Patent Grant
8428410
The present invention relates to the field of fiber optic transmission and, more specifically, to a multimode optical fiber having reduced bending losses and a high bandwidth for high-data-rate applications.
An optical fiber (i.e., a glass fiber typically surrounded by one or more coating layers) conventionally includes an optical fiber core, which transmits and/or amplifies an optical signal, and an optical cladding, which confines the optical signal within the core. Accordingly, the refractive index of the core nc is typically greater than the refractive index of the optical cladding ng (i.e., nc>ng).
For optical fibers, the refractive index profile is generally classified according to the graphical appearance of the function that associates the refractive index with the radius of the optical fiber. Conventionally, the distance r to the center of the optical fiber is shown on the x-axis, and the difference between the refractive index (at radius r) and the refractive index of the optical fiber's outer cladding (e.g., an outer optical cladding) is shown on the y-axis. The refractive index profile is referred to as a “step” profile, “trapezoidal” profile, “alpha” profile, or “triangular” profile for graphs having the respective shapes of a step, a trapezoid, an alpha, or a triangle. These curves are generally representative of the optical fiber's theoretical or set profile. Constraints in the manufacture of the optical fiber, however, may result in a slightly different actual profile.
Generally speaking, two main categories of optical fibers exist: multimode fibers and single-mode fibers. In a multimode optical fiber, for a given wavelength, several optical modes are propagated simultaneously along the optical fiber, whereas in a single-mode optical fiber, the higher order modes are strongly attenuated. The typical diameter of a single-mode or multimode glass fiber is 125 microns. The core of a multimode optical fiber typically has a diameter of between about 50 microns and 62.5 microns, whereas the core of a single-mode optical fiber typically has a diameter of between about 6 microns and 9 microns. Multimode systems are generally less expensive than single-mode systems, because multimode light sources, connectors, and maintenance can be obtained at a lower cost.
Multimode optical fibers are commonly used for short-distance applications requiring a broad bandwidth, such as local networks or LAN (local area network). Multimode optical fibers have been the subject of international standardization under the ITU-T G.651.1 recommendations, which, in particular, define criteria (e.g., bandwidth, numerical aperture, and core diameter) that relate to the requirements for optical fiber compatibility. The ITU-T G.651.1 standard is hereby incorporated by reference in its entirety.
In addition, the OM3 standard has been adopted to meet the demands of high-bandwidth applications (i.e., a data rate higher than 1 GbE) over long distances (i.e., distances greater than 300 meters). The OM3 standard is hereby incorporated by reference in its entirety. With the development of high-bandwidth applications, the average core diameter for multimode optical fibers has been reduced from 62.5 microns to 50 microns.
Typically, an optical fiber should have the broadest possible bandwidth to perform well in a high-bandwidth application. For a given wavelength, the bandwidth of an optical fiber may be characterized in several different ways. Typically, a distinction is made between the so-called “overfilled launch” condition (OFL) bandwidth and the so-called “effective modal bandwidth” condition (EMB). The acquisition of the OFL bandwidth assumes the use of a light source exhibiting uniform excitation over the entire radial surface of the optical fiber (e.g., using a laser diode or light emitting diode (LED)).
Recently developed light sources used in high-bandwidth applications, such as VCSELs (Vertical Cavity Surface Emitting Lasers), exhibit an inhomogeneous excitation over the radial surface of the optical fiber. For this kind of light source, the OFL bandwidth is a less suitable measurement, and so it is preferable to use the effective modal bandwidth (EMB). The calculated effective bandwidth (EMBc) estimates the minimum EMB of a multimode optical fiber independent of the kind of VCSEL used. The EMBc is obtained from a differential-mode-delay (DMD) measurement (e.g., as set forth in the FOTP-220 standard).
An exemplary method of measuring DMD and calculating the effective modal bandwidth can be found in the FOTP-220 standard, which is hereby incorporated by reference in its entirety. Further details on this technique are set forth in the following publications, each of which is hereby incorporated by reference: P. F. Kolesar and D. J. Mazzarese, “Understanding Multimode Bandwidth and Differential Mode Delay Measurements and Their Applications,” Proceedings of the 51st International Wire and Cable Symposium, pp. 453-460; and D. Coleman and Philip Bell, “Calculated EMB Enhances 10 GbE Performance Reliability for Laser-Optimized 50/125 μm Multimode Fiber,” Corning Cable Systems Whitepaper.
The TIA-492AAAC-A standard, which is hereby incorporated by reference in its entirety, specifies the performance requirements for 50-micron-diameter multimode optical fibers used over long distances in Ethernet high-bandwidth transmission network applications. The OM3 standard requires, at a wavelength of 850 nanometers, an EMB of at least 2,000 MHz·km. The OM3 standard assures error-free transmissions for a data rate of 10 Gb/s (10 GbE) up to a distance of 300 meters. The OM4 standard requires, at a wavelength of 850 nanometers, an EMB of at least 4,700 MHz·km to obtain error-free transmissions for a data rate of 10 Gb/s (10 GbE) up to a distance of 550 meters. The OM4 standard is hereby incorporated by reference in its entirety.
In a multimode optical fiber, the difference between the propagation times, or group delay times, of the several modes along the optical fiber determine the bandwidth of the optical fiber. In particular, for the same propagation medium (i.e., in a step-index multimode optical fiber), the different modes have different group delay times. This difference in group delay times results in a time lag between the pulses propagating along different radial offsets of the optical fiber.
For example, as shown in the graph on the right side of
As depicted in
To reduce intermodal dispersion, the multimode optical fibers used in telecommunications generally have a core with a refractive index that decreases progressively from the center of the optical fiber to its interface with a cladding (i.e., an “alpha” core profile). Such an optical fiber has been used for a number of years, and its characteristics have been described in “Multimode Theory of Graded-Core Fibers” by D. Gloge et al., Bell system Technical Journal 1973, pp. 1563-1578, and summarized in “Comprehensive Theory of Dispersion in Graded-Index Optical Fibers” by G. Yabre, Journal of Lightwave Technology, February 2000, Vol. 18, No. 2, pp. 166-177. Each of the above-referenced articles is hereby incorporated by reference in its entirety.
A graded-index profile (i.e., an alpha-index profile) can be described by a relationship between the refractive index value n and the distance r from the center of the optical fiber according to the following equation:
wherein,
α≧1, and α is a non-dimensional parameter that is indicative of the shape of the index profile;
n1 is the maximum refractive index of the optical fiber's core;
a is the radius of the optical fiber's core; and
where n0 is the minimum refractive index of the multimode core, which may correspond to the refractive index of the outer cladding (most often made of silica).
A multimode optical fiber with a graded index (i.e., an alpha profile) therefore has a core profile with a rotational symmetry such that along any radial direction of the optical fiber the value of the refractive index decreases continuously from the center of the optical fiber's core to its periphery. When a multimode light signal propagates in such a graded-index core, the different optical modes experience differing propagation mediums (i.e., because of the varying refractive indices). This, in turn, affects the propagation speed of each optical mode differently. Thus, by adjusting the value of the parameter α, it is possible to obtain a group delay time that is virtually equal for all of the modes. Stated differently, the refractive index profile can be modified to reduce or even eliminate intermodal dispersion.
In practice, however, a manufactured multimode optical fiber has a graded-index central core surrounded by an outer cladding of constant refractive index. The core-cladding interface interrupts the core's alpha-index profile. Consequently, the multimode optical fiber's core never corresponds to a theoretically perfect alpha profile (i.e., the alpha set profile). The outer cladding accelerates the higher-order modes with respect to the lower-order modes. This phenomenon is known as the “cladding effect.” In DMD measurements, the responses acquired for the highest radial positions (i.e., nearest the outer cladding) exhibit multiple pulses, which results in a temporal spreading of the response signal. Therefore, bandwidth is diminished by this cladding effect.
Multimode optical fibers are commonly used for short-distance applications requiring a broad bandwidth, such as local area networks (LANs). In such applications, the optical fibers may be subjected to accidental or otherwise unintended bending, which can modify the mode power distribution and the bandwidth of the optical fiber.
It is therefore desirable to achieve multimode optical fibers that are unaffected by bends having a radius of curvature of less than 10 millimeters. One proposed solution involves adding a depressed trench between the core and the cladding. Nevertheless, the position and the depth of the trench can significantly affect the optical fiber's bandwidth.
Japanese Patent Publication No. JP 2006/47719 A, which is hereby incorporated by reference in its entirety, discloses a graded index optical fiber having a depressed trench in its cladding. Nevertheless, the disclosed optical fiber exhibits higher bending losses than desired and a relatively low bandwidth. Moreover, the disclosed optical fiber's cladding effect is not mentioned.
International Publication No. WO-A-2008/085851, which is hereby incorporated by reference in its entirety, discloses a graded index optical fiber having a depressed trench in its cladding. Nevertheless, the disclosed optical fiber exhibits a relatively low bandwidth, and its cladding effect is not mentioned.
U.S. Patent Application Publication No. 2009/0154888, which is hereby incorporated by reference in its entirety, discloses a graded index optical fiber having a depressed trench in its cladding. Nevertheless, the disclosed optical fiber exhibits a relatively low bandwidth, and its cladding effect is not mentioned.
European Patent No. EP 0131729, which is hereby incorporated by reference in its entirety, discloses a graded index optical fiber having a depressed trench in its cladding. According to this patent, to achieve a high bandwidth, the distance between the end of the graded-index core and the beginning of the depressed trench should be between 0.5 micron and 2 microns. Nevertheless, the disclosed optical fiber exhibits higher bending losses than desired. Moreover, the disclosed optical fiber's cladding effect is not mentioned.
Therefore, a need exists for a graded-index multimode optical fiber having reduced bending losses and a high bandwidth with a reduced cladding effect for high-data rate applications.
Accordingly, in one aspect, the present invention embraces an optical fiber that includes a central core, an inner cladding, a depressed trench, and an outer cladding (e.g., an outer optical cladding). Typically, the central core is a glass-based central core having an alpha-index profile (i.e., a graded-index profile) and a radius r1. The central core's alpha-index profile has a minimum refractive index at the central core's radius r1 that corresponds to a refractive index difference Δnend with respect to the outer cladding. Stated differently, the central core has a radius r1 and an alpha-index profile, and, at the central core's radius r1, a refractive index difference Δnend with respect to the outer cladding.
The optical fiber's inner cladding is positioned between the central core and the outer cladding. The inner cladding has a radius r2, a width w2, and a refractive index difference Δn2 with respect to the outer cladding.
The optical fiber's depressed trench is positioned between the inner cladding and the outer cladding. The depressed trench has a radius rout, a width w3, and a refractive index difference Δn3 with respect to the outer cladding.
In an exemplary embodiment, the central core's refractive index difference Δnend is negative. Typically, the central core's refractive index difference Δnend, is greater than about −1×10−3 (e.g., between about −1×10−3 and −0.01×10−3). More typically, the central core's refractive index difference Δnend is less than −0.2×10−3, such as between about −0.7×10−3 and −0.3×10−3.
In another exemplary embodiment, the depressed trench's refractive index difference Δn3 is between −15×10−3 and −3×10−3.
In yet another exemplary embodiment, the inner cladding's refractive index difference Δn2 and the depressed trench's refractive index difference Δn3 satisfy the following inequality:
1000×Δn3<−1.29×(1000×Δn2)2−1.64×1000×Δn2−2.51.
In yet another exemplary embodiment, the inner cladding's refractive index difference Δn2 and the depressed trench's refractive index difference Δn3 satisfy both of the following inequalities:
−1.89×(1000×Δn2)2−7.03×(1000×Δn2)−9.91<1000×Δn3; and
1000×Δn3<−1.53×(1000×Δn2)2−3.34×1000×Δn2−4.25.
In yet another exemplary embodiment, the inner cladding's refractive index difference Δn2 satisfies the following inequality:
0.2×10−3<|Δn2|<2×10−3.
In yet another exemplary embodiment, the central core's refractive index difference Δnend is zero and the inner cladding's refractive index difference Δn2 satisfies the following inequality:
0.2×10−3<|Δn2|.
In yet another exemplary embodiment, the inner cladding's width w2 is between about 0.5 micron and 2 microns.
In yet another exemplary embodiment, the depressed trench's refractive index difference Δn3 is between −10×10−3 and −5×10−3.
In yet another exemplary embodiment, the depressed trench's width w3 is between about 3 microns and 5 microns.
In yet another exemplary embodiment, the depressed trench's radius rout is about 32 microns or less (e.g., 30 microns or less).
In yet another exemplary embodiment, the depressed trench's volume is between about 200%·μm2 and 1,200%·μm2 (e.g., between 250%·μm2 and 750%·μm2).
In yet another exemplary embodiment, for two turns around a bend radius (e.g., a radius of curvature) of 15 millimeters at a wavelength of 850 nanometers, the optical fiber has bending losses of less than 0.1 dB (e.g., less than 0.05 dB).
In yet another exemplary embodiment, for two turns around a bend radius of 10 millimeters at a wavelength of 850 nanometers, the optical fiber has bending losses of less than 0.3 dB (e.g., less than 0.1 dB).
In yet another exemplary embodiment, for two turns around a bend radius of 7.5 millimeters at a wavelength of 850 nanometers, the optical fiber has bending losses of less than 0.4 dB (e.g., less than 0.2 dB).
In yet another exemplary embodiment, for two turns around a bend radius of 7.5 millimeters at a wavelength of 850 nanometers, the optical fiber has bending losses of less than 0.1 dB (e.g., less than 0.05 dB).
In yet another exemplary embodiment, for two turns around a bend radius of 7.5 millimeters at a wavelength of 850 nanometers, the optical fiber has bending losses of less than 0.04 dB (e.g., less than 0.01 dB).
In yet another exemplary embodiment, for two turns around a bend radius of 5 millimeters at a wavelength of 850 nanometers, the optical fiber has bending losses of less than 1 dB (e.g., less than 0.3 dB).
In yet another exemplary embodiment, for two turns around a bend radius of 5.5 millimeters at a wavelength of 850 nanometers, the optical fiber has bending losses of less than 0.1 dB.
In yet another exemplary embodiment, at a wavelength of 850 nanometers, the optical fiber has an overfilled launch (OFL) bandwidth of at least about 1,500 MHz·km.
In yet another exemplary embodiment, at a wavelength of 850 nanometers, the optical fiber has an overfilled launch (OFL) bandwidth of at least about 3,500 MHz·km.
In yet another exemplary embodiment, the optical fiber has a numerical aperture of between about 0.185 and 0.215.
In yet another exemplary embodiment, the central core's alpha index profile has an alpha parameter of between about 1.9 and 2.1.
In yet another exemplary embodiment, the central core's maximum refractive index difference Δn1 with respect to the outer cladding is between about 11×10−3 and 18×10−3 (e.g., between 13×10−3 and 16×10−3).
In yet another exemplary embodiment, at a wavelength of 850 nanometers, the optical fiber has an outer DMD value of less than 0.33 ps/m.
In yet another exemplary embodiment, at a wavelength of 850 nanometers, the optical fiber has an outer DMD value of less than 0.25 ps/m.
In yet another exemplary embodiment, at a wavelength of 850 nanometers, the optical fiber has an outer DMD value of less than 0.14 ps/m.
In another aspect, the present invention embraces an optical transmission system that includes a portion of an optical fiber in accordance with the foregoing.
In an exemplary embodiment, the optical system has a data rate of at least 10 Gb/s over at least 100 meters (e.g., 300 meters).
The foregoing illustrative summary, as well as other exemplary objectives and/or advantages of the invention, and the manner in which the same are accomplished, are further explained within the following detailed description and its accompanying drawings.
The present invention embraces a multimode optical fiber that achieves reduced bending losses and a high bandwidth with a reduced cladding effect. The present multimode optical fiber is especially suitable for high-data rate applications.
As noted,
Typically, the central core's alpha-index profile has a minimum refractive index value at the central core's radius r1 that is less than the refractive index value of the outer cladding. Thus, Δnend is negative when expressed as a refractive index difference with the outer cladding (e.g., ncore(r1)−ncladding). That said, in some alternative embodiments, the central core's refractive index difference Δnend may be zero (i.e., the central core's alpha-index profile may have a minimum refractive index value at the central core's radius r1 that is equal to that of the outer cladding).
In an exemplary embodiment, the central core's refractive index difference Δnend (i.e., at the end of the central core's alpha profile) is greater than about −1×10−3 and less than 0. Stated differently, with respect to the outer cladding, the central core has a negative refractive index difference Δnend of greater than about −1×10−3. Typically, the central core's refractive index difference Δnend is between −1×10−3 and −0.01×10−3 (e.g., between −0.8×10−3 and −0.2×10−3). More typically, the central core's refractive index difference Δnend is between about −0.7×10−3 and −0.3×10−3.
In another exemplary embodiment, the central core's refractive index difference Δnend (i.e., at the end of the central core's alpha profile) is between about −1×10−3 and 0. For example, the central core's refractive index difference Δnend may be between −0.8×10−3 and 0, such as between −0.7×10−3 and 0.
In a typical embodiment, the central core's radius r1 is about 25 microns. The central core's maximum refractive index difference Δn1 with respect to the outer cladding is typically between about 11×10−3 and 18×10−3 (e.g., between 13×10−3 and 16×10−3). Additionally, the alpha parameter of the central core's alpha-index profile is typically between about 1.9 and 2.1.
The optical fiber also includes an inner cladding positioned between the central core and the outer cladding (e.g., immediately surrounding the central core). The inner cladding has a radius r2, a width w2, and a refractive index difference Δn2 with respect to the outer cladding.
In some exemplary embodiments, the inner cladding's refractive index difference Δn2 is constant over the inner cladding's width w2. The absolute value of the inner cladding's refractive index difference Δn2 (i.e., |Δn2|) is typically greater than about 0.2×10−3 and less than 2×10−3. The inner cladding's width w2 is between about 0.5 micron and 2 microns.
In another exemplary embodiment, the central core's refractive index difference Δnend is zero and the inner cladding's refractive index difference Δn2 satisfies the following inequality:
0.2×10−3<|n2|.
A depressed trench is typically positioned between the inner cladding and the outer cladding (e.g., immediately surrounding the inner cladding). The depressed trench has a width w3, a radius rout, and a refractive index difference Δn3 with respect to the outer cladding.
Typically, the term “depressed trench” is used to describe a radial portion of an optical fiber that has a refractive index that is substantially less than the refractive index of the outer cladding. The depressed trench's refractive index difference Δn3 is typically between about −15×10−3 and −3×10−3 (e.g., between −10×10−3 and −5×10−3). The depressed trench's width w3 is typically between about 3 microns and 5 microns.
Generally speaking, a refractive index difference can also be expressed as a percentage using the following equation:
where n(r) is the comparative refractive index value as a function of radial position (e.g., the refractive index n3 of a depressed trench), and ncladding is the refractive index value of the outer cladding. Those of ordinary skill in the art will recognize that this equation can be used if the refractive index varies over a given section of the optical fiber (i.e., the refractive index value varies as a function of radial position) or if the refractive index is constant over a given section.
Those of ordinary skill in the art will recognize that the outer cladding typically has a constant refractive index. That said, if the outer cladding has a non-constant refractive index, refractive index differences are typically measured with respect to the innermost portion of the outer cladding (i.e., that portion of the outer cladding that is closest to the central core and that may affect the propagation of optical signals within the optical fiber).
A constant refractive index difference with respect to an outer cladding can also be expressed as a percentage using the following equation:
where n is the comparative refractive index value (e.g., the refractive index nt of a depressed trench), and ncladding is the refractive index value of the outer cladding.
As used herein, the volume v of a depressed trench is defined by the following equation:
in which rext and rint are the outer radius and inner radius of the depressed trench, respectively, and Δ % (r) is the depressed trench's refractive index difference with respect to the outer cladding expressed in percentage. Those of ordinary skill in the art will recognize that this equation can be used in the context of both non-rectangular and rectangular trenches.
If a depressed trench has a rectangular shape (i.e., a step index profile), the equation (above) can be simplified to the following equation:
ν=Δ%×π×(rext2−rint2)
in which rext and rint are the outer radius and inner radius of the depressed trench, respectively, and Δ % is the depressed trench's refractive index difference with respect to the outer cladding expressed in percentage.
Thus, in an exemplary optical fiber including a depressed trench that immediately surrounds an inner cladding, the depressed trench has a volume v3 defined by the following equations:
The depressed trench's volume v3 is typically between about 200%·μm2 and 1,200%·μm2 (e.g., between 250%·μm2 and 750%·μm2). Generally speaking, the characteristics of the second depressed trench facilitate the achievement of low bending losses.
In an exemplary embodiment, the inner cladding's refractive index difference Δn2 and the depressed trench's refractive index difference Δn3 satisfy the following inequality:
1000×Δn3<−1.29×(1000×Δn2)2−1.64×1000×Δn2−2.51.
Without being bound to any particular theory, the present inventors have found that the relationship between the inner cladding's refractive index difference Δn2 and the depressed trench's refractive index difference Δn3 achieves low bending losses while preserving a high bandwidth.
In some exemplary embodiments, at a wavelength of 850 nanometers, the optical fiber has bending losses for two turns around a bend radius of 15 millimeters of less than 0.1 dB (e.g., less than 0.05 dB); bending losses for two turns around a bend radius of 10 millimeters of less than 0.3 dB (e.g., less than 0.1 dB); bending losses for two turns around a bend radius of 7.5 millimeters of less than 0.4 dB (e.g., less than 0.2 dB); and bending losses for two turns around a bend radius of 5 millimeters of less than 1 dB (e.g., less than 0.3 dB).
Typically, the present optical fiber has higher bandwidth than prior art fibers. In particular, at a wavelength of 850 nanometers, the optical fiber may have an OFL bandwidth of at least 1500 MHz·km, such as 6,000 MHz·km or higher. More typically, the optical fiber exhibits an OFL bandwidth of at least 10,000 MHz·km.
As noted, however, OFL bandwidth is not the only parameter used to evaluate an optical fiber's suitability for high-data-rate applications. To improve optical fiber performance for high-data-rate applications, reducing the cladding effect in the optical fiber (e.g., at the core-cladding interface) can be important.
An optical fiber's cladding effect may also be evaluated using differential-mode-delay measurements acquired with an outer mask. For example, for a 50-micron central core (i.e., a central core diameter of 50±3 microns or radius of 25±1.5 microns), the differential-mode-delay value on the outer mask 0-23 microns can be obtained using the method of the FOTP-220 standard. In this regard, a differential mode delay value on the outer mask 0-23 microns (i.e., an outer DMD (0-23 microns)) is measured using the DMD method over the radial offset range from the center of the central core (i.e., 0 microns) to 23 microns. In other words, when calculating an optical fiber's outer DMD value, the signals for radial offset values greater than 23 microns are not considered. Those of ordinary skill in the art will recognize that the dimensions of an outer mask may be modified for optical fibers having larger or smaller core diameters. For example, a mask with larger dimensions (e.g., a larger inner and outer radius) might be used with respect to a multimode optical fiber having a 62.5-micron diameter core. Similarly, a mask with smaller dimensions (e.g., a smaller inner and outer radius) might be used with respect to a multimode optical fiber having a core that is less than 50 microns.
The outer DMD originates from a plot for DMD measured over 750 meters of optical fiber. The light source used may be a pulsed Ti:Sapphire laser emitting at 850 nanometers. The source emits pulses of less than 40 ps at quarter height, and the RMS (Root Mean Square) spectral width is less than 0.1 nanometer.
An exemplary optical fiber according to the present invention exhibits improved outer DMD values. In particular, at a wavelength of 850 nanometers, the exemplary optical fiber typically exhibits an outer DMD value of less than about 0.33 ps/m (e.g., less than 0.25 ps/m). More typically, the exemplary optical fiber exhibits an outer DMD value of 0.14 ps/m or less.
In some exemplary embodiments, the optical fiber employing a depressed trench with a small outer radius rout has high bandwidth and improved bending losses. The optical fiber's refractive index profile makes it possible to use a high depressed-trench volume v3, while limiting the combined width of the central core, the inner cladding, and the depressed trench. In other words, the optical fiber's refractive index profile achieves high bandwidth and low bending losses because of the depressed trench's volume, yet typically maintains a small depressed trench outer radius rout.
Those of ordinary skill in the art will understand that, when manufacturing a primary preform such as via a Plasma Chemical Vapor Deposition (PCVD) process, employing a depressed trench having a reduced outer radius rout permits thicker central core depositions. The primary preform may then be provided with an outer overcladding layer to achieve the desired ratio between the central core's radius and the final preform's outer radius. Increasing the thickness of the central core deposit allows a thicker outer overcladding layer to be provided during the overcladding process. Thus, larger final preforms can be achieved while maintaining the desired ratio between the central core's radius and the final preform's outer radius. Increasing the final preform's size permits more optical fiber to be drawn from the final preform. In sum, the smaller the depressed trench's outer radius rout, the more optical fiber that can be produced from a single optical preform. Furthermore, when the outer radius rout is small, it is easier to monitor the quality of the central core's alpha index profile. Thus, optical-fiber production costs can be reduced, and optical-fiber production speeds can be increased.
In some exemplary embodiments, the depressed trench's outer radius rout is about 32 microns or less (e.g., 30 microns or less). Additionally, at a wavelength of 850 nanometers, the exemplary optical fiber exhibits bending losses for two turns around a bend radius of 7.5 millimeters of 0.1 dB or less (e.g., 0.01 dB or less); bending losses for a half turn around a bending radius of 5.5 millimeters of 0.1 dB or less; and an outer DMD value of 0.1 ps/nm or less (e.g., 0.06 ps/nm or less). Consequently, the exemplary optical fiber makes it possible to achieve low bending losses and high bandwidth with a limited outer radius rout. Furthermore, the exemplary optical fiber facilitates reduced production costs and an enhanced production rate.
According to another exemplary embodiment, the optical fiber according to the present invention complies with the OM3 standard. In particular, at a wavelength of 850 nanometers, the optical fiber has (i) an effective modal bandwidth (EMB) greater than 2,000 MHz·km; (ii) an outer DMD value of less than 0.3 ps/m; (iii) an OFL bandwidth greater than 1,500 MHz·km; and (iv) a numerical aperture of between 0.185 and 0.215.
In one exemplary embodiment, the inner cladding's refractive index difference Δn2 and the depressed trench's refractive index difference Δn3 satisfy both of the following inequalities:
−1.89×(1000×Δn2)2−7.03×(1000×Δn2)−9.91<1000×Δn3; and
1000×Δn3<−1.53×(1000×Δn2)2−3.34×1000×Δn2−4.25.
The optical fiber of this exemplary embodiment has a bandwidth of at least about 4,700 MHz·km (e.g., at least 6,000 MHz·km, such as 10,000 MHz·km) with low bending losses. Additionally, this exemplary optical fiber typically complies with the OM4 standard. In particular, at a wavelength of 850 nanometers, the optical fiber has (i) an effective modal bandwidth (EMB) of at least 4,700 MHz·km, (ii) an outer DMD value of less than 0.14 ps/m, (iii) an OFL bandwidth greater than 3,500 MHz·km, and (iv) a numerical aperture of between 0.185 and 0.215.
The invention will be better understood with the help of the exemplary optical fiber profiles given in Table 1. Table 1 (below) shows simulated fiber-profile-parameters and performance characteristics of exemplary optical fibers in accordance with the present invention.
The first column of Table 1 provides the reference number for each exemplary optical fiber. The second and third columns, respectively, show the inner cladding's width w2 and the depressed trench's width w3. The fourth and fifth columns, respectively, show the inner cladding's refractive index difference Δn2 and the depressed trench's refractive index difference Δn3. The sixth column shows the depressed trench's refractive index difference Δ3% expressed in percentage. The seventh column shows the depressed trench's volume v3. The final four columns show outer DMD values, OFL bandwidth at 850 nanometers, bending losses for two turns around a bend radius of 5 millimeters at 850 nanometers, and bending losses for two turns around a bend radius of 7.5 millimeters at 850 nanometers.
Exemplary optical fibers 1 and 2 have negative inner cladding refractive index differences Δn2. Exemplary optical fibers 3 through 11 have positive inner cladding refractive index differences Δn2. Examples 1 through 11 show that increasing the depressed trench's volume v3 reduces bending losses to 0.041 dB for a 5-millimeter bending radius and to 0.008 dB for a 7.5-millimeter bending radius. Additionally, the outer DMD value and OFL bandwidth are not adversely affected. Thus, adjusting the inner cladding's refractive index difference Δn2 and the depressed trench's refractive index difference Δn3 decreases bending losses while preserving an outer DMD value of about 0.06 ps/m and an OFL bandwidth higher than 13200 MHz·km.
According to one embodiment, the optical fiber of the present invention complies with ITU-T Recommendation G.651.1. Thus, it has a central-core diameter of 50 microns (i.e., a central-core radius r1 of 25 microns) and/or a numerical aperture of 0.2±0.015.
In another aspect, the present invention embraces a multimode optical system that includes at least a portion of an optical fiber as disclosed herein in accordance with the present invention. In particular, the optical system can exhibit a data rate of at least 10 Gb/s over at least 100 meters (e.g., 300 meters).
The present optical fibers may facilitate the reduction in overall optical-fiber diameter. As will be appreciated by those having ordinary skill in the art, a reduced-diameter optical fiber is cost-effective, requiring less raw material. Moreover, a reduced-diameter optical fiber requires less deployment space (e.g., within a buffer tube and/or fiber optic cable), thereby facilitating increased fiber count and/or reduced cable size.
Those having ordinary skill in the art will recognize that an optical fiber with a primary coating (and an optional secondary coating and/or ink layer) typically has an outer diameter of between about 235 microns and about 265 microns (μm). The component glass fiber itself (i.e., the glass core and surrounding cladding layers) typically has a diameter of about 125 microns, such that the total coating thickness is typically between about 55 microns and 70 microns.
With respect to the present optical fiber, the component glass fiber typically has an outer diameter of about 125 microns. With respect to the optical fiber's surrounding coating layers, the primary coating typically has an outer diameter of between about 175 microns and about 195 microns (i.e., a primary coating thickness of between about 25 microns and 35 microns), and the secondary coating typically has an outer diameter of between about 235 microns and about 265 microns (i.e., a secondary coating thickness of between about 20 microns and 45 microns). Optionally, the present optical fiber may include an outermost ink layer, which is typically between two and ten microns in thickness.
In one alternative embodiment, an optical fiber may possess a reduced diameter (e.g., an outermost diameter between about 150 microns and 230 microns). In this alternative optical fiber configuration, the thickness of the primary coating and/or secondary coating is reduced, while the diameter of the component glass fiber is maintained at about 125 microns. (Those having ordinary skill in the art will appreciate that, unless otherwise specified, diameter measurements refer to outer diameters.)
By way of illustration, in such exemplary embodiments the primary coating layer may have an outer diameter of between about 135 microns and about 175 microns (e.g., about 160 microns), typically less than 165 microns (e.g., between about 135 microns and 150 microns), and usually more than 140 microns (e.g., between about 145 microns and 155 microns, such as about 150 microns).
Moreover, in such exemplary embodiments the secondary coating layer may have an outer diameter of between about 150 microns and about 230 microns (e.g., more than about 165 microns, such as 190-210 microns or so), typically between about 180 microns and 200 microns. In other words, the total diameter of the optical fiber is reduced to less than about 230 microns (e.g., between about 195 microns and 205 microns, and especially about 200 microns). By way of further illustration, an optical fiber may employ a secondary coating of about 197 microns at a tolerance of +/−5 microns (i.e., a secondary-coating outer diameter of between 192 microns to 202 microns). Typically, the secondary coating will retain a thickness of at least about 10 microns (e.g., an optical fiber having a reduced thickness secondary coating of between 15 microns and 25 microns).
In another alternative embodiment, the outer diameter of the component glass fiber may be reduced to less than 125 microns (e.g., between about 60 microns and 120 microns), perhaps between about 70 microns and 115 microns (e.g., about 80-110 microns). This may be achieved, for instance, by reducing the thickness of one or more cladding layers. As compared with the prior alternative embodiment, (i) the total diameter of the optical fiber may be reduced (i.e., the thickness of the primary and secondary coatings are maintained in accordance with the prior alternative embodiment) or (ii) the respective thicknesses of the primary and/or secondary coatings may be increased relative to the prior alternative embodiment (e.g., such that the total diameter of the optical fiber might be maintained).
By way of illustration, with respect to the former, a component glass fiber having a diameter of between about 90 and 100 microns might be combined with a primary coating layer having an outer diameter of between about 110 microns and 150 microns (e.g., about 125 microns) and a secondary coating layer having an outer diameter of between about 130 microns and 190 microns (e.g., about 155 microns). With respect to the latter, a component glass fiber having a diameter of between about 90 and 100 microns might be combined with a primary coating layer having an outer diameter of between about 120 microns and 140 microns (e.g., about 130 microns) and a secondary coating layer having an outer diameter of between about 160 microns and 230 microns (e.g., about 195-200 microns).
Reducing the diameter of the component glass fiber might make the resulting optical fiber more susceptible to microbending attenuation. That said, the advantages of further reducing optical-fiber diameter may be worthwhile for some optical-fiber applications.
As noted, the present optical fibers may include one or more coating layers (e.g., a primary coating and a secondary coating). At least one of the coating layers—typically the secondary coating—may be colored and/or possess other markings to help identify individual fibers. Alternatively, a tertiary ink layer may surround the primary and secondary coatings.
The present optical fibers may be manufactured by drawing from final preforms.
A final preform may be manufactured by providing a primary preform with an outer overcladding layer (i.e., an overcladding process). The outer overcladding layer typically consists of doped or undoped, natural or synthetic, silica glass. Several methods are available for providing the outer overcladding layer.
In a first exemplary method, the outer overcladding layer may be provided by depositing and vitrifying natural or synthetic silica particles on the outer periphery of the primary preform under the influence of heat. Such a process is known, for example, from U.S. Pat. Nos. 5,522,007, 5,194,714, 6,269,663, and 6,202,447, each of which is hereby incorporated by reference in its entirety.
In another exemplary method, a primary preform may be overcladded using a silica sleeve tube, which may or may not be doped. This sleeve tube may then be collapsed onto the primary preform.
In yet another exemplary method, an overcladding layer may be applied via an Outside Vapor Deposition (OVD) method. Here, a soot layer is first deposited on the outer periphery of a primary preform, and then the soot layer is vitrified to form glass.
The primary preforms may be manufactured via outside vapor deposition techniques, such as Outside Vapor Deposition (OVD) and Vapor Axial Deposition (VAD). Alternatively, the primary preforms may be manufactured via inside deposition techniques in which glass layers are deposited on the inner surface of a substrate tube of doped or undoped silica glass, such as Modified Chemical Vapor Deposition (MCVD), Furnace Chemical Vapor Deposition (FCVD), and Plasma Chemical Vapor Deposition (PCVD).
By way of example, the primary preforms may be manufactured using a PCVD process, which can precisely control the central core's gradient refractive index profile.
A depressed trench, for instance, may be deposited on the inner surface of a substrate tube as part of the chemical vapor deposition process. More typically, a depressed trench may be manufactured either (i) by using a fluorine-doped substrate tube as the starting point of the internal deposition process for deposition of the gradient refractive index central core or (ii) by sleeving a fluorine-doped silica tube over the gradient refractive index central core, which itself may be produced using an outside deposition process (e.g., OVD or VAD). Accordingly, a component glass fiber manufactured from the resulting preform may have a depressed trench located at the periphery of its central core.
As noted, a primary preform may be manufactured via an inside deposition process using a fluorine-doped substrate tube. The resulting tube containing the deposited layers may be sleeved by one or more additional fluorine-doped silica tubes so as to increase the thickness of a depressed trench, or to create a depressed trench having a varying refractive index over its width. Although not required, one or more additional sleeve tubes (e.g., fluorine-doped substrate tubes) may be collapsed onto the primary preform before an overcladding step is carried out. The process of sleeving and collapsing is sometimes referred to as jacketing and may be repeated to build several glass layers on the outside of the primary preform.
The present optical fibers may be deployed in various structures, such as those exemplary structures disclosed hereinafter.
For example, one or more of the present optical fibers may be enclosed within a buffer tube. For instance, optical fiber may be deployed in either a single-fiber loose buffer tube or a multi-fiber loose buffer tube. With respect to the latter, multiple optical fibers may be bundled or stranded within a buffer tube or other structure. In this regard, within a multi-fiber loose buffer tube, fiber sub-bundles may be separated with binders (e.g., each fiber sub-bundle is enveloped in a binder). Moreover, fan-out tubing may be installed at the termination of such loose buffer tubes to directly terminate loose buffered optical fibers with field-installed connectors.
In other embodiments, the buffer tube may tightly surround the outermost optical fiber coating (i.e., tight buffered fiber) or otherwise surround the outermost optical-fiber coating or ink layer to provide an exemplary radial clearance of between about 50 and 100 microns (i.e., a semi-tight buffered fiber).
With respect to the former tight buffered fiber, the buffering may be formed by coating the optical fiber with a curable composition (e.g., a UV-curable material) or a thermoplastic material. The outer diameter of tight buffer tubes, regardless of whether the buffer tube is formed from a curable or non-curable material, is typically less than about 1,000 microns (e.g., either about 500 microns or about 900 microns).
With respect to the latter semi-tight buffered fiber, a lubricant may be included between the optical fiber and the buffer tube (e.g., to provide a gliding layer).
As will be known by those having ordinary skill in the art, an exemplary buffer tube enclosing optical fibers as disclosed herein may be formed of polyolefins (e.g., polyethylene or polypropylene), including fluorinated polyolefins, polyesters (e.g., polybutylene terephthalate), polyamides (e.g., nylon), as well as other polymeric materials and blends. In general, a buffer tube may be formed of one or more layers. The layers may be homogeneous or include mixtures or blends of various materials within each layer.
In this context, the buffer tube may be extruded (e.g., an extruded polymeric material) or pultruded (e.g., a pultruded, fiber-reinforced plastic). By way of example, the buffer tube may include a material to provide high temperature and chemical resistance (e.g., an aromatic material or polysulfone material).
Although buffer tubes typically have a circular cross section, buffer tubes alternatively may have an irregular or non-circular shape (e.g., an oval or a trapezoidal cross-section).
Alternatively, one or more of the present optical fibers may simply be surrounded by an outer protective sheath or encapsulated within a sealed metal tube. In either structure, no intermediate buffer tube is necessarily required.
Multiple optical fibers as disclosed herein may be sandwiched, encapsulated, and/or edge bonded to form an optical fiber ribbon. Optical fiber ribbons can be divisible into subunits (e.g., a twelve-fiber ribbon that is splittable into six-fiber subunits). Moreover, a plurality of such optical fiber ribbons may be aggregated to form a ribbon stack, which can have various sizes and shapes.
For example, it is possible to form a rectangular ribbon stack or a ribbon stack in which the uppermost and lowermost optical fiber ribbons have fewer optical fibers than those toward the center of the stack. This construction may be useful to increase the density of optical elements (e.g., optical fibers) within the buffer tube and/or cable.
In general, it is desirable to increase the filling of transmission elements in buffer tubes or cables, subject to other constraints (e.g., cable or mid-span attenuation). The optical elements themselves may be designed for increased packing density. For example, the optical fiber may possess modified properties, such as improved refractive-index profile, core or cladding dimensions, or primary-coating thickness and/or modulus, to improve microbending and macrobending characteristics.
By way of example, a rectangular ribbon stack may be formed with or without a central twist (i.e., a “primary twist”). Those having ordinary skill in the art will appreciate that a ribbon stack is typically manufactured with rotational twist to allow the tube or cable to bend without placing excessive mechanical stress on the optical fibers during winding, installation, and use. In a structural variation, a twisted (or untwisted) rectangular ribbon stack may be further formed into a coil-like configuration (e.g., a helix) or a wave-like configuration (e.g., a sinusoid). In other words, the ribbon stack may possess regular “secondary” deformations.
As will be known to those having ordinary skill in the art, such optical fiber ribbons may be positioned within a buffer tube or other surrounding structure, such as a buffer-tube-free cable. Subject to certain restraints (e.g., attenuation), it is desirable to increase the density of elements such as optical fibers or optical fiber ribbons within buffer tubes and/or optical fiber cables.
A plurality of buffer tubes containing optical fibers (e.g., loose or ribbonized fibers) may be positioned externally adjacent to and stranded around a central strength member. This stranding can be accomplished in one direction, helically, known as “S” or “Z” stranding, or Reverse Oscillated Lay stranding, known as “S-Z” stranding. Stranding about the central strength member reduces optical fiber strain when cable strain occurs during installation and use.
Those having ordinary skill in the art will understand the benefit of minimizing fiber strain for both tensile cable strain and longitudinal compressive cable strain during installation or operating conditions.
With respect to tensile cable strain, which may occur during installation, the cable will become longer while the optical fibers can migrate closer to the cable's neutral axis to reduce, if not eliminate, the strain being translated to the optical fibers. With respect to longitudinal compressive strain, which may occur at low operating temperatures due to shrinkage of the cable components, the optical fibers will migrate farther away from the cable's neutral axis to reduce, if not eliminate, the compressive strain being translated to the optical fibers.
In a variation, two or more substantially concentric layers of buffer tubes may be positioned around a central strength member. In a further variation, multiple stranding elements (e.g., multiple buffer tubes stranded around a strength member) may themselves be stranded around each other or around a primary central strength member.
Alternatively, a plurality of buffer tubes containing optical fibers (e.g., loose or ribbonized fibers) may be simply placed externally adjacent to the central strength member (i.e., the buffer tubes are not intentionally stranded or arranged around the central strength member in a particular manner and run substantially parallel to the central strength member).
Alternatively still, the present optical fibers may be positioned within a central buffer tube (i.e., the central buffer tube cable has a central buffer tube rather than a central strength member). Such a central buffer tube cable may position strength members elsewhere. For instance, metallic or non-metallic (e.g., GRP) strength members may be positioned within the cable sheath itself, and/or one or more layers of high-strength yarns (e.g., aramid or non-aramid yarns) may be positioned parallel to or wrapped (e.g., contrahelically) around the central buffer tube (i.e., within the cable's interior space). As will be understood by those having ordinary skill in the art, such strength yarns provide tensile strength to fiber optic cables. Likewise, strength members can be included within the buffer tube's casing.
Strength yarns may be coated with a lubricant (e.g., fluoropolymers), which may reduce unwanted attenuation in fiber optic cables (e.g., rectangular, flat ribbon cables or round, loose tube cables) that are subjected to relatively tight bends (i.e., a low bend radius). Moreover, the presence of a lubricant on strength yarns (e.g., aramid strength yarns) may facilitate removal of the cable jacketing by reducing unwanted bonding between the strength yarns and the surrounding cable jacket.
In other embodiments, the optical fibers may be placed within a slotted core cable. In a slotted core cable, optical fibers, individually or as a fiber ribbon, may be placed within pre-shaped helical grooves (i.e., channels) on the surface of a central strength member, thereby forming a slotted core unit. The slotted core unit may be enclosed by a buffer tube. One or more of such slotted core units may be placed within a slotted core cable. For example, a plurality of slotted core units may be helically stranded around a central strength member.
Alternatively, the optical fibers may also be stranded in a maxitube cable design, whereby the optical fibers are stranded around themselves within a large multi-fiber loose buffer tube rather than around a central strength member. In other words, the large multi-fiber loose buffer tube is centrally positioned within the maxitube cable. For example, such maxitube cables may be deployed in optical ground wires (OPGW).
In another cabling embodiment, multiple buffer tubes may be stranded around themselves without the presence of a central member. These stranded buffer tubes may be surrounded by a protective tube. The protective tube may serve as the outer casing of the fiber optic cable or may be further surrounded by an outer sheath. The protective tube may tightly or loosely surround the stranded buffer tubes.
As will be known to those having ordinary skill in the art, additional elements may be included within a cable core. For example, copper cables or other active, transmission elements may be stranded or otherwise bundled within the cable sheath. Passive elements may also be placed within the cable core, such as between the interior walls of the buffer tubes and the enclosed optical fibers. Alternatively and by way of example, passive elements may be placed outside the buffer tubes between the respective exterior walls of the buffer tubes and the interior wall of the cable jacket, or within the interior space of a buffer-tube-free cable.
For example, yarns, nonwovens, fabrics (e.g., tapes), foams, or other materials containing water-swellable material and/or coated with water-swellable materials (e.g., including super absorbent polymers (SAPs), such as SAP powder) may be employed to provide water blocking and/or to couple the optical fibers to the surrounding buffer tube and/or cable jacketing (e.g., via adhesion, friction, and/or compression). Exemplary water-swellable elements are disclosed in commonly assigned U.S. Pat. No. 7,515,795 for a Water-Swellable Tape, Adhesive-Backed for Coupling When Used Inside a Buffer Tube, which is hereby incorporated by reference in its entirety.
Moreover, an adhesive (e.g., a hot-melt adhesive or curable adhesive, such as a silicone acrylate cross-linked by exposure to actinic radiation) may be provided on one or more passive elements (e.g., water-swellable material) to bond the elements to the buffer tube. An adhesive material may also be used to bond the water-swellable element to optical fibers within the buffer tube. Exemplary arrangements of such elements are disclosed in commonly assigned U.S. Pat. No. 7,599,589 for a Gel-Free Buffer Tube with Adhesively Coupled Optical Element, which is hereby incorporated by reference in its entirety.
The buffer tubes (or buffer-tube-free cables) may also contain a thixotropic composition (e.g., grease or grease-like gels) between the optical fibers and the interior walls of the buffer tubes. For example, filling the free space inside a buffer tube with water-blocking, petroleum-based filling grease helps to block the ingress of water. Further, the thixotropic filling grease mechanically (i.e., viscously) couples the optical fibers to the surrounding buffer tube.
Such thixotropic filling greases are relatively heavy and messy, thereby hindering connection and splicing operations. Thus, the present optical fibers may be deployed in dry cable structures (i.e., grease-free buffer tubes).
Exemplary buffer tube structures that are free from thixotropic filling greases are disclosed in commonly assigned U.S. Pat. No. 7,724,998 for a Coupling Composition for Optical Fiber Cables (Parris et al.), which is hereby incorporated by reference in its entirety. Such buffer tubes employ coupling compositions formed from a blend of high-molecular weight elastomeric polymers (e.g., about 35 weight percent or less) and oils (e.g., about 65 weight percent or more) that flow at low temperatures. Unlike thixotropic filling greases, the coupling composition (e.g., employed as a cohesive gel or foam) is typically dry and, therefore, less messy during splicing.
As will be understood by those having ordinary skill in the art, a cable enclosing optical fibers as disclosed herein may have a sheath formed from various materials in various designs. Cable sheathing may be formed from polymeric materials such as, for example, polyethylene, polypropylene, polyvinyl chloride (PVC), polyamides (e.g., nylon), polyester (e.g., PBT), fluorinated plastics (e.g., perfluoroethylene propylene, polyvinyl fluoride, or polyvinylidene difluoride), and ethylene vinyl acetate. The sheath and/or buffer tube materials may also contain other additives, such as nucleating agents, flame-retardants, smoke-retardants, antioxidants, UV absorbers, and/or plasticizers.
The cable sheathing may be a single jacket formed from a dielectric material (e.g., non-conducting polymers), with or without supplemental structural components that may be used to improve the protection (e.g., from rodents) and strength provided by the cable sheath. For example, one or more layers of metallic (e.g., steel) tape, along with one or more dielectric jackets, may form the cable sheathing. Metallic or fiberglass reinforcing rods (e.g., GRP) may also be incorporated into the sheath. In addition, aramid, fiberglass, or polyester yarns may be employed under the various sheath materials (e.g., between the cable sheath and the cable core), and/or ripcords may be positioned, for example, within the cable sheath.
Similar to buffer tubes, optical fiber cable sheaths typically have a circular cross section, but cable sheaths alternatively may have an irregular or non-circular shape (e.g., an oval, trapezoidal, or flat cross-section).
By way of example, the present optical fiber may be incorporated into single-fiber drop cables, such as those employed for Multiple Dwelling Unit (MDU) applications. In such deployments, the cable jacketing must exhibit crush resistance, abrasion resistance, puncture resistance, thermal stability, and fire resistance as required by building codes. An exemplary material for such cable jackets is thermally stable, flame-retardant polyurethane (PUR), which mechanically protects the optical fibers yet is sufficiently flexible to facilitate easy MDU installations. Alternatively, a flame-retardant polyolefin or polyvinyl chloride sheath may be used.
In general, and as will be known to those having ordinary skill in the art, a strength member is typically in the form of a rod or braided/helically wound wires or fibers, though other configurations will be within the knowledge of those having ordinary skill in the art.
Optical fiber cables containing optical fibers as disclosed may be variously deployed, including as drop cables, distribution cables, feeder cables, trunk cables, and stub cables, each of which may have varying operational requirements (e.g., temperature range, crush resistance, UV resistance, and minimum bend radius).
Such optical fiber cables may be installed within ducts, microducts, plenums, or risers. By way of example, an optical fiber cable may be installed in an existing duct or microduct by pulling or blowing (e.g., using compressed air). An exemplary cable installation method is disclosed in commonly assigned U.S. Pat. No. 7,574,095 for a Communication Cable Assembly and Installation Method, (Lock et al.), and U.S. Pat. No. 7,665,902 for a Modified Pre-Ferrulized Communication Cable Assembly and Installation Method, (Griffioen et al.), each of which is incorporated by reference in its entirety.
As noted, buffer tubes containing optical fibers (e.g., loose or ribbonized fibers) may be stranded (e.g., around a central strength member). In such configurations, an optical fiber cable's protective outer sheath may have a textured outer surface that periodically varies lengthwise along the cable in a manner that replicates the stranded shape of the underlying buffer tubes. The textured profile of the protective outer sheath can improve the blowing performance of the optical fiber cable. The textured surface reduces the contact surface between the cable and the duct or microduct and increases the friction between the blowing medium (e.g., air) and the cable. The protective outer sheath may be made of a low coefficient-of-friction material, which can facilitate blown installation. Moreover, the protective outer sheath can be provided with a lubricant to further facilitate blown installation.
In general, to achieve satisfactory long-distance blowing performance (e.g., between about 3,000 to 5,000 feet or more), the outer cable diameter of an optical fiber cable should be no more than about 70 to 80 percent of the duct's or microduct's inner diameter.
Compressed air may also be used to install optical fibers in an air blown fiber system. In an air blown fiber system, a network of unfilled cables or microducts is installed prior to the installation of optical fibers. Optical fibers may subsequently be blown into the installed cables as necessary to support the network's varying requirements.
Moreover, the optical fiber cables may be directly buried in the ground or, as an aerial cable, suspended from a pole or pylori. An aerial cable may be self-supporting, or secured or lashed to a support (e.g., messenger wire or another cable). Exemplary aerial fiber optic cables include overhead ground wires (OPGW), all-dielectric self-supporting cables (ADSS), all dielectric lash cables (AD-Lash), and figure-eight cables, each of which is well understood by those having ordinary skill in the art. Figure-eight cables and other designs can be directly buried or installed into ducts, and may optionally include a toning element, such as a metallic wire, so that they can be found with a metal detector.
In addition, although the optical fibers may be further protected by an outer cable sheath, the optical fiber itself may be further reinforced so that the optical fiber may be included within a breakout cable, which allows for the individual routing of individual optical fibers.
To effectively employ the present optical fibers in a transmission system, connections are required at various points in the network. Optical fiber connections are typically made by fusion splicing, mechanical splicing, or mechanical connectors.
The mating ends of connectors can be installed to the optical fiber ends either in the field (e.g., at the network location) or in a factory prior to installation into the network. The ends of the connectors are mated in the field in order to connect the optical fibers together or connect the optical fibers to the passive or active components. For example, certain optical fiber cable assemblies (e.g., furcation assemblies) can separate and convey individual optical fibers from a multiple optical fiber cable to connectors in a protective manner.
The deployment of such optical fiber cables may include supplemental equipment, which itself may employ the present optical fiber as previously disclosed. For instance, an amplifier may be included to improve optical signals. Dispersion compensating modules may be installed to reduce the effects of chromatic dispersion and polarization mode dispersion. Splice boxes, pedestals, and distribution frames, which may be protected by an enclosure, may likewise be included. Additional elements include, for example, remote terminal switches, optical network units, optical splitters, and central office switches.
A cable containing the present optical fibers may be deployed for use in a communication system (e.g., networking or telecommunications). A communication system may include fiber optic cable architecture such as fiber-to-the-node (FTTN), fiber-to-the-telecommunications enclosure (FTTE), fiber-to-the-curb (FTTC), fiber-to-the-building (FTTB), and fiber-to-the-home (FTTH), as well as long-haul or metro architecture. Moreover, an optical module or a storage box that includes a housing may receive a wound portion of the optical fiber disclosed herein. By way of example, the optical fiber may be wound around a bending radius of less than about 15 millimeters (e.g., 10 millimeters or less, such as about 5 millimeters) in the optical module or the storage box.
Moreover, present optical fibers may be used in other applications, including, without limitation, fiber optic sensors or illumination applications (e.g., lighting).
The present optical fibers may include Fiber Bragg Grating (FBG). As will be known by those having ordinary skill in the art, FBG is a periodic or aperiodic variation in the refractive index of an optical fiber core and/or cladding. This variation in the refractive index results in a range of wavelengths (e.g., a narrow range) being reflected rather than transmitted, with maximum reflectivity occurring at the Bragg wavelength.
Fiber Bragg Grating is commonly written into an optical fiber by exposing the optical fiber to an intense source of ultraviolet light (e.g., a UV laser). In this respect, UV photons may have enough energy to break molecular bonds within an optical fiber, which alters the structure of the optical fiber, thereby increasing the optical fiber's refractive index. Moreover, dopants (e.g., boron or germanium) and/or hydrogen loading can be employed to increase photosensitivity.
In order to expose a coated glass fiber to UV light for the creation of FBG, the coating may be removed. Alternatively, coatings that are transparent at the particular UV wavelengths (e.g., the UV wavelengths emitted by a UV laser to write FBG) may be employed to render coating removal unnecessary. In addition, silicone, polyimide, acrylate, or PFCB coatings, for instance, may be employed for high-temperature applications.
A particular FBG pattern may be created by employing (i) a photomask placed between the UV light source and the optical fiber, (ii) interference between multiple UV light beams, which interfere with each other in accordance with the desired FBG pattern (e.g., a uniform, chirped, or titled pattern), or (iii) a narrow UV light beam for creating individual variations. The FBG structure may have, for example, a uniform positive-only index change, a Gaussian-apodized index change, a raised-cosine-apodized index change, or a discrete phase shift index change. Multiple FBG patterns may be combined on a single optical fiber.
Optical fibers having FBG may be employed in various sensing applications (e.g., for detecting vibration, temperature, pressure, moisture, or movement). In this respect, changes in the optical fiber (e.g., a change in temperature) result in a shift in the Bragg wavelength, which is measured by a sensor. FBG may be used to identify a particular optical fiber (e.g., if the optical fiber is broken into pieces).
Fiber Bragg Grating may also be used in various active or passive communication components (e.g., wavelength-selective filters, multiplexers, demultiplexers, Mach-Zehnder interferometers, distributed Bragg reflector lasers, pump/laser stabilizers, and supervisory channels).
To supplement the present disclosure, this application incorporates entirely by reference the following commonly assigned patents, patent application publications, and patent applications: U.S. Pat. No. 4,838,643 for a Single Mode Bend Insensitive Fiber for Use in Fiber Optic Guidance Applications (Hodges et al.); U.S. Pat. No. 7,623,747 for a Single Mode Optical Fiber (de Montmorillon et al.); U.S. Pat. No. 7,587,111 for a Single-Mode Optical Fiber (de Montmorillon et al.); U.S. Pat. No. 7,356,234 for a Chromatic Dispersion Compensating Fiber (de Montmorillon et al.); U.S. Pat. No. 7,483,613 for a Chromatic Dispersion Compensating Fiber (Bigot-Astruc et al.); U.S. Pat. No. 7,555,186 for an Optical Fiber (Flammer et al.); U.S. Patent Application Publication No. US2009/0252469 A1 for a Dispersion-Shifted Optical Fiber (Sillard et al.); U.S. patent application Ser. No. 12/098,804 for a Transmission Optical Fiber Having Large Effective Area (Sillard et al.), filed Apr. 7, 2008; International Patent Application Publication No. WO 2009/062131 A1 for a Microbend-Resistant Optical Fiber, (Overton); U.S. Patent Application Publication No. US2009/0175583 A1 for a Microbend-Resistant Optical Fiber, (Overton); U.S. Patent Application Publication No. US2009/0279835 A1 for a Single-Mode Optical Fiber Having Reduced Bending Losses, filed May 6, 2009, (de Montmorillon et al.); U.S. Patent Application Publication No. US2009/0279836 A1 for a Bend-Insensitive Single-Mode Optical Fiber, filed May 6, 2009, (de Montmorillon et al.); U.S. Patent Application Publication No. US2010/0021170 A1 for a Wavelength Multiplexed Optical System with Multimode Optical Fibers, filed Jun. 23, 2009, (Lumineau et al.); U.S. Patent Application Publication No. US2010/0028020 A1 for a Multimode Optical Fibers, filed Jul. 7, 2009, (Gholami et al.); U.S. Patent Application Publication No. US2010/0119202 A1 for a Reduced-Diameter Optical Fiber, filed Nov. 6, 2009, (Overton); U.S. Patent Application Publication No. US2010/0142969 A1 for a Multimode Optical System, filed Nov. 6, 2009, (Gholami et al.); U.S. Patent Application Publication No. US2010/0118388 A1 for an Amplifying Optical Fiber and Method of Manufacturing, filed Nov. 12, 2009, (Pastouret et al.); U.S. Patent Application Publication No. US2010/0135627 A1 for an Amplifying Optical Fiber and Production Method, filed Dec. 2, 2009, (Pastouret et al.); U.S. Patent Application Publication No. US2010/0142033 for an Ionizing Radiation-Resistant Optical Fiber Amplifier, filed Dec. 8, 2009, (Regnier et al.); U.S. Patent Application Publication No. US2010/0150505 A1 for a Buffered Optical Fiber, filed Dec. 11, 2009, (Testu et al.); U.S. Patent Application Publication No. US2010/0171945 for a Method of Classifying a Graded-Index Multimode Optical Fiber, filed Jan. 7, 2010, (Gholami et al.); U.S. Patent Application Publication No. US2010/0189397 A1 for a Single-Mode Optical Fiber, filed Jan. 22, 2010, (Richard et al.); U.S. Patent Application Publication No. US2010/0189399 A1 for a Single-Mode Optical Fiber Having an Enlarged Effective Area, filed Jan. 27, 2010, (Sillard et al.); U.S. Patent Application Publication No. US2010/0189400 A1 for a Single-Mode Optical Fiber, filed Jan. 27, 2010, (Sillard et al.); U.S. Patent Application Publication No. US2010/0214649 A1 for a Optical Fiber Amplifier Having Nanostructures, filed Feb. 19, 2010, (Burov et al.); U.S. Patent Application Publication No. US2010/0254653 A1 for a Multimode Fiber, filed Apr. 22, 2010, (Molin et al.); U.S. patent application Ser. No. 12/794,229 for a Large Bandwidth Multimode Optical Fiber Having a Reduced Cladding Effect, filed Jun. 4, 2010, (Molin et al.); U.S. patent application Ser. No. 12/878,449 for a Multimode Optical Fiber Having Improved Bending Losses, filed Sep. 9, 2010, (Molin et al.); U.S. patent application Ser. No. 12/884,834 for a Multimode Optical Fiber, filed Sep. 17, 2010, (Molin et al.); U.S. patent application Ser. No. 12/887,813 for a Optical Fiber for Sum-Frequency Generation, filed Sep. 22, 2010, (Richard et al.); U.S. patent application Ser. No. 12/953,948 for a High-Bandwidth, Multimode Optical Fiber with Reduced Cladding Effect, filed Nov. 24, 2010, (Molin et al.); U.S. patent application Ser. No. 12/954,036 for a High-Bandwidth, Dual-Trench-Assisted Multimode Optical Fiber, filed Nov. 24, 2010, (Molin et al.); and U.S. patent application Ser. No. 12/959,688 for a Multimode Optical Fiber with Low Bending Losses and Reduced Cladding Effect, filed Dec. 3, 2010, (Molin et al.).
To supplement the present disclosure, this application further incorporates entirely by reference the following commonly assigned patents, patent application publications, and patent applications: U.S. Pat. No. 5,574,816 for Polypropylene-Polyethylene Copolymer Buffer Tubes for Optical Fiber Cables and Method for Making the Same; U.S. Pat. No. 5,717,805 for Stress Concentrations in an Optical Fiber Ribbon to Facilitate Separation of Ribbon Matrix Material; U.S. Pat. No. 5,761,362 for Polypropylene-Polyethylene Copolymer Buffer Tubes for Optical Fiber Cables and Method for Making the Same; U.S. Pat. No. 5,911,023 for Polyolefin Materials Suitable for Optical Fiber Cable Components; U.S. Pat. No. 5,982,968 for Stress Concentrations in an Optical Fiber Ribbon to Facilitate Separation of Ribbon Matrix Material; U.S. Pat. No. 6,035,087 for an Optical Unit for Fiber Optic Cables; U.S. Pat. No. 6,066,397 for Polypropylene Filler Rods for Optical Fiber Communications Cables; U.S. Pat. No. 6,175,677 for an Optical Fiber Multi-Ribbon and Method for Making the Same; U.S. Pat. No. 6,085,009 for Water Blocking Gels Compatible with Polyolefin Optical Fiber Cable Buffer Tubes and Cables Made Therewith; U.S. Pat. No. 6,215,931 for Flexible Thermoplastic Polyolefin Elastomers for Buffering Transmission Elements in a Telecommunications Cable; U.S. Pat. No. 6,134,363 for a Method for Accessing Optical Fibers in the Midspan Region of an Optical Fiber Cable; U.S. Pat. No. 6,381,390 for a Color-Coded Optical Fiber Ribbon and Die for Making the Same; U.S. Pat. No. 6,181,857 for a Method for Accessing Optical Fibers Contained in a Sheath; U.S. Pat. No. 6,314,224 for a Thick-Walled Cable Jacket with Non-Circular Cavity Cross Section; U.S. Pat. No. 6,334,016 for an Optical Fiber Ribbon Matrix Material Having Optimal Handling Characteristics; U.S. Pat. No. 6,321,012 for an Optical Fiber Having Water Swellable Material for Identifying Grouping of Fiber Groups; U.S. Pat. No. 6,321,014 for a Method for Manufacturing Optical Fiber Ribbon; U.S. Pat. No. 6,210,802 for Polypropylene Filler Rods for Optical Fiber Communications Cables; U.S. Pat. No. 6,493,491 for an Optical Drop Cable for Aerial Installation; U.S. Pat. No. 7,346,244 for a Coated Central Strength Member for Fiber Optic Cables with Reduced Shrinkage; U.S. Pat. No. 6,658,184 for a Protective Skin for Optical Fibers; U.S. Pat. No. 6,603,908 for a Buffer Tube that Results in Easy Access to and Low Attenuation of Fibers Disposed Within Buffer Tube; U.S. Pat. No. 7,045,010 for an Applicator for High-Speed Gel Buffering of Flextube Optical Fiber Bundles; U.S. Pat. No. 6,749,446 for an Optical Fiber Cable with Cushion Members Protecting Optical Fiber Ribbon Stack; U.S. Pat. No. 6,922,515 for a Method and Apparatus to Reduce Variation of Excess Fiber Length in Buffer Tubes of Fiber Optic Cables; U.S. Pat. No. 6,618,538 for a Method and Apparatus to Reduce Variation of Excess Fiber Length in Buffer Tubes of Fiber Optic Cables; U.S. Pat. No. 7,322,122 for a Method and Apparatus for Curing a Fiber Having at Least Two Fiber Coating Curing Stages; U.S. Pat. No. 6,912,347 for an Optimized Fiber Optic Cable Suitable for Microduct Blown Installation; U.S. Pat. No. 6,941,049 for a Fiber Optic Cable Having No Rigid Strength Members and a Reduced Coefficient of Thermal Expansion; U.S. Pat. No. 7,162,128 for Use of Buffer Tube Coupling Coil to Prevent Fiber Retraction; U.S. Pat. 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In the specification and/or figures, typical embodiments of the invention have been disclosed. The present invention is not limited to such exemplary embodiments. The use of the term “and/or” includes any and all combinations of one or more of the associated listed items. The figures are schematic representations and so are not necessarily drawn to scale. Unless otherwise noted, specific terms have been used in a generic and descriptive sense and not for purposes of limitation.
| Number | Date | Country | Kind |
|---|---|---|---|
| 09 58639 | Dec 2009 | FR | national |
This application claims the benefit of commonly assigned pending French application Ser. No. 09/58639 for a “Fibre Optique Multimode à Large Bande Passante et à Faibles Pertes par Courbure” (filed Dec. 3, 2009, at the National Institute of Industrial Property (France)), which is hereby incorporated by reference in its entirety. This application further claims the benefit of commonly assigned U.S. Patent Application No. 61/266,754 for a “Fibre Optique Multimode à Large Bande Passante et à Faibles Pertes par Courbure” (filed Dec. 4, 2009), which is hereby incorporated by reference in its entirety.
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| Number | Date | Country | |
|---|---|---|---|
| 20110135263 A1 | Jun 2011 | US |
| Number | Date | Country | |
|---|---|---|---|
| 61266754 | Dec 2009 | US |
