LOW BEND LOSS OPTICAL FIBER

Abstract

According to some embodiments a single mode fiber includes: a germania doped central core region having outer radius r1 and relative refractive index Δ1; anda cladding region comprising (i) a first inner cladding region having an outer radius r2>6 microns and relative refractive index Δ2 and 0.3≦r1/r2≦0.85; and (ii) a second inner cladding region having an outer radius r3>9 microns and comprising a minimum relative refractive index Δ3, wherein said second inner cladding region has at least one region with a relative refractive index delta that becomes more negative with increasing radius; and (iii) an outer cladding region surrounding the inner cladding region and comprising relative refractive index Δ4, wherein Δ1>Δ2>Δ3, Δ3<Δ4.

Description

FIELD

The present invention relates to optical fibers having low bend losses.

TECHNICAL BACKGROUND

There is a need for low bend loss optical fibers, particularly for optical fibers utilized in so-called “access” and fiber to the premises (FTTx) optical networks. Optical fiber can be deployed in such networks in a manner which induces bend losses in optical signals transmitted through the optical fiber. Some fiber applications that can impose physical demands such as tight bend radii, or compression of optical fiber, etc., that induce fiber bend losses. The requirements that impose these demands include, for example, the deployment of optical fiber in optical drop cable assemblies, distribution cables with Factory Installed Termination Systems (FITS) and slack loops, small bend radius multiports located in cabinets that connect feeder and distribution cables, and jumpers in Network Access Points between distribution and drop cables. It has been difficult in some single mode optical fiber designs to achieve both low bend loss at both large and small bends at the same time.

For example, single mode optical fibers with a low index trench in the cladding are being used for making fibers with low bend loss performance. These fibers have a trench where the depth of the trench is relatively constant across the width of the trench. In these designs, while the performance of the fiber at smaller diameters (˜10 mm mandrel diameter) is excellent (<0.25 dB/turn), the performance at large diameters (˜30 mm mandrel diameter) is not as good as in other bend optimized fibers that have been optimized for larger bend diameters. To improve the bend performance at both small and larger bend radii, fiber designs that include multiple trenches have been proposed. However, such an approach results in additional steps during processing and makes making of the fiber more costly.

SUMMARY

According to some embodiments a single mode optical fiber includes:

a central core region having outer radius r₁ and a relative refractive index delta A_1max;

a cladding region comprising (i) a first inner cladding region having an outer radius r₂>6 microns and a relative refractive index delta Δ₂ and 0.3≦r₁/r₂≦0.85; (ii) and a second inner cladding region having an outer radius r₃>9 microns and comprising a minimum relative refractive index delta Δ_3min, wherein said second cladding region has at least one region with a relative refractive index delta that becomes more negative with increasing radius; and (iii) an outer cladding region surrounding the inner cladding region and comprising relative refractive index delta Δ₄, wherein Δ_1max>Δ₂>Δ_3min, Δ_3min<Δ₄,

According to some embodiments, disclosed herein are optical fibers comprising a central core region having outer radius ri and a maximum relative refractive index delta Δ_1max, a cladding comprising a first inner cladding region having an outer radius r₂>8 microns and a relative refractive index delta Δ₂, a second inner cladding region having a relative refractive index delta Δ₃ and a minimum relative refractive index delta Δ_3min, wherein Δ₁>Δ₂>Δ_3min, such that the difference between Δ₂ and Δ_3min is greater than 0.15%, and an outer cladding region surrounding the two inner cladding regions. The fibers embodiments disclosed herein preferably exhibit a 22m cable cutoff less than or equal to 1260 nm, a mode field diameter (MFD) at 1310 nm between 8.2 and 9.6 microns and a zero wavelength dispersion between 1300 and 1324 nm. In at least some fibers embodiments r₁/r₂ is greater than or equal to 0.25, more preferably greater than 0.3. Preferably |Δ₄−Δ₂|≧0.01.

According to some other embodiments a single mode optical fiber includes:

a germania doped central core region having outer radius r₁, peak (maximum) relative refractive index delta in the central core region of Δ_1,max; and the core region having a refractive index alpha profile, α_core, with α_core between 1 and 100 (and for example, 1.8≦α_core≦100; 1.8≦α_core≦2.2; 2≦α_core≦100; 5≦α_core≦100; 2≦α_core≦20, or 5≦α_core≦20);

a cladding region comprising (i) a first inner cladding region having an outer radius r₂>6 microns and relative refractive index Δ₂ and 0.3≦r₁/r₂≦0.85; (ii) and a second inner cladding region having an outer radius r₃>9 microns and comprising a minimum relative refractive index delta Δ_3min, wherein said second cladding region has at least one region with a relative refractive index delta that becomes more negative with increasing radius; and (iii) an outer cladding region surrounding the inner cladding region and comprising relative refractive index Δ₄, wherein Δ₁>Δ₂>Δ₃, Δ₃<Δ₄.

Disclosed herein are optical fiber embodiments comprising a central core region having outer radius r₁ and a maximum relative refractive index delta Δ₁, a cladding region comprising a first inner cladding region having an outer radius r₂>8 microns and a relative refractive index delta Δ₂, and a second inner cladding region surrounding the first inner cladding region and having relative refractive index Δ₃, wherein Δ_{1 max}>Δ₂>Δ_3min, and Δ₂−Δ_3min is ≧0.15. The fibers disclosed herein preferably exhibit a 22m cable cutoff less than or equal to 1260 nm, a mode field diameter (MFD) at 1310 nm between 8.2 and 9.6 microns and a zero wavelength dispersion between 1300 and 1324 nm. In these fibers some embodiments r₁/r₂ is greater than or equal to 0.25, more preferably greater than 0.3. Preferably, |Δ₄−Δ₂|≧0.01.

Applicants discovered having a fiber with a trench that has a non-constant relative refractive index delta helps in achieving good macrobending performance at both small (<10 mm) and large (>20 mm) diameters. The following single mode fiber embodiments have an offset trench with a non-constant relative refractive index delta that decreases with an increasing radius in at least a region thereof, resulting in low macrobend loss and opticals (optical performance parameters) that are ITU-G.652 standards compliant. In at least some embodiments the index in the second inner cladding region decreases with increasing radial position.

In at least some embodiments the shape of the trench is defined by the parameter

$\beta =\frac{\left(R_3-R_2\right)}{{\Delta }_{3,\min }}{\left(\frac{\Delta }{r}\right)}_{\mathrm{average}},\mathrm{where}{\left(\frac{\Delta }{r}\right)}_{\mathrm{average}}$

is the average index slope in the second inner cladding region that is determined by averaging the index slope at different radial locations between R₂ and R₃. In some embodiments, the parameter β is greater than 0.25, more preferably greater than 0.5 and even more preferably greater than 0.75. Preferably β<1.5. For fiber embodiments with a triangular trench the value of parameter β is 1.

In at least some embodiments α_c≦50, where is a trench alpha parameter. For some embodiments 0.5≦α_c≦5.

The moat volume ratio, V_3a3ratio, is defined as follows:

V _3a3ratio =V _3a3/[Δ_3min(r₃²−r₂²)]

Preferably the optical fibers herein have a moat volume ratio of 0.3≦V_3a3ratio≦0.8.

Reference will now be made in detail to the present preferred embodiments, examples of which are illustrated in the accompanying drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

FIGS. 1A-1G show relative refractive index profiles corresponding to several embodiments of an optical fiber as disclosed herein;

FIG. 2 illustrates relative refractive index profiles corresponding to three embodiments of an optical fiber as disclosed herein, and that of a comparative fiber;

FIG. 3 illustrates bend loss as a function of bend diameters for the optical fibers corresponding to the relative refractive index profiles shown in FIG. 2;

FIG. 4 illustrates relative refractive index profiles corresponding to three embodiments of an optical fiber as disclosed herein, and that of another comparative fiber;

FIG. 5 illustrates bend loss as a function of bend diameters for the optical fibers corresponding to the relative refractive index profiles shown in FIG. 4; and

FIG. 6 illustrates relative refractive index profile of a modeled fiber embodiment.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT

Additional features and advantages will be set forth in the detailed description which follows and will be apparent to those skilled in the art from the description or recognized by practicing as described in the following description together with the claims and appended drawings.

The “refractive index profile” is the relationship between refractive index or relative refractive index and optical fiber radius. The radius for each segment of the relative refractive index profile is given by the abbreviations r₁, r₂, r₃, r₄, etc. and lower an upper case are used interchangeability herein (e.g., r₁ is equivalent to R₁).

The “relative refractive index percent” is defined as Δ %=100×(n_i²−n_c²)/2n_i², and as used herein n_o is the average refractive index of the outer cladding region and unless otherwise specified is the refractive index of pure silica. As used herein, the relative refractive index is represented by Δ and its values are given in units of “%”, unless otherwise specified. The terms: relative refractive index delta, delta, Δ, Δ %, % Δ, delta %, % delta and percent delta may be used interchangeability herein. In cases where the refractive index of a region is less than the average refractive index of the outer cladding, the relative index percent is negative and is referred to as having a depressed region or depressed index. In cases where the refractive index of a region is greater than the average refractive index of the outer cladding region, the relative index percent is positive. An “updopant” is herein considered to be a dopant which has a propensity to raise the refractive index relative to pure undoped SiO₂. A “downdopant” is herein considered to be a dopant which has a propensity to lower the refractive index relative to pure undoped SiO₂. Examples of updopants include GeO₂ (germania), Al₂O₃, P₂O₅, TiO₂, Cl, Br. Examples of down dopants include fluorine and boron. For a person skilled in the art, it will be obvious that the relative index profiles disclosed herein can be modified such that entire index profile is shifted linearly up or down relative to the index of pure silica and result in similar optical properties of the resulting optical fibers.

“Chromatic dispersion”, herein referred to as “dispersion” unless otherwise noted, of an optical fiber is the sum of the material dispersion, the waveguide dispersion, and the inter-modal dispersion. In the case of single mode optical fibers the inter-modal dispersion is zero. Zero dispersion wavelength is a wavelength at which the dispersion has a value of zero. Dispersion slope is the rate of change of dispersion with respect to wavelength.

“Effective area” is defined as:

A _eff=2π(∫f²r dr)²/(∫f⁴r dr),

where the integration limits are 0 to ∞, and f is the transverse component of the electric field associated with light propagated in the optical fiber. As used herein, “effective area” or “A_eff” refers to optical effective area at a wavelength of 1550 nm unless otherwise noted.

The term “α-profile” refers to a relative refractive index profile of the region (e.g., core region), expressed in terms of Δ(r) which is in units of “%”, where r is radius. The α-profile of the core (which is defined by the core alpha, or alpha_core herein) follows the equation,

Δ(r)=Δ(r₀)(1−[|r−r₀|/(r₁−r₀)]⁰),

where r₀ is the point at which Δ(r) is maximum, the radius r is moving radially outward from the centerline, r₁ is the radial location at which Δ(r)% first reaches the value 0.03%, and r is in the range r₁≦r≦r_f, where Δ is defined above, r₁ is the initial point of the α-profile, r_f is the final point of the α-profile, and α is an exponent which is a real number.

The mode field diameter (MFD) is measured using the Peterman II method wherein, 2w=MFD, and w²=(2∫f²r dr/∫[df/dr]²r dr), the integral limits being 0 to ∞.

The bend resistance of an optical fiber can be gauged by induced attenuation under prescribed test conditions, for example by deploying or wrapping the fiber around a mandrel of a prescribed diameter, e.g., by wrapping 1 turn around a either a 6 mm, 10 mm, 20 mm, 30 mm or similar diameter mandrel (e.g. “1×10 mm diameter macrobend loss” or the “1×30 mm diameter macrobend loss”) and measuring the increase in attenuation per turn.

One type of bend test is the lateral load microbend test. In this so-called “lateral load” test (LLWM), a prescribed length of optical fiber is placed between two flat plates. A #70 wire mesh is attached to one of the plates. A known length of optical fiber is sandwiched between the plates and a reference attenuation is measured while the plates are pressed together with a force of 30 Newtons. A 70 Newton force is then applied to the plates and the increase in attenuation in dB/m is measured. The increase in attenuation is the lateral load attenuation of the optical fiber in dB/m at a specified wavelength (typically within the range of 1200-1700 nm, e.g., 1310 nm or 1550 nm or 1625 nm).

Another type of bend test is the wire mesh covered drum microbend test (WMCD). In this test, a 400 mm diameter aluminum drum is wrapped with wire mesh. The mesh is wrapped tightly without stretching, and should have no holes, dips, or damage. Wire mesh material specification: McMaster-Carr Supply Company (Cleveland, Ohio), part number 85385T106, corrosion-resistant type 304 stainless steel woven wire cloth, mesh per linear inch: 165×165, wire diameter: 0.0019″, width opening: 0.0041″, open area (%): 44%. A prescribed length (750 meters) of optical fiber is wound at 1 m/s on the wire mesh drum at 0.050 centimeter take-up pitch while applying 80 (+/−1) grams tension. The ends of the prescribed length of fiber are taped to maintain tension and there are no fiber crossovers. The attenuation of the optical fiber is measured at a specified wavelength (typically within the range of 1200-1700 nm, e.g., 1310 nm or 1550 nm or 1625 nm); a reference attenuation is measured on the optical fiber wound on a smooth drum. The increase in attenuation is the wire mesh covered drum attenuation of the optical fiber in dB/km at a specified wavelength (typically within the range of 1200-1700 nm, e.g., 1310 nm or 1550 nm or 1625 nm).

The “pin array” bend test is used to compare relative resistance of optical fiber to bending. To perform this test, attenuation loss is measured for a optical fiber with essentially no induced bending loss. The optical fiber is then woven about the pin array and attenuation again measured. The loss induced by bending is the difference between the two measured attenuations. The pin array is a set of ten cylindrical pins arranged in a single row and held in a fixed vertical position on a flat surface. The pin spacing is 5 mm, center to center. The pin diameter is 0.67 mm During testing, sufficient tension is applied to make the optical fiber conform to a portion of the pin surface. The increase in attenuation is the pin array attenuation in dB of the optical fiber at a specified wavelength (typically within the range of 1200-1700 nm, e.g., 1310 nm or 1550 nm or 1625 nm).

The theoretical fiber cutoff wavelength, or “theoretical fiber cutoff”, or “theoretical cutoff”, for a given mode, is the wavelength above which guided light cannot propagate in that mode. A mathematical definition can be found in Single Mode Fiber Optics, Jeunhomme, pp. 39-44, Marcel Dekker, New York, 1990 wherein the theoretical fiber cutoff is described as the wavelength at which the mode propagation constant becomes equal to the plane wave propagation constant in the outer cladding. This theoretical wavelength is appropriate for an infinitely long, perfectly straight fiber that has no diameter variations.

Fiber cutoff is measured by the standard 2m fiber cutoff test, FOTP-80 (EIA-TIA-455-80), to yield the “fiber cutoff wavelength”, also known as the “2m fiber cutoff” or “measured cutoff”. The FOTP-80 standard test is performed to either strip out the higher order modes using a controlled amount of bending, or to normalize the spectral response of the fiber to that of a multimode fiber.

By cabled cutoff wavelength, or “cabled cutoff” as used herein, we mean the 22 m cabled cutoff test described in the EIA-445 Fiber Optic Test Procedures, which are part of the EIA-TIA Fiber Optics Standards, that is, the Electronics Industry Alliance—Telecommunications Industry Association Fiber Optics Standards.

Unless otherwise noted herein, optical properties (such as dispersion, dispersion slope, etc.) are reported for the LP01 mode.

Applicants discovered that putting an off-set trench with a non-constant depth in the profile of a single mode fiber can simultaneously improve bend performance at both small (≦5 mm) and large (≧10 mm) bend radii. The following fiber embodiments result in low bend performance at small and large bend diameters and have other opticals that are G.652 standards compliant (MFD between 8.2 and 9.6 microns at 1310 nm, a zero dispersion wavelength between 1300 and 1324 nm, cable cutoff wavelength less than or equal to 1260 nm). Optical fibers disclosed herein are capable of exhibiting an effective area at 1310 nm which is between 52 and 72 microns². Optical fibers disclosed herein are capable of exhibiting an effective area at 1550 nm which is between 75 and 90 microns².

Preferably MFD (at a wavelength of 1310 nm) of the optical fiber 10 is between 8.2 μm and 9.6 μm. For example, 8.2 microns≦MFD≦ and 9.6 microns, or 8.5 μm≦MFD≦and 9.4 microns (e.g., 8.6, 8.8, 9, 9.2, 9.4, 9.6 microns, or therebetween).

Several relative refractive index profiles of an exemplary fiber 10 are shown in FIGS. 1A-1G. Optical fibers 10 of FIGS. 1A-1G include a central glass core region 1 (or core) comprising maximum relative refractive index delta percent Δ_1max. The core may have a step index profile or a graded index profile (also referred to as a gradient index profile herein). A first inner cladding region 2 surrounds central core region 1, the first inner cladding region 2 comprising refractive index delta percent Δ₂. A second inner cladding region 3 (also referred to as a trench herein) surrounds the first inner clad region 2, the second inner cladding region 3 comprising refractive minimum index delta percent Δ_{3 min}. The second inner cladding region 3 does not have a constant Δ₃(r). Preferably Δ₃(r) decreases with increasing radius and may have a triangular cross-section. Thus, in some embodiments minimum relative refractive index Δ₃ of this region occurs at r=r₃ (i.e., Δ₃(r=r₃)=Δ_3min). The outer cladding region 4 surrounds second inner cladding region 3 and comprises relative refractive index delta percent Δ₄ As shown in FIGS. 1A-1G, the second inner cladding region 3 is offset from the core region 1, such that the first inner cladding region 2 is sandwiched between the central glass core region 1 and the second inner cladding region 3. Outer cladding region 4 surrounds second inner cladding region 3 (trench) and comprises Δ₄. FIG. 1A illustrates a relative refractive index profile Δ₃(r) of an embodiment of fiber 10 that has a triangular trench profile. This figure shows that the relative refractive index of the second inner cladding region 3 monotonically decreases with increasing radius, and Δ₃(r₂)>Δ₃(r₃). In the embodiment of FIG. 1A Δ₂=Δ₄. However, Δ₂ does not need to be the same as Δ₄ (e.g., Δ₂ may be larger or smaller than Δ₄). Preferably Δ₄≧Δ₂. For example, FIG. 1D illustrates relative refractive index profile of an embodiment of fiber 10 that also has a triangular trench profile and that is similar to the profile of FIG. 1A, but in FIG. 1D Δ₄>Δ₂. In some embodiments, Δ₄−Δ₂ is between 0.01% and 0.1%, in other embodiments between 0.02% and 0.05%. FIG. 1B illustrates a relative refractive index profile of embodiment of fiber 10 that has a trapezoid-shaped trench profile. In this embodiment the refractive index of the second inner cladding region 3 also decreases with increasing radius, and Δ₃(r₂)>Δ₃(r₃). In the embodiment of FIG. 1B Δ₂=Δ₄, but in some embodiments Δ₂ and Δ₄ have different values (e.g., Δ₂>Δ₄, or Δ₂<Δ₄). FIG. 1C illustrates a relative refractive index profile of another embodiment of fiber 10. In this embodiment the refractive index of the second inner cladding region 3 monotonically decreases with increasing radius until it reaches a value r=r_3A, and then is constant between the radii r_3A and r₃. In this embodiment Δ₃(r₂)>Δ₃(r₃). In the embodiment of FIG. 1C Δ₂=Δ₄ but in some embodiments Δ₂ and Δ₄ have different values (e.g., Δ₂>Δ₄, or Δ₂<Δ₄). In some embodiments 0.05%>|Δ_2−Δ4|≧0.01%. FIG. 1E illustrates relative refractive index profile of an embodiment of fiber 10 that also has a triangular trench profile and that is similar to the profile of FIG. 1A, but in FIG. 1E the central core region has a maximum refractive index delay percent Δ_1max and a refractive index alpha profile α_core. Optical fibers 10 may have cores with the alpha values ranging as 1≦α_core≦100. In some preferred embodiments 5≦α_core≦100, in other preferred embodiments 2≦α_core≦20, or 5≦α_core≦20.

In at least some embodiments α_c≦50, where α_c, is a trench alpha parameter. For some embodiments, 0.5≦α_t≦5. FIG. 1F illustrates relative refractive index profile of an embodiment of fiber 10 that also has a trench profile that is similar to the profile of FIG. 1A, but in FIG. 1F the relative refractive index profile of the second inner cladding region 3 has a shape that is convex. FIG. 1G illustrates relative refractive index profile of an embodiment of fiber 10 that also has a trench profile and that is similar to the profile of FIG. 1A, but in FIG. 1G the relative refractive index profile of the second inner cladding regon 3 has a shape that is concave.

In the exemplary embodiments, Δ_1max>Δ₂>Δ_3min and Δ_3min<Δ₄. Preferably Δ₂−Δ_3min≧0.1%; more preferably Δ₂−Δ_3min≧0.15%, even more preferably Δ₂−Δ₃≧0.2%. In the embodiments illustrated in FIGS. 1A through 1G, regions 1, 2, 3 are immediately adjacent one another. However, this is not required, and alternatively additional optional core or cladding regions may be employed. For example (not shown), another region (2A) may be situated between the core and the region 3. The optional inner cladding region 2A may be may be directly adjacent to and surround core region 1 and comprise a higher or a lower relative refractive index delta percent Δ_2A than that of the annular region 2 (i.e., Δ_2A<Δ₂, or Δ_2A>Δ₂).

The index of refraction (and thus the relative refractive index delta) of the second inner cladding region 3 (the trench) preferably decreases with increasing radial position. The shape of the second inner cladding region 3 is defined by the parameter

$\beta =\frac{\left(R_3-R_2\right)}{{\Delta }_{3,\min }}{\left(\frac{\Delta }{r}\right)}_{\mathrm{average}},\mathrm{where}{\left(\frac{\Delta }{r}\right)}_{\mathrm{average}}$

is the average index slope in the second inner cladding region that is determined by averaging the index slope at different radial locations between R₂ and R₃. For a triangular trench the value of parameter β is 1. For a rectangular trench, the value of parameter β is 0. In other embodiments of optical fiber 10, the parameter β is greater than 0.25, more preferably greater than 0.5 and even more preferably greater than 0.75. Preferably, β is less than 1.5, and more preferably less than 1.1.

Another parameter that can be used to define the trench shape in the second inner cladding region 3 is the parameter, α_t, which refers to a relative refractive index profile in the second inner cladding region 3, expressed in terms of Δ(r) which is in units of “%”, where r is radius, which follows the equation,

Δ(r)=Δ_3,min(1−[|r₃−r|/(r₃−r₂)]^αt),

where α_t is the trench alpha parameter. For a rectangular trench, the value of parameter α_t is greater than 100, while for a triangular trench the value of parameter α_t is 1. Preferably α_t≦50. In some embodiments of optical fiber 10, the parameter α_t is 0.5≦α_t≦5, in some embodiments 0.5≦α_t≦3, and in some embodiments 0.75≦α_t≦2.

Preferably, according to the exemplary embodiments disclosed herein the optical fibers have the moat volume ratio of 0.3≦V_3α3ratio≦0.8, where V_3α3ratio, is:

V _3a3ratio =V _3a3/[Δ_{3 min}(r₃²−r₂²)]

Central core region 1 comprises an outer radius r₁, r₁ is the point when the radius r moving radially outward from the centerline corresponds to at the value at which Δ(r) % first reaches 0.03%. Core region 1 (also referred to as a core herein) preferably exhibits a maximum relative refractive index delta percent, Δ_{1 max}, between about 0.3 to 0.5, more preferably between about 0.31 to 0.48, for example between about 0.31 to 0.45. In some embodiments, Δ_1max is between 0.31 and 0.43. In some embodiments Δ_1max is less than 0.42. Core radius r₁ is preferably between 3 and 10 microns, more preferably between about 3.5 to 8.0 microns, for example 3.5≦r₁≦7.0 microns, or 3.5≦r₁≦5.0 microns. Central core region 1 may comprise a single segment, step index profile. In some embodiments, central core region 1 exhibits an alpha profile with an alpha (α_core) value greater than 0.5 and less than 10, and in some embodiments less than 7.5, less than 5, or less than 3 (for example, between 1.8 and 2.2, such as 1.85, 1.95, 1,98, 2, 2.05, 2.1 or therebetween). However, in other embodiments, central core region 1 may comprise an alpha, α_core between about 2 and about 100; or between 10 and 40, such as 15, 20, 30, or therebetween), and in some cases 5≦alpha_core≦20.

In some preferred embodiments, central core region 1 exhibits an 5≦alpha_core≦20, and a core region 1 having a relative refractive index delta percent, Δ₁ between 0.30 to 0.48 (e.g., 0.32≦Δ₁≦0.4). In some preferred embodiments, central core region 1 exhibits an alpha 5≦alpha_core≦20, and a core region 1 having a refractive index delta percent, Δ_1max between 0.3 to 0.48 (e.g., 0.32≦Δ₁≦0.4), and a core radius between about 3.5 to 7 microns. In some preferred embodiments, central core region 1 exhibits an alpha greater than 0.5 and less than 10, and in some embodiments less than 7.5, less than 5, or less than 3, and a core region 1 has a relative refractive index delta percent, Δ₁ between 0.30 to 0.48 (e.g., 0.32≦Δ₁≦0.4). In some embodiments, central core region 1 exhibits an alpha greater than 0.5 and less than 10, and in some embodiments less than 7.5, less than 5, or less than 3, and a core region 1 having a refractive index delta percent, Δ_1max between 0.3 to 0.48 (e.g., 0.32≦Δ₁≦0.4), and a core radius between about 3.5 to 7 microns.

In the embodiment illustrated in FIG. 1, inner cladding region 2 surrounds central core region 1 and comprises inner radius r₁ and outer radius r₂, r₁ being defined as above and r₂ which is defined as the first radial location moving away radially outward from r₁ where the relative refractive index is equal to 0.03(Δ_3min). In some cases the refractive index in region 2 is essentially flat, in other cases there can be a gradient index profile, and in some embodiments region 2 decreases in refractive index as radius increases. Still in other cases there can be fluctuations as a result of small profile design or process variations (see, for example, FIG. 6). In some embodiments, the first inner cladding region 2 contains less than 0.02 wt % fluorine. In some embodiments, the inner cladding region 2 comprises silica which is substantially undoped with either fluorine or germania, i.e., such that the region is essentially free of fluorine and germania. In some other embodiments, region 2 is doped with fluorine that is less than 0.2 wt %. The inner cladding region 2 preferably exhibits a width between about 1 to 13 microns, more preferably 2 to 10 microns, even more preferably between about 2 to 7 microns. Preferably, 6 microns≦r₂≦15 microns, more preferably 6.5 microns≦r₂≦12 microns. The ratio of the core radius r₁ over the inner cladding region 2 radius r₂ is preferably at least 0.3 and less than 1, more preferably greater than 0.3, for example, between about 0.33 and 0.85, or between 0.33 and 0.7, or between 0.4 to 0.6.

Inner cladding region 2 comprises refractive index delta percent Δ₂ which is calculated using:

$\begin{array}{cc}{\Delta }_2={\int }_{r1}^{r2}\Delta \left(r\right)r/\left(r_2-r_1\right)& \mathrm{Eq}.1\end{array}$

In some embodiments, the first inner cladding region 2 comprises silica which is substantially undoped with either fluorine or germania, i.e., such that the region is essentially free of fluorine and germania. Inner cladding region 3 preferably includes a down-dopant, for example fluorine to provide a minimum relative refractive index delta that is lower than that of region 2. In the embodiments illustrated in FIGS. 1A-1G, the second inner cladding region 3 (also referred to as trench) surrounds the first inner cladding region 2 and comprises inner radius r₂ and outer radius r₃, r₂ being defined as above and r₃ being defined as where the relative refractive index profile curve again crosses the zero delta line (Δ_t) at the first radial location moving away radially outward from the radius r₂. In some cases the relative refractive index in region 3 can be a gradient index profile, in some cases (preferably) the relative refractive index in region 3 has a shallower depression in the inner part of the region and a deeper depression in the outer part of the region. In addition, there can be fluctuations as a result of small profile design or process variations. In some embodiments the second inner cladding region 3 includes fluorine and/or boron. In some embodiments, the depressed-index annular portion comprises voids, either non-periodically disposed, or periodically disposed, or both. By “non-periodically disposed” or non-periodic distribution”, we mean that when one takes a cross section (such as a cross section perpendicular to the longitudinal axis) of the optical fiber, the non-periodically disposed voids are randomly or non-periodically distributed across a portion of the fiber. Similar cross sections taken at different points along the length of the fiber will reveal different cross-sectional hole patterns, i.e., various cross sections will have different hole patterns, wherein the distributions of voids and sizes of voids do not match. That is, the voids or voids are non-periodic, i.e., they are not periodically disposed within the fiber structure. These voids are stretched (elongated) along the length (i.e. parallel to the longitudinal axis) of the optical fiber, but do not extend the entire length of the entire fiber for typical lengths of transmission fiber. The voids can contain one or more gases, such as argon, nitrogen, krypton, CO₂, SO₂, or oxygen, or the voids can contain a vacuum with substantially no gas; regardless of the presence or absence of any gas, the relative refractive index in the annular portion 3l is lowered due to the presence of the voids. While not wishing to be bound by theory, it is believed that the voids extend less than a few meters, and in many cases less than 1 meter along the length of the fiber. Optical fibers disclosed herein can be made by methods which utilize preform consolidation conditions which are effective to result in a significant amount of gases being trapped in the consolidated glass blank, thereby causing the formation of voids in the consolidated glass optical fiber preform. Rather than taking steps to remove these voids, the resultant preform is used to form an optical fiber with voids, or voids, therein. As used herein, the diameter of a hole is the longest line segment whose endpoints are disposed on the silica internal surface defining the hole when the optical fiber is viewed in perpendicular cross-section transverse to the longitudinal axis of the fiber. Inner cladding region 3 comprises relative refractive index delta percent Δ₃ (r), and the minimum relative refractive index delta Δ_3min . The minimum index in the second inner cladding region Δ_3min is preferably less than −0.1% (i.e., Δ₄−4₃≧0.1%), in some embodiments less than −0.25%, and in some other embodiments less than −0.35%.

The volume V₃ of the second inner cladding region 3 (the trench), is defined as shown in Eq. 2, and given in units of percent delta micron square (% Δmicrons²)

$\begin{array}{cc}{V}_3=2{\int }_{r2}^{r3}{\Delta }_{\left(2-3\right)}\left(r\right)rr& \mathrm{Eq}.2\end{array}$

In the embodiments of FIGS. 1A-1D the absolute volume V₃ of the inner cladding region 3 is 10 Δ % micron²≦V₃≦105 Δ % microns², in some embodiments 20 Δ % microns²≦V₃≦95 Δ % microns². The inner cladding region 3 preferably exhibits a width W₃, (i.e., r₃−r₂), of about 5≦(r₃−r₂)≦20 microns, in some embodiments 5≦(r₃−r₂)≦15 microns. In some embodiments of FIGS. 1A-1D the absolute volume V₃ of the inner cladding region 3 is 35 Δ % microns²≦V₃≦105 Δ % microns², for example, 50 Δ % microns²≦V₃≦95 Δ % microns², (e.g., greater than 70 Δμm², and in some embodiments greater than 85 Δμm³²) The inner cladding region 3 preferably exhibits a width W between about 5 to 20 microns, more preferably 5 to 15 microns. The ratio of the core radius r₃ over the inner cladding region 2 radius r₂ is preferably greater than 1.3, more preferably between 1.5 and about 4.

Outer cladding region 4 surrounds the depressed annular region 3 and comprises relative refractive index delta percent Δ₄ which is higher than the index Δ_3min of inner cladding region 3. In some embodiments outer cladding region 4 has relative refractive index greater than that of first inner cladding region 2, thereby forming a region which is an “updoped” outer cladding region 4 with respect to first inner cladding region 2, e.g. by adding an amount of dopant (such as germania or chlorine) sufficient to increase the relative refractive index of the outer cladding region 4. Note, however, that it is not critical that region 4 be updoped in the sense that an index increasing dopant must be included in region 4. Indeed, the same sort of raised index effect in outer cladding region 4 may be achieved by downdoping first inner cladding region 2 with respect to outer cladding region 4. Outer cladding region 4 comprises a higher relative refractive index than first inner cladding region 2, and may comprises relative refractive index delta percent Δ₄ which is greater than 0.01%, and in some embodiments be greater than 0.02% or 0.03% , relative to relative refractive index in the first inner cladding region 2. Preferably, the higher index portion (compared to first inner cladding region 2) of outer cladding region 4 extends at least to the point where the optical power which would be transmitted through the optical fiber is greater than or equal to 90% of the optical power transmitted, more preferably to the point where the optical power which would be transmitted through the optical fiber is greater than or equal to 95% of the optical power transmitted, and most preferably to the point where the optical power which would be transmitted through the optical fiber is greater than or equal to 98% of the optical power transmitted. In many embodiments, this is achieved by having the “updoped” third annular region extend at least to a radial point of about 30 microns. Consequently, the volume V₄ of the third annular region 4, is defined herein being calculated between radius r₃ and r₃₀ (the radius at 30 microns) and thus is defined as

$\begin{array}{cc}{V}_4=2{\int }_{r3}^{r30}{\Delta }_{\left(4-2\right)}\left(r\right)rr& \mathrm{Eq}.4\end{array}$

The volume V₄ of the outer cladding region 4 (inside 30 microns) compared to that of the first inner cladding region 2, is preferably greater than 5 Δ % microns², more preferably greater than 7 Δ % microns², and maybe greater than 10% Δ microns². This volume V₄ of the outer cladding region (inside 30 microns) is in some embodiments less than 50% Δ microns².

In some embodiments, the relative refractive index Δ₄ of the outer cladding region 4 is greater than first inner cladding index Δ₂ by 0.01%, more preferably greater than 0.02%. In some embodiments, the outer cladding region 4 comprises chlorine (Cl). In some embodiments the outer cladding region includes germania (GeO₂).

The core region 1 preferably has a positive relative refractive index throughout. The core 1 comprises a maximum relative refractive index Δ_1MAX occurring between r=0 and r=3 μm. Δ_1MAX is preferably between 0.30% and 0.48%, and even more preferably 0.3% to 0.45%.

The first inner cladding region 2 preferably has a substantially constant relative refractive index profile, i.e. the difference between the relative refractive index at any two radii within the intermediate region is less than 0.02%, and in some preferred embodiments less than 0.01%. Thus, the relative refractive index profile of the first inner cladding region 2 preferably has a substantially flat shape. In some embodiments the outer cladding region 4 is updoped relative to pure silica and in some embodiments the first inner cladding region 2 is downdoped relative to pure silica.

The core region 1 may be a step index core, and may comprise an alpha (α) shape. In preferred embodiments, r₁ is less than 8.0 microns, and more preferably is between 3.5 microns and 7.0 microns. The fibers are capable of exhibiting mode field diameter at 1310 nm between 8.2 and 9.6 microns, zero dispersion wavelength between 1300 and 1324 nm, cable cutoff less than or equal to 1260 nm and a bend loss of less than 2, and preferably less than 1 dB/turn when wound upon on a 10 mm radius mandrel.

The fibers disclosed herein may be drawn from optical fiber preforms made using conventional manufacturing techniques and using known fiber draw methods and apparatus, for example as is disclosed in U.S. Pat. No. 7,565,820, the specification of which is hereby incorporated by reference.

Various exemplary embodiments will be further clarified by the following examples. It will be apparent to those skilled in the art that various modifications and variations can be made without departing from the spirit or scope of the claims.

FIBER EXAMPLES 1-6

Tables 1A, 1B, 2A, 2B, 3-5 below list characteristics of modeled illustrative examples 1-6 and 8-27, manufactured fiber example 7, and those of the two comparative example fibers. In particular, set forth below for each example of Table 1A and 1B is the relative refractive index delta Δ₁, alpha, and outer radius r₁ of the central core region 1, relative refractive index delta Δ₂ and outer radius r₂ first inner cladding region 2, relative refractive index delta Δ₃ and volume V₃ of the second inner cladding region 3, relative refractive index delta Δ₄ and volume V₄ of the outer cladding region 4, which is calculated between inner radius r₃ of outer cladding region 3 and a radial distance of 30 microns, and a moat volume ratio.

TABLE 1A
	Comparative	Exemplary	Exemplary	Exemplary
	Example	embodiment	embodiment	embodiment
Parameter	1	1	2	3
Δ1max (%)	0.35	0.35	0.35	0.39
α	20	20	20	2
r1 (microns)	4.0	4.0	4.0	5.4
Δ2 (%)	0.00	0.00	0.00	0.00
r2 (microns)	9.5	7.6	7.6	6.6
Δ3 (%)	−0.28	−0.40	−0.40	−0.40
r3 (microns)	16.8	16.8	17.9	18.2
V3 (% Δ	53.75	50.54	59.6	66.3
microns)
Shape of	Rectangular	Triangular	Triangular	Triangular
Trench
Δ4 (%)	0.00	0.00	0.00	0.00
r4 (microns)	62.5	62.5	62.5	62.5
r1/r2	0.421	0.526	0.565	0.818
r3/r2	1.77	2.21	2.36	2.76
Parameter β	0	1	1	1
Parameter ατ	100	1	1	1
V4 (% Δ	0	0	0	0
microns)

TABLE 1B
	Comparative	Exemplary	Exemplary	Exemplary
	Example	embodiment	embodiment	embodiment
Parameter	2	4	5	6
Δ1max (%)	0.34	0.34	0.34	0.44
α	20	20	20	2
r1 (microns)	4.0	4.0	4.0	5.4
Δ2 (%)	0.00	0.00	0.00	0.00
r2 (microns)	9.5	6.6	6.6	7.5
Δ3 (%)	−0.40	−0.40	−0.40	−0.44
r3 (microns)	16.8	20.8	22.1	19.0
V3 (% Δ	76.79	91.26	105	105.6
microns)
Shape of	Rectangular	Triangular	Triangular	Convex
Trench
Δ4 (%)	0.00	0.00	0.00	0.00
r4 (microns)	62.5	62.5	62.5	62.5
r1/r2	0.42	0.606	0.606	0.72
r3/r2	1.76	3.15	3.35	2.53
Parameter β	0	1	1	1
Parameter ατ	>100	1	1	0.5
V4 (% Δ	18.53	14.02	13.64	21.56
microns)

Also set forth (Tables 2A, 2B) are modeled data including: theoretical cutoff wavelength in nm, chromatic dispersion and dispersion slope at 1310 nm, chromatic dispersion and dispersion slope at 1550 nm, mode field diameter at 1310 nm and 1550 nm, effective area Aeff at 1550 nm, lateral load wire mesh microbend at 1550 nm, pin array macrobend at 1550 nm, zero dispersion wavelength, 22 m cable cutoff, 1×10 and 1×30 mm diameter induced bend losses in dB per turn at 1550 nm, and kappa value (dispersion D divided by the dispersion slope).

More specifically, the exemplary fiber embodiments Tables 1A, 1B, 2A and 2B have core alpha values between 2 and 20, core radii between about 4 and about 5.5 microns, and 0.3%<Δ_1MAX<0.4%. Most of these fiber embodiments have a bend loss of less than 0.5 dB/turn (at 1550 nm) when bent around 10 mm diameter mandrel, and less than 0.01 dB/turn when bent around 30 mm mandrel.

TABLE 2A
	Comparative	Exemplary	Exemplary	Exemplary
Parameter	Example 1	Embodiment 1	Embodiment 2	Embodiment 3
Cutoff (nm)	1150	1150	1151	1150
MFD at 1310 nm (microns)	8.7	8.7	8.7	9.0
Aeff at 1310 nm (microns2)	59.1	59.0	59.1	61.4
Dispersion at 1310 nm (ps/nm/km)	−0.49	−0.56	−0.62	−0.45
Slope at 1310 nm (ps/nm2/km)	0.0888	0.0880	0.0878	0.0918
kappa at 1310 nm (nm)	−5.6	−6.3	−7.0	−4.9
MFD at 1550 nm (microns)	9.9	9.9	9.9	10.2
Aeff at 1550 nm (microns2)	74.2	74.2	74.5	78.0
Dispersion at 1550 nm (ps/nm/km)	17.2	16.9	16.8	17.7
Slope at 1550 nm (ps/nm2/km)	0.0635	0.0632	0.0621	0.0641
kappa at 1550 nm (nm)	271.3	271.3	270.3	275.8
Lateral load at 1550 nm (dB)	0.3	0.4	0.3	0.4
Pin array at 1550 nm (dB)	10.5	11.0	10.1	11.2
Zero Dispersion Wavelength (nm)	1315	1316	1316	1315
Cable Cutoff (nm)	<1260	<1260	<1260	<1260
Bend loss per turn on a 10 mm	0.47	0.67	0.50	0.49
mandrel diameter (dB/turn)
Bend loss per turn on a 30 mm	0.0033	0.0038	0.0022	0.0037
mandrel diameter (dB/turn)

TABLE 2B
	Comparative	Exemplary	Exemplary	Exemplary
Parameter	Example 2	embodiment 4	embodiment 5	embodiment 6
Cutoff (nm)	1037	1035	1036	1023
MFD at 1310 nm (microns)	8.8	8.8	8.8	8.9
Aeff at 1310 nm (microns2)	60.0	59.8	59.9	60.0
Dispersion at 1310 nm (ps/nm/km)	−0.30	−0.51	−0.58	−0.05
Slope at 1310 nm (ps/nm2/km)	0.0900	0.0880	0.0878	0.0930
kappa at 1310 nm (nm)	−3.4	−5.8	−6.6	−0.53
MFD at 1550 nm (microns)	9.9	10.0	10.0	10.0
Aeff at 1550 nm (microns2)	75.0	75.4	75.6	75.2
Dispersion at 1550 nm (ps/nm/km)	17.7	16.9	16.8	18.3
Slope at 1550 nm (ps/nm2/km)	0.0649	0.0620	0.0618	0.0650
kappa at 1550 nm (nm)	273.4	272.8	271.8	282.1
Lateral load at 1550 nm (dB)	0.7	0.6	0.5	0.5
Pin array at 1550 nm (dB)	29.4	26.2	23.2	23.3
Zero Dispersion Wavelength (nm)	1313	1315	1316	1310.5
Cable Cutoff (nm)	<1260	<1260	<1260	<1260
Bend loss per turn on a 10 mm	0.1	0.19	0.12	0.04
mandrel diameter (dB/turn)
Bend loss per turn on a 30 mm	0.01	0.0015	0.0004	0.0026
mandrel diameter (dB/turn)

TABLE 3
Parameter                        Example 7
R1 (microns)                     5.0
Δ1max (%)                        0.46
core alpha                       15
R2 (microns)                     9.6
Δ2 (%)                           0.00
R1/R2                            0.52
R3a (microns)                    19.4
Δ3min (%)                        −0.52
moat alpha (alphaτ)              1
R3 (microns)                     19.4
Δ3a (%)                          −0.52
(R3a − R2)/(R3 − R2)             1.00
Moat Volume, V3a3 (% Δ microns2) 82.2
Moat Volume Ratio                0.56
R4 (microns)                     62.5
Δ4 (%)                           0.00
V4 (% Δ microns2)                0
MFD at 1310 nm (microns)         9.01
MFD at 1550 nm (microns)         10.16
Dispersion at 1310 nm (ps/nm/km) −0.94
Slope at 1310 nm (ps/nm2/km)     0.086
Dispersion at 1550 nm (ps/nm/km) 15.8
Slope at 1550 nm (ps/nm2/km)     0.059
Cable Cutoff (nm)                1254
MACCab (MFD in microns at        7.19
1310 nm/CabCutoff in microns)
10 mm diameter Bend              1.23
(dB/turn) at 1550 nm
15 mm diameter Bend              0.190
(dB/turn) at 1550 nm
20 mm diameter Bend              0.023
(dB/turn) at 1550 nm
Lambda0 (nm)                     1320

TABLE 4
Parameter	Ex-8	Ex-9	Ex-10	Ex-11	Ex-12	Ex-13	Ex-14	Ex-15
R1 (microns)	4.88	4.64	4.56	4.40	4.88	4.56	4.40	4.56
Δ1max (%)	0.36	0.36	0.36	0.36	0.36	0.36	0.36	0.36
core alpha	5	5	10	10	5	10	15	10
R2 (microns)	10.3	9.79	9.62	9.28	11.03	10.31	9.94	10.31
Δ2 (%)	0.00	0.00	0.00	0.00	0.00	0.00	0.00	0.00
R1/R2	0.47	0.47	0.47	0.47	0.44	0.44	0.44	0.44
R3a (microns)	14.64	13.92	13.68	13.20	17.08	18.24	17.60	17.10
Δ3min (%)	−0.45	−0.45	−0.45	−0.43	−0.20	−0.10	−0.15	−0.20
moat alpha (alphat)	1	1	1	1	1	1	1	2
R3 (microns)	14.64	16.29	13.68	15.44	17.08	18.24	17.6	17.1
Δ3a (%)	−0.45	−0.45	−0.45	−0.43	−0.20	−0.10	−0.15	−0.20
(R3a − R2)/(R3 − R2)	1.00	0.64	1.00	0.64	1.00	1.00	1.00	1.00
Moat Volume, V3a3	26	59.2	23.0	49.7	18.5	12.5	17.5	26.4
(%Δ microns2)
Moat Volume Ratio	0.54	0.78	0.54	0.73	0.54	0.55	0.55	0.71
R4 (microns)	62.5	62.5	62.5	62.5	62.5	62.5	62.5	62.5
Δ4 (%)	0.00	0.00	0.00	0.02	0.00	0.00	0.00	0.00
V4 (%Δ microns2)	0.0	0.0	0.0	13.2	0.0	0.0	0.0	0.0
MFD at 1310 nm	9.01	8.86	8.90	8.81	9.02	8.94	8.88	8.92
(microns)
MFD at 1550 nm	10.12	10.07	10.01	9.93	10.25	10.12	10.04	10.07
(microns)
LP11 Cutoff (nm)	1256	1194	1275	1167	1268	1297	1287	1286
Dispersion at 1310 nm	0.04	−0.53	0.50	0.19	−0.17	0.17	0.16	0.26
(ps/nm/km)
Slope at 1310 nm	0.079	0.073	0.078	0.088	0.082	0.083	0.081	0.077
(ps/nm2/km)
Dispersion at 1550 nm	17.5	17.1	17.9	17.6	16.9	17.0	17.0	17.3
(ps/nm/km)
Slope at 1550 nm	0.062	0.063	0.061	0.062	0.061	0.059	0.089	0.060
(ps/nm2/km)
Cable Cutoff (nm)	1218	1236	1232	1225	1196	1203	1192	1241
MACCab (MFD in	7.40	7.17	7.22	7.19	7.54	7.43	7.45	7.19
microns at 1310 nm/
Cable Cutoff in
microns)
10 mm diameter	1.25	0.24	1.17	0.36	2.22	2.54	2.25	0.91
bend loss (dB/turn)
20 mm diameter	0.263	0.060	0.228	0.088	0.460	0.486	0.460	0.179
bend loss (dB/turn)
30 mm diameter	0.005	0.003	0.003	0.004	0.006	0.005	0.006	0.003
bend loss (dB/turn)
Lambda0 (nm)	1309	1317	1304	1308	1312	1308	1318	1307
LLWM (dB/m at	0.182	0.169	0.147	0.145	0.195	0.158	0.224	0.158
1550 nm)
Pin Array (dB at	6.40	7.59	4.52	10.19	7.09	4.89	9.16	4.40
1550 nm)

TABLE 5
Parameter	Ex-16	Ex-17	Ex-18	Ex-19	Ex-20
R1 (microns)	4.56	4.56	4.33	4.46	4.25
Δ1max (%)	0.36	0.36	0.393	0.364	0.373
core alpha	10	10	12	12	12
R2 (microns)	10.31	13.04	6.80	7.00	7.86
Δ2 (%)	0.00	0.00	0.00	0.00	0.00
R1/R2	0.44	0.35	0.63	0.64	0.54
R3a (microns)	17.10	18.24	16.8	17.3	19.4
Δ3min (%)	−0.25	−0.20	−0.44	−0.44	−0.48
moat alpha (alphaτ)	0.5	1	1	1	1
R3 (microns)	17.1	18.24	16.8	17.3	19.4
Δ3a (%)	−0.25	−0.20	−0.44	−0.44	−0.48
(R3a − R2)/(R3 − R2)	1.00	1.00	1.00	1.00	1.00
Moat Volume, V3a3	17.0	26.6	57	60	83
(% Δ microns2)
Moat Volume Ratio	0.37	0.82	0.55	0.55	0.55
R4 (microns)	62.5	62.5	62.5	62.5	62.5
Δ4 (%)	0.00	0.00	0.00	0.00	0.00
V4 (% Δ microns2)	0.0	0.0	0.0	0.0	0
MFD at 1310 nm	8.93	8.93	8.57	8.88	8.59
(microns)
MFD at 1550 nm	10.10	10.12	9.73	10.09	9.9
(microns)
LP11 Cutoff (nm)	1293	1301	1163	1151	1156
Dispersion at 1310	0.18	0.13	−0.76	−0.49	not
nm (ps/nm/km)					calculated
Slope at 1310 nm	0.081	0.081	0.088	0.089	not
(ps/nm2/km)					calculated
Dispersion at 1550	17.1	16.9	16.8	17.2	not
nm (ps/nm/km)					calculated
Slope at 1550 nm	0.059	0.058	0.062	0.063	not
(ps/nm2/km)					calculated
Cable Cutoff (nm)	1215	1242	1207	1205	1210
MACCab (MFD in	7.35	7.19	7.10	7.37	7.10
microns at 1310
nm/Cable Cutoff in
microns)
10 mm diameter	1.82	0.89	0.26	0.35	0.07
Bend (dB/turn)
20 mm diameter	0.352	0.18	0.060	0.10	0.02
Bend (dB/turn)
30 mm diameter	0.004	0.003	0.002	0.003	0.002
Bend (dB/turn)
Lambda0 (nm)	1308	1308	1319	1316	1310
LLWM (dB/m at	0.162	0.166	0.134	0.178	not
1550 nm)					calculated
Pin Array (dB at	4.93	5.00	7.30	11.95	not
1550 nm)					calculated

TABLE 6
Parameter	Ex-21	Ex-22	Ex-23	Ex-24	Ex-25	Ex-26	Ex-27	Ex-28
R1 (microns)	4.51	4.55	4.57	4.58	4.41	4.36	4.33	4.38
Δ1max (%)	0.365	0.355	0.345	0.355	0.355	0.355	0.355	0.363
core alpha	12	12	12	12	12	12	12	12
R2 (microns)	5.95	6.02	6.09	5.78	7.67	6.14	5.6	6.09
Δ2 (%)	0.00	0.00	0.00	0.00	0.00	0.00	0.00	0.00
R1/R2	0.76	0.76	0.75	0.79	0.57	0.71	0.77	0.72
R3a (microns)	17	17.2	17.4	16.7	17.7	17.5	17.4	16.5
Δ3min (%)	−0.435	−0.435	−0.435	−0.433	−0.481	−0.466	−0.466	−0.55
moat alpha (alphat)	1	1	1	1	1	1	1	1
R3 (microns)	17	17.2	17.4	16.7	17.7	17.5	17.4	16.5
Δ3a (%)	−0.435	−0.435	−0.435	−0.433	−0.481	−0.466	−0.466	−0.55
(R3a − R2)/(R3 − R2)	1	1	1	1	1	1	1	1
Moat Volume, V3a3	64	66	67	62	69	73	76	76
(%Δ microns2)
Moat Volume Ratio	0.58	0.58	0.58	0.58	0.56	0.58	0.60	0.59
R4 (microns)	62.5	62.5	62.5	62.5	62.5	62.5	62.5	62.5
Δ4 (%)	0.00	0.00	0.00	0.00	0.00	0.00	0.00	0.00
V4 (%Δ microns2)	0	0	0	0	0	0	0	0
MFD at 1310 nm	8.72	8.83	8.95	8.81	9.08	8.95	8.82	8.6
(microns)
MFD at 1550 nm	9.83	9.96	10.08	9.9	10.29	10.1	9.88	9.67
(microns)
LP11 Cutoff (nm)	1113	1110	1107	1155	1120	1096	1077	1077
Dispersion at 1310 nm	−0.712	−0.623	−0.534	−0.356	−0.801	−0.445	−0.089	−0.72
(ps/nm/km)
Slope at 1310 nm	0.089	0.089	0.089	0.089	0.089	0.089	0.089	0.09
(ps/nm2/km)
Dispersion at 1550 nm	17.73	17.87	18	18.1	17.65	18	18.3	17.9
(ps/nm/km)
Slope at 1550 nm	0.063	0.063	0.063	0.063	0.063	0.063	0.063	0.063
(ps/nm2/km)
Cable Cutoff (nm)	1213	1214	1216	1214	1219	1217	1218	1213
MACCab (MFD in	7.19	7.27	7.36	7.26	7.45	7.35	7.24	7.09
microns at 1310 nm/
Cable Cutoff in
microns)
10 mm diameter	0.206	0.223	0.245	0.271	0.234	0.196	0.167	0.1
Bend (dB/turn)
20 mm diameter	0.057	0.065	0.074	0.077	0.072	0.062	0.054	0.03
Bend (dB/turn)
30 mm diameter	0.002	0.0027	0.003	0.0029	0.003	0.003	0.003	0.002
Bend (dB/turn)
Lambda0 (nm)	1318	1317	1316	1314	1319	1315	1311	1318
LLWM (dB/m at	0.138	0.152	0.17	0.143	0.209	0.17	0.138	0.121
1550 nm)
Pin Array (dB at	14.07	16.12	18.49	15.84	19.17	20.8	22.7	16.48
1550 nm)

Also set forth (Tables 4, 5 and 6) are modeled data including: theoretical cutoff (LP11) wavelength in nm, chromatic dispersion and dispersion slope at 1310 nm, chromatic dispersion and dispersion slope at 1550 nm, mode field diameter at 1310 nm and 1550 nm, effective area Aeff at 1550 nm, lateral load wire mesh microbend at 1550 nm, pin array macrobend at 1550 nm, zero dispersion wavelength, 22 m cable cutoff, MACCab, and 1×10, 1×20 and 1×30 mm diameter induced bend losses in dB per turn at 1550 nm. The optical fiber embodiments of Tables 4, 5 and 6 (fiber examples 8-27) have core alpha values between 5 and 15, core radii between about 4 and about 5 microns, and 0.3%<Δ1MAX<0.4%. Most of these fiber embodiments have a bend loss of less than 2 dB/turn (at 1550 nm) when bent around the 10 mm diameter mandrel, less than 0.5 dB/turn (at 1550 nm) when bent around the 20 mm mandrel, and less than 0.01 dB/turn when bent around 30 mm mandrel. The optical fiber embodiments corresponding to Tables 4, 5 and 6 have mode field diameters (MFD) between about 8.5 microns and about 9.1 microns at 1310 nm, and between about 9.6 microns and about 10.3 microns at 1310 nm; Cable Cutoff between 1190 nm and 1250 nm, and MACCab values between 7.1 and 7.6 (MACCab=MFD in microns at 1310 nm/Cable Cutoff in microns).

The relative refractive index profiles of a comparative example fiber (rectangular trench) and exemplary fiber embodiments (exemplary fiber embodiments 1, 2 and 3) of Table 1A are illustrated in FIG. 2. More specifically, FIG. 2 illustrates that the exemplary fiber embodiments 1 and 2 have a step like core profile (α=20), and that the exemplary fiber embodiment 3 has a parabolic profile (α=2). Exemplary fiber embodiments 1-3 have trenches having shallower depression in the inner part of the trench and a deeper depression in the outer part of the trench (i.e., the relative refractive index delta is more negative at or near the outer part of the trench). Exemplary embodiment 1 has a radius r₃ that is the same as the outer trench radius of the comparative example fiber 1 and smaller trench volume V₃. Fiber Example 2 has a radius r₃ that is larger than that of Fiber Example 2, but the trench has the larger volume V₃ as that of the comparative fiber. Exemplary embodiment 3 has a trench volume the same as that of the exemplary embodiment 2.

FIG. 3 illustrates the bend loss as a function of bend diameters for Fiber examples 1, 2 and 3 (i.e., for the Exemplary embodiments 1-3) and for the comparative example 1 fiber of Table 1. FIG. 3 illustrates that the fibers with square trench profile and triangular trench profile have similar bend loss at 10 mm bend diameter (5 mm bend radius) but the fiber with a non-rectangular or triangular trench design has similar or better bend loss performance at 30 mm bend diameter (15 mm bend radius).

The relative refractive index profiles of another comparative example fiber 2 (rectangular trench) and three fiber embodiments (Fiber Examples 4, 5 and 6) of Table 1 are illustrated in FIG. 4. The fibers in FIG. 4 have an updoped outer cladding region 4. More specifically, FIG. 4 illustrates that Fiber Examples 4 and 5 have a step like core profile (α=20), and Fiber Example 6 has a parabolic profile (α=2). Fiber Examples 4-6 have triangular trenches having shallower depression in the inner part of the trench and a deeper depression in the outer part of the trench. Fiber Example 4 has a radius r₃ that is larger than the outer trench radius of the comparative example fiber. Fiber Example 5 has a radius r₃ that is larger than that of Fiber Example 4. Fiber Example 6 has a trench shape that is different than Fiber Example 5, but the trench volume is similar for Examples 5 and 6. The shape of the trench region 3 and the updoping of outer cladding region (with respect to first inner cladding region 2) also helps in having larger trench volume V₃ (˜105% micron) and simultaneously have cable cutoff less than 1260 nm.

FIG. 5 illustrates the Bend loss as a function of bend diameters for Fiber Examples 4, 5 and 6 of Table 1B and for the second comparative example fiber. Applicants discovered that the fiber with square moat and triangular moat have similar bend loss at 10 mm bend diameter (5 mm bend radius) but the triangular trench fiber design has much better bend loss performance at 30 mm bend diameter (15 mm bend radius). If the trench volume is increased, fiber performance improves even further.

The relative refractive index profiles for another modeled fiber corresponding to this profile are illustrated in FIG. 6. The measured optical properties of the manufactured fiber Example 7 are shown in Table 3, demonstrating good bend performance and other properties compatible with G.657 and G.652 specifications.

Preferably, exemplary optical fiber embodiments 10 exhibit a bend loss at 1550 nm, when wound upon on a 20 mm diameter mandrel, of less than 0.5 dB/turn, and in some cases less than 0.25 dB/turn. These fibers also exhibit a bend loss at 1550 nm, when wound upon on a 10 mm diameter mandrel, of less than 2 dB/turn, more preferably less than 1 dB/turn, more preferably less than 0.5 dB/turn, and some fibers most preferably less than 0.2 dB/turn. These fibers also exhibit a bend loss at 1550 nm, when wound upon on a 30 mm diameter mandrel, of less than 0.01 dB/turn, and some fibers more preferably less than 0.003 dB/turn. Some of these examples employ chlorine in the outer cladding region in an amount greater than 2000 ppm, and in some cases greater than 3 000 or even greater than 4000 ppm by weight. In some embodiments the outer cladding region comprises chlorine in an amount greater than 2000 and less than 12000 ppm by weight.

Some exemplary optical fiber embodiments 10 exhibit a bend loss at 1550 nm, when wound upon on a 15 mm diameter mandrel, of less than 0.5 dB/turn, and in some cases less than 0.25 dB/turn. At least some of these e fibers also exhibit a bend loss at 1550 nm, when wound upon on a 10 mm diameter mandrel, of less than 1 dB/turn, more preferably less than 0.5 dB/turn, and some fibers most preferably less than 0.2 dB/turn. The fibers exhibit a bend loss at 1550 nm, when wound upon on a 15 mm diameter mandrel, of less than 0.25 dB/turn, and some fibers more preferably less than 0.15 dB/turn. The fibers exhibit a bend loss at 1550 nm, when wound upon on a 20 mm diameter mandrel, of less than 0.1 dB/turn, and some fibers more preferably less than 0.03 dB/turn.

Attenuation (spectral) at 1550 nm is preferably less than 0.21 dB/km, more preferably less than 0.20 dB/km, even more preferably less than 0.197 dB/km. In some preferred embodiments the attenuation (spectral) at 1550 nm is less than or equal to 0.191 dB/km, even more preferably less than or equal to 0.189 dB/km, even more preferably less than or equal to 0.182 dB/km.

Thus, the embodiments of the optical fibers 10 described herein provide outstanding bending performance, and additionally provide cutoff wavelengths suitable for single mode operation at wavelengths greater than about 1260 nm.

In some embodiments, the core may comprise a relative refractive index profile having a so-called centerline dip which may occur as a result of one or more optical fiber manufacturing techniques. However, the centerline dip in any of the relative refractive index profiles disclosed herein is optional.

The optical fiber disclosed herein comprises a core and a cladding layer (or cladding or outermost annular cladding region) surrounding and directly adjacent the core. Preferably, the core is comprised of silica doped with germanium, i.e. germania doped silica. Dopants other than germanium, singly or in combination, may be employed within the core, and particularly at or near the centerline, of the optical fiber disclosed herein to obtain the desired refractive index and density. In preferred embodiments, the core of the optical fiber disclosed herein has a non-negative relative refractive index profile, more preferably a positive relative refractive index profile, wherein the core is surrounded by and directly adjacent to a cladding layer.

Preferably, the optical fiber disclosed herein has a silica-based core and cladding. In preferred embodiments, the cladding has an outer diameter, 2 times r₄, of about 125 micron.

The fibers disclosed herein exhibit low PMD values particularly when fabricated with OVD processes. Spinning of the optical fiber may also lower PMD values for the fiber disclosed herein.

It is to be understood that the foregoing description is exemplary only and is intended to provide an overview for the understanding of the nature and character of the fibers which are defined by the claims. The accompanying drawings are included to provide a further understanding of the preferred embodiments and are incorporated and constitute part of this specification. The drawings illustrate various features and embodiments which, together with their description, serve to explain the principals and operation. It will become apparent to those skilled in the art that various modifications to the preferred embodiments as described herein can be made without departing from the spirit or scope of the appended claims.

Claims

1. A single mode optical fiber comprising: a central core region having outer radius r1 and relative refractive index Δ1;a cladding region comprising (i) a first inner cladding region having an outer radius r2>6 microns and relative refractive index Δ2 and 0.3≦r1/r2≦0.85; (ii) and a second inner cladding region having an outer radius r3>9 microns and comprising a minimum relative refractive index Δ3, wherein said second cladding region has at least one region with a relative refractive index delta that becomes more negative with increasing radius; and (iii) an outer cladding region surrounding the inner cladding region and comprising relative refractive index Δ4, wherein Δ1>Δ2>Δ3, Δ3<Δ4.

2. The optical fiber of claim 1 wherein 0.15≦|Δ4−Δ3|≦0.7 and the absolute difference between Δ3 and Δ2 is greater than 0.03, the absolute value V3 of the second inner cladding region is 35% Δμm2≦V3≦105% Δμm2, said fiber exhibits a 22m cable cutoff less than or equal to 1260 nm, and has a zero dispersion wavelength λo and 1300 nm≦λo≦1324 nm.

3. The optical fiber of claim 2 wherein 0.20≦|Δ4−Δ3|≦0.7.

4. The optical fiber of claim 2 wherein 0.25≦|Δ4−Δ3|≦0.7.

5. The optical fiber of claim 2 wherein 0.35≦|Δ4−Δ3|≦0.7.

6. The optical fiber of claim 1, wherein the first inner cladding region is essentially free of fluorine and germania.

7. The optical fiber of claim 1, wherein Δ4>Δ2 for a length extending from r3 to a radius of at least 30 microns.

8. The optical fiber of claim 1, wherein 0.33≦r1/r2.

9. The optical fiber of claim 1, wherein the profile volume, V4 of the outer cladding region, calculated between the outer radius of the second inner cladding region and a radial distance of 30 um, is equal to:

10. The optical fiber of claim 1, wherein said fiber exhibits a bend loss of less than 0.75 dB/turn when wound upon on a 20 mm radius mandrel and exhibits a MAC number between 6.6 and 7.5.

11. The optical fiber of claim 1, wherein the width of second inner cladding region r3−r2 is between 3 and 20 microns.

12. The optical fiber of claim 10, wherein said fiber exhibits a bend loss of less than 1 dB/turn when wound upon on a 15 mm radius mandrel.

13. The optical fiber of claim 1, wherein the second inner cladding region contains less than 0.02 wt % fluorine.

14. The optical fiber of claim 1, wherein said central core region comprises essentially germania doped silica.

15. The optical fiber of claim 1, wherein 1.5≧β≧0.25, where and

16. The optical fiber of claim 14, wherein 1.1≧β≧0.5.

17. The optical fiber of claim 14, wherein 1.1≧β≧0.75.

18. The optical fiber of claim 1, wherein 50≧αt, where αt is the trench alpha parameter.

19. The optical fiber of claim 18, wherein 5≧αi≧0.5.

20. The optical fiber of claim 1, where said central core region has an alpha profile, alphacore, of 2<alphacore≦100.

21. The optical fiber of claim 20, where said central core region has an alpha profile, alphacore, of 2≦alphacore≦20.