optical fiber using conventional fiber drawing techniques.
While
Further, while
The embodiments of the PM optical fiber described herein will be further clarified by the following examples.
A single core PM optical fiber as depicted in
The birefringence of the optical fiber was then determined using the polarization beat length measurement. To perform the measurement, a broadband light source is polarized and launched into a fiber having a test length L. The polarization direction of the light is adjusted to an angle of about 45° to the x-birefringence axis of the fiber to excite both the x and y polarized modes. A polarizer is placed at an angle of about 45° to the x-birefringence axis at the output of fiber. The output light is detected and the spectrum is analyzed to get the beat length. That spectrum will exhibit oscillations with a period Δλ, from which the polarization beat length can be calculated by:
LB=(Δλ/λ)L
The birefringence is related to the beat length by
B=λ/LB.
The measurement was performed at 1550 nm with a super luminescent diode (SLD) light source and an optical spectral analyzer (OSA) detector. From the oscillations in the OSA signal (
A multiple core PM optical fiber as depicted in
The birefringence of the optical fiber was then determined using the polarization beat length measurement as described above. The measurement was performed at 1550 nm with an SLD light source and an OSA detector. From the oscillations in the OSA signal (
It should now be understood that the PM optical fibers described herein utilize a multi-region core in order to achieve a desired birefringence in the optical fiber. Specifically, the PM optical fibers described herein include a core portion which includes at least a first core region and a second core region, each of which have a different coefficient of thermal expansion. At least one of the first core region and the second core region is also non-circular symmetric with respect to the centerline of the optical fiber. The combination of the difference in CTEs with the designed asymmetry of at least one of the core regions creates a stress differential within the core portion of the optical fiber thereby facilitating the polarization maintaining properties of the optical fiber. Moreover, creating first and second core regions with different coefficients of thermal expansion without disrupting the light transmission properties of the core portion of the optical fiber is achieved by doping at least one of the core regions with both up-dopants and down-dopants such that the coefficient of thermal expansion of the core region is changed without changing the index of refraction of the core region relative to the other core region.
PM optical fibers as described herein (i.e., PM optical fibers without stress applying parts in the cladding portion) are an improvement over conventional PM optical fibers in which the stress applying parts are external to the core portion. For example, creating the applied stress within the core portion of the optical fiber reduces the thickness of the cladding of the optical fiber, thereby providing a more compact, lower cost optical fiber. This also facilitates positioning additional core elements within the cladding, thereby facilitating multi-core PM optical fibers. Further, because the stress inducing the birefringence is generated within the core portion of the optical fiber, less stress is required to achieve the same level of birefringence.
It will be apparent to those skilled in the art that various modifications and variations can be made to the embodiments described herein without departing from the spirit and scope of the claimed subject matter. Thus it is intended that the specification cover the modifications and variations of the various embodiments described herein provided such modification and variations come within the scope of the appended claims and their equivalents.
This application claims the benefit of priority under 35 U.S.C. §119 of U.S. Provisional Application Ser. No. 61/704,840 filed on Sep. 24, 2012 the content of which is relied upon and incorporated herein by reference in its entirety.
| Number | Name | Date | Kind |
|---|---|---|---|
| 4354736 | Maklad et al. | Oct 1982 | A |
| 4426129 | Matsumura et al. | Jan 1984 | A |
| 7116887 | Farroni et al. | Oct 2006 | B2 |
| 7158705 | Berkey et al. | Jan 2007 | B2 |
| 7386210 | Farroni et al. | Jun 2008 | B2 |
| 7697809 | Bookbinder et al. | Apr 2010 | B2 |
| 8000575 | Chen et al. | Aug 2011 | B2 |
| 8213070 | Koplow | Jul 2012 | B2 |
| 8731357 | Hirano et al. | May 2014 | B2 |
| 20040086245 | Farroni et al. | May 2004 | A1 |
| 20060045446 | Berkey et al. | Mar 2006 | A1 |
| 20090207483 | Goto | Aug 2009 | A1 |
| 20110081123 | Pare et al. | Apr 2011 | A1 |
| 20130308914 | Hayashi et al. | Nov 2013 | A1 |
| Number | Date | Country | |
|---|---|---|---|
| 20140212102 A1 | Jul 2014 | US |
| Number | Date | Country | |
|---|---|---|---|
| 61704840 | Sep 2012 | US |
