Method of fabrication of low-bend-loss single mode fibers of very large mode areas
09594211 ยท 2017-03-14
Assignee
Inventors
Cpc classification
C03B2203/04
CHEMISTRY; METALLURGY
C03B37/016
CHEMISTRY; METALLURGY
C03B2203/26
CHEMISTRY; METALLURGY
G02B6/02338
PHYSICS
B29D11/00721
PERFORMING OPERATIONS; TRANSPORTING
C03B37/0122
CHEMISTRY; METALLURGY
C03B2203/18
CHEMISTRY; METALLURGY
C03B37/0279
CHEMISTRY; METALLURGY
G02B6/02333
PHYSICS
G02B6/02357
PHYSICS
C03B37/02718
CHEMISTRY; METALLURGY
International classification
C03B37/02
CHEMISTRY; METALLURGY
B29D11/00
PERFORMING OPERATIONS; TRANSPORTING
Abstract
The present invention provides an optical fiber and method of making the same. The optical fiber includes a body for transmitting light. The body has an anisotropic refractive index wherein the anisotropic refractive index offsets changes in the refractive index of the fiber caused by bending the fiber. The fiber body may further include a core and cladding.
Claims
1. An optical fiber comprising: a body for transmitting light, said body having an anisotropic refractive index wherein said anisotropic refractive index offsets changes in the refractive index of the fiber caused by bending the fiber; said body made from a preform comprising a plurality of successive layers, each of said layers having a refractive index, the refractive index of each layer successively increases; and said layers are comprised of rows of tubes having solid rods located therein wherein the reflective index of each row unidirectionally increases by varying the diameters of the rods in the tubes.
2. The optical fiber of claim 1 wherein the anisotropic refractive index varies continuously.
3. The optical fiber of claim 1 wherein the anisotropic refractive index is unidirectional and decreases in a direction away from the center of the bend, such that the rate of refractive index variation as a function of the transverse dimension of the fiber that is aligned with the direction of bending is proportional to the first order on the inverse of the design bend radius.
4. The fiber of claim 1 wherein said anisotropic refractive index changes stepwise.
5. The fiber of claim 1 wherein said anisotropic refractive index has a predefined slope.
6. The fiber of claim 1 wherein said body comprises a core and cladding.
7. The fiber of claim 6 wherein said refractive index maintains transmitted light within the core when the fiber is bent.
8. The fiber of claim 1 wherein said refractive index n due to the bending at radius R has a slope of n/rn/R.
9. The fiber of claim 1 wherein said fiber has a refractive index pre-tilt of 1.510.sup.5/m and said fiber has a mode area greater than 500 um.sup.2.
10. The optical fiber of claim 1 wherein the anisotropic refractive index substantially cancels the bend loss of the fiber when the fiber is bent at bend radii within the design bend range.
11. The optical fiber of claim 1 wherein the refractive index of each layer unidirectionally increases.
12. The optical fiber of claim 1 wherein the refractive index of each layer increase stepwise by 310.sup.4 between adjacent layers.
13. A method of making an optical fiber comprising the steps of: providing a preform, said preform comprising a plurality of successive layers, each of said layers having a refractive index, the refractive index of each layer successively increases; and drawing said preform in a furnace to create an optical fiber, said furnace heats opposing sides of said preform at different temperatures to create an anisotropic refractive index in said optical fiber.
14. The method of 13 wherein said preform is comprised of rows of solid rods or hollow tubes, said tubes having substantially the same outer diameter and each successive row of tubes having incrementally smaller inner diameters.
Description
BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWINGS
(1) In the drawings, which are not necessarily drawn to scale, like numerals may describe substantially similar components throughout the several views. Like numerals having different letter suffixes may represent different instances of substantially similar components. The drawings illustrate generally, by way of example, but not by way of limitation, a detailed description of certain embodiments discussed in the present document.
(2)
(3)
(4)
(5)
(6)
(7)
(8)
(9)
(10)
(11)
(12)
(13)
(14)
(15)
(16)
(17)
(18)
(19)
(20)
DETAILED DESCRIPTION OF THE INVENTION
(21) Detailed embodiments of the present invention are disclosed herein; however, it is to be understood that the disclosed embodiments are merely exemplary of the invention, which may be embodied in various forms. Therefore, specific structural and functional details disclosed herein are not to be interpreted as limiting, but merely as a representative basis for teaching one skilled in the art to variously employ the present invention in virtually any appropriately detailed method, structure or system. Further, the terms and phrases used herein are not intended to be limiting, but rather to provide an understandable description of the invention.
(22) Optical fiber bend loss is related to the radius of curvature R of a typical step index fiber. When the actual radius of curvature approaches a critical value R.sub.c, the bend loss increases sharply from negligible values to intolerably large values, implying very large bend losses when fibers with A.sub.eff>1000 m.sup.2 are not kept straight. An approximate expression for R.sub.c is given by: R.sub.c20/[{square root over (n)}(2.7480.996/.sub.c)].sup.3, where the critical radius is a function of the refractive index difference (n), the operating wavelength () and the cutoff wavelength (.sub.c). For a single-mode step index fiber, for a desired mode area, A.sub.eff (and a wavelength of 1.55 m), Table 1 depicts calculated values of the core radius, numerical aperture (NA), and the critical bend radius, R.sub.c.
(23) TABLE-US-00001 TABLE 1 Parameters of step index optical fibers and critical bend R.sub.c for different desired mode areas in single mode fibers (assuming a normalized frequency V = 2.405, .sub.c = 1.5 m, = 1.55 m, = mode field radius and a radius of step index core) A.sub.eff, desired mode area (.sup.m.sup.2) (.sup.m) a (.sup.m) NA .sup.n R.sub.c (m) 100 5.64 5.13 0.112 0.00431 0.022 300 9.77 8.88 0.065 0.00144 0.112 500 12.62 11.46 0.05 0.00086 0.241 1000 17.84 16.21 0.035 0.00043 0.683 2000 25.23 22.93 0.025 0.00022 1.932 3000 30.9 28.08 0.02 0.00014 3.549 4000 35.68 32.42 0.018 0.00011 5.464
(24) An aspect of the present invention is illustrated schematically in
(25) Using the following expression: n.sub.e.sup.2=n.sup.2 (r)(1+2r/R) for the effective refractive index profile of a uniform index fiber at a bend radius R, the effective refractive index or tilt due to the bending (at radius R) has a slope of n/rn/R. The stress-induced index changes can be accounted for by adding another small multiplicative factor to this index gradient. Such bend induced index gradients can cause mode distortions and severe bend-induced propagation losses. The present invention, in one embodiment, negates or counteracts these bend-index losses by pre-tilting the index in the opposite direction to offset the bend-induced index changes. In one embodiment, the design of the fiber of the present invention involves using a fiber in which the refractive indices in the core and cladding are pre-tilted to maintain minimum mode loss at the desired modes, usually the lowest order mode, when the fiber is bent. In general, the fiber may have an anisotropic refractive index that has a predefined linear slope. In other embodiments, the anisotropic index variation may be nonlinear, curved and in other predetermined or predefined variations as well as a continuous rate of change.
(26) Accordingly, to reduce bend loss in the optical fiber, in a preferred embodiment, the present invention provides an optical fiber comprising a core and a cladding wherein the refractive index of the core and the cladding varies anisotropicallyin the direction of the bendacross the core and the cladding. In addition, the refractive index of the core alone, or within both the core and the cladding, may vary monotonically across the fiber, in such a manner that a significant portion of this variation is aligned along the direction of the bend. More specifically, in a bendable or bent fiber, the refractive index of the fiber decreases in a direction away from the direction in which the fiber is bent or curved. In yet another preferred embodiment, the refractive index of the optical fiber unidirectionally decreases in a direction away from the direction in which the fiber is bent or curved. In yet another embodiment, the bendable optical fiber comprises a core and/or cladding having an anisotropic refractive index wherein the anisotropic refractive index offsets changes in the refractive index of the fiber caused by bending the fiber. In yet other embodiments, the optical fiber has an anisotropic refractive index variation that is unidirectional and decreases in a direction away from the center of the bend, such that the rate of refractive index variation as a function of the transverse dimension of the fiber that is aligned with the direction of bending is proportional to the first order on the inverse of the design bend radius.
(27) While the tilt has been described as being in the core, cladding or both, it may also be in a portion or part of the fiber. It is also within the scope of the present invention to view the tilt as being in the body of the fiber, with the body including one or more parts, portions or components of the fiber such as cladding and/or core.
(28) In other embodiments of the present invention, the optical fiber may have a bend radius of between 3 cm and 50 cm with no significant bend loss. In a preferred embodiment, the fiber may have a refractive index pre-tilt of the order of 1.510.sup.5/M in UGRIP VLMA fibers of bend radii between 5 and 10 cm, and mode areas >1000 m.sup.2; this pre-tilt will be increased for smaller design bend radii, and decreased for larger bend radii. In other embodiments, the fiber may have a refractive index pre-tilt of the order of 110.sup.5/m or 210.sup.5/m or in the range of 110.sup.3 to 110.sup.7/um.
(29) In certain embodiments, bend losses may be eliminated nearly completely while retaining very large mode areas in the fundamental mode even for very small design bend radii. This may be achieved by fabricating a fiber that has a pre-defined, built-in tilt in its core and/or cladding with one or more refractive index profiles that offset bend losses. For example, bending the fiber one way will cancel the built-in index while bending it the other way will increase the refractive index tilt. When the tilt is completely cancelled or substantially cancelled, the bend loss will be negligible and may be nearly eliminated vis--vis the needs of the device. Bending the fiber one way will cancel the built-in index while, bending it other way will increase the tilt. When the tilt is reduced or cancelled, there will be significantly reduced bend loss. Under these conditions it is possible to obtain very large mode area fibers with very small effective NAs.
(30) As shown in
(31) In addition to stepwise changes, the tilt may be accomplished as a gradient or grading. The tilt, gradient or grading may also be incremental or continuous. In other embodiments, a graded index tilt may be obtained by using a custom fiber preform in which two opposing sides of a conventional circular step-index or graded-index preform have been shapedpreferably, but not necessarily to flat surfacesand the refractive index gradient is achieved during the draw process in a draw furnace such that the two flat surfaces are adjacent to two distinct heating elements, which may be flat, whose temperatures are different, thereby causing the draw process to yield a drawn fiber with a stress and index gradient.
(32)
(33) As is the case for photonic crystal fibers (PCFs) fabricated by a stack and draw technique, in which the preform consists of a collection of capillary tubes that are drawn into the PCF fiber, the air holes in the capillary tubes reduce the effective index in the fiber. One method to create the present fiber is to start with a preform in which small rods of very precise refractive index are arranged in rows to create the desired refractive index profiles, including addition of suitably elevated refractive index rods, doped with the desired rare earth or other gain dopants such as Yb if necessary, for the region comprising the core. Another method to create the embodiments described herein is to vary the effective refractive index in the cladding and/or core in a chosen direction in the vicinity of the core to achieve the desired tilted refractive index profile by monotonically varying the size of the air holes in the capillary tubes along a desired direction, with appropriate modifications to the index values, and thus of the hole sizes in the capillary tubes comprising the core region. The use of appropriate anisotropic cladding shapes or flat surfaces aligned parallel or perpendicular to the direction of the index gradient should help keep track of the direction of the index change, and thus of the direction of the winding/coiling of the fiber around the spools to precisely neutralize the bend loss that would have been experienced during the winding of a conventional LMA fiber around the spool.
(34) The present invention further provides a method of fabrication that uses preforms that may be fabricated by using an appropriately designed core surrounded by layers of hollow capillary tubes of continually varying air-hole sizes. Embodiments deploying this design are shown in
(35)
(36) The structures described herein may be fabricated via ultrasonic drilling of solid glass preforms and by using the other techniques described below. Lastly, arrow 330 indicates the direction of the general unidirectional increase in the refractive index, which may be achieved by small incremental increases in the effective refractive index from one row to the next in the cladding region, with row 9 in the cladding region having the largest holes and the smallest average refractive index and row 1 in the cladding region having the smallest holes and largest average refractive index. The refractive index in the core regions will have to be increased in a manner that enables the desired light guiding properties.
(37) Table 2 shows representative design parameters for fabrication of a unidirectional linear refractive index gradient preforms of an embodiment of the present invention using a 9-row varying inner diameter capillary tube designs.
(38) TABLE-US-00002 TABLE 2 Design parameters for fabrication of a unidirectional linear refractive index gradient preform with capillary tubes of varying diameter. Designed refractive index values (column 2) and inner diameters (column 3) are given for each row of this 9-layer perform. The corresponding diameters of the holes in the rows of the drawn fiber are indicated in Column 4. This design corresponds to a n = 3 10.sup.4 (refractive index gradient of the capillary tube) and a n = 4 10.sup.4 (size of corrected step index) and linear index gradient of 1.4 10.sup.4/micron in the fiber design. D.sub.i, inner n.sub.eff, diameter of d.sub.i ,inner effective hole in diameter of Row refractive capillary hole in number index tube, m fiber, m 9 1.4569 163 1.63 8 1.4572 154 1.54 7 1.4575 146 1.46 6(clad) 1.4578 136 1.36 5(clad) 1.4581 127 1.27 4(clad) 1.4584 116 1.16 3 1.4587 104 1.04 2 1.459 91 0.91 1 1.4593 75 0.75 6(core) 1.4582 123 1.23 5(core) 1.4585 112 1.12 4(core) 1.4588 100 1
(39)
(40) Specifically,
(41) As stated above, a preferred embodiment of the preform and any subsequent fiber may have one or more flat surfaces to enhance coupling. Configurations that may be so arranged include, but are not limited to, a triangular or trapezoidal shaped preform which can be easily achieved by reducing the width of Row 9 and using an outer triangular or trapezoidal shaped holding tube.
(42) In preforms 400 and 470, one or more opposingly located solid rods 450-458 may be located near the periphery of the outer one or more containment tubes (which can also be of lower index material for pump diode confinement), which act as spacer rods that create a more stable and rugged structure. The tubes making up the rows may be held in place either by fusing and sealing one end (which becomes the top end) or by using matched porous or nonporous retaining plate cap structures that are fused to one or both ends of the preform. The porous structures enable control of internal gas pressure and the use of an inert gas such as nitrogen or argon. The nonporous retaining plate structures are used for fiber draws with pre-set internal pressures.
(43) Although the circular containment tubes of
(44) Other embodiments of the invention may include marker rods 460-462, as shown in
(45) As an illustrative example of typical dimensions, for the 9-row embodiments discussed above, an outer capillary tube diameter of 2 mm in
(46) Another UGRIP fiber shape of the present invention is that of a trapezoidas discussed aboveand also shown in
(47) The designed refractive index values (Column 2) correspond to an index step of 310.sup.4 between adjacent reduced tube elements in the drawn fiber, corresponding to an index gradient of 1.510.sup.5/um in the UGRIP fiber, assuming a reduction factor of 100:1 in the preform to-fiber conversion. Based on this design, the inner diameter for the holes in the capillary tube, are tabulated in Column 3 of Table 2. For an undoped fiber, or for doped fibers in which the refractive index of the core capillary tubes can be matched precisely to the refractive index of the cladding capillary tubes, the desired step index (targeted at 410.sup.4) can be readily achieved by simply reducing the diameters of the holes in the core rods for the same row as shown in the last three rows of Table 2.
(48)
(49) TABLE-US-00003 TABLE 3 Design parameters for fabrication of a unidirectional linear refractive index gradient perform with capillary tubes of fixed diameter and fiber inserts of varying diameter. Designed refractive index values (column 2) and diameter of fiber insert (column 4) are given for each row of the 9 layer perform as required to achieve an index gradient of 1.5 10.sup.5 /micron in the microstructured fiber. This design corresponds to a n = 3 10.sup.4 (refractive index gradient of the capillary tube) and a n = 4 10.sup.4 (size of corrected step index). D.sub.i, inner Diameter n.sub.eff,I diameter of of fiber effective hole in insert in Row refractive capillary perform number index tube (m) (m) 9 1.4569 1000 0 8 1.4572 1000 26 7 1.4575 1000 36 6(clad) 1.4578 1000 44 5(clad) 1.4581 1000 51 4(clad) 1.4584 1000 57 3 1.4587 1000 62 2 1.459 1000 67 1 1.4593 1000 72 6(core) 1.4582 1000 53 5(core) 1.4585 1000 59 4(core) 1.4588 1000 64
(50) Column 4 of Table 3 shows the calculated diameters of the one or more fiber inserts 501-507 needed in each row to achieve an index gradient similar to the inner diameter capillary tube designs of
(51) A method of fabricating the embodiment shown in
(52) 10 kW-100 kW fiber arrays require higher power single elements and scalable beam combining techniques, such as the use of side pumping for efficient power scaling. As a result, the present invention provides a near-monolithic high power fiber laser system 600 as shown in
(53) The refractive index tilts in opposingly shaped trapezoids will be in opposite directions relative to the wide bases, i.e., such that the index gradients will all be pointed in the same direction to allow effective compensation for bend-induced index tilts. Alternatively, these array sections could be very short straight sections such that the propagation losses are negligible, and the straight sections have been designed simply to facilitate coherent coupling in a rugged well-designed packaged configuration.
(54) In the preferred embodiment illustrated in
(55) A small straight portion of tilted index semi-hexagonal fiber at both ends of the laser may be used to remove higher order modes (via use of mode-dependent losses in these UGRIP fibers, analogous to using coiled regions in conventional non-tilted index fibers). The water-cooled metallic grooved cylinder 650 may be used to spool the fibers and will remove heat generated inside the fiber laser.
(56) In other embodiments, fabrication techniques similar to those used for the fabrication of holey fibers may be used. For such an implementation, the preform will be made using a central core rod and a series of hollow capillary tubes of continually varying air-hole sizes. The holes in the tubes reduce the effective index in the fiber when the preform, consisting of the collection of tubes, is drawn into a fiber. By monotonically varying the size of the air holes in the tubes, the effective refractive index in the cladding in a chosen direction may be varied or predetermined to achieve the desired tilted refractive index profile.
(57) Anisotropic cladding shapes and coatings may also be used to help keep track of the direction of the index change, and thus of the direction of the winding of the fiber around the spools to precisely neutralize the bend loss that would have been experienced during the winding of a conventional LMA fiber around the spool. The embodiments of the present invention may achieve a bend loss of less than 0.1 dB/m, even with bend radii as small as 10 cm while providing relatively compact footprints for LMA-based fiber lasers.
(58) In other embodiments, the fibers of the present invention may be constructed by a two-step process. In the first step, the preform is introduced into the furnace of a fiber drawing tower and is heated to about 2000 C., where it is fused together and drawn down to the order of millimeter size, using gravity and pressure. In a preferred embodiment, a microstructured fiber may be fabricated by using a capillary stacking and draw method in accordance with the following parameters: Temperature: 1650-2300 degrees C., Feed rate: 1-5 mm/min, Pressure: 1.5-5.5 torr. Through careful process control, the air holes retain their arrangement all through the drawing process and even fibers with very complex designs and high air filling fraction can be produced.
(59) In other embodiments, holey fiber (HF) preforms may be fabricated by stacking capillary tubes around a rare-earth doped solid rod of the same outer diameter. The RE-doped solid rod (which becomes the core subsequent to the fiber draw) is fabricated by using a conventional MCVD process to obtain a high dopant distribution in the center, and will have a ring-like elevated index near its periphery with a NA of 0.05 or lower (n810.sup.4). High Yb and Er concentrations may be used along with phosphate co-doping to reduce the effect of concentration quenching of the Er ions. In addition, the inner rod may be Ge-doped to make the core photosensitive and thereby enable the fabrication of in-line gratings.
(60) As shown in
(61) These modified preforms, which may include rare-earth (RE)-doped solid tube cores 905, capillary tubes 907, and air holes 908 may be configured as described above. The preform is drawn into the desired advanced double clad fiber (DCF). Subsequent to the drawing process, the glass inner claddings may be coated with a low index polymer outer cladding 913 to obtain the final fibers. To preserve the orientation of the fiber and memory of the tilt-index, these coatings may be made to conform to the shape of the fiber. Such low-index polymeric cladding materials are generally very absorbing in the ultraviolet and will thus be removed for the grating (FBG) fabrication process, followed by a recoating to reduce the pump losses in these regimes. To make such fibers sensitive to UV light, a Ge dopant may be added. The core may also be located near the flat surface to ensure that a strong FBG is obtained.
(62) As an alternative, the lower index outer cladding region of the DCF fiber may be fabricated by enlarging the hole sizes of two or more rows of capillaries at the desired distance from the core. This will enable circumvention of the use of a polymer cladding. Likewise D-shaped coreless pumping fibers may also be drawn in a similar way. Polarization maintenance in such fibers is achieved by either using boron stress rods or by proper arrangement of different air hole sizes along two different directions around the core.
(63)
(64) In one preferred embodiment, the present invention includes all of the following criteria: An advanced LMA core design, enabling single mode areas of >1000 m.sup.2 with bend losses of <0.1 dB/m (i.e. total bend losses of <2 dB for a 20 m long fiber). A Yb-dopant profile with a gain in the lowest order transverse mode (i.e. with a higher concentration of optically pumped Yb-dopant near the center of the mode). A large net birefringence at the core of the order of 510.sup.4 or larger to facilitate polarization maintenance.
(65) Other embodiments may include dopants (such as Ge or B) at strategic locations in the fiber or by using other stress inducing structures such as borosilicate rods or appropriate air-hole distribution in the preform (and thus the fiber). An inner cladding design which is not circularly symmetric, and which yields a relatively small inner-cladding-to-core area ratio (<50), combined with a significantly large peak Yb dopant density (10,000 ppm) to enable efficient absorption of the pump radiation for high slope and optical-to-optical power conversion efficiencies. A core dopant (Ge) that enables photosensitivity and fabrication of FBGs and large-period gratings (LPGs) in the core or cladding directly in the Yb-doped fibers (YDFs) may also be used. Offsetting of the LMA core to one side of a flat-faced inner cladding (and an easily removable polymer outer cladding of low refractive index) may be used to enable lithography of FBGs and LPGs on the fiber. In accordance with one or more of the criteria described above, several preferred embodiments are shown in
(66) In other aspects, embodiments of the present invention provide HF preforms fabricated by stacking capillary tubes around a solid rod of the same outer diameter, d.sub.0. The solid rod (which will form the core) may be fabricated by a conventional MCVD process to obtain a very high dopant distribution in the center (up to a diameter of d.sub.0/2), and will have a ring like elevated index near its periphery with a NA of 0.05 or lower (n810.sup.4). High Yb concentrations (between 3,000 ppm and 15,000 ppm) may be used along with aluminum co-doping to reduce the effect of concentration quenching of the Yb ions. In addition, the inner rod may be Ge doped to make the core photosensitive and thereby enable the fabrication of in-line gratings.
(67)
(68) Sol-gel glass technology provides an inexpensive and reliable method for fabricating the fibers of the present invention. Suitable chemical precursor compositions include ethanol, water, hydrofluoric acid (HF), n, n-dimethylformamide (DMF), and tetraethyl orthosilicate with hydrofluoric acid (HF) as a catalyst for sol gel processing. DMF may also be used to minimize cracking. Two specific advantages of using HF are: HF catalyzed gels have much shorter gelation times (about 12 hours) than other catalyzed gel solutions. The bulk densities and porosities of the HF-catalyzed gels are similar to those of the base catalyzed gel. Larger average pore sizes are obtained, which help minimize cracking problems.
(69) One suitable procedure to make the gel and reduce the capillary pressure which leads to cracking is to use a capillary pressure, Pc, which is given by
(70)
where is contact angle and rlv, sv, and sl, denote the interfacial tensions between the liquid and the vapor, the solid and the vapor, and the solid and the liquid respectively. In order to overcome the cracking problem by reducing the capillary pressure, DMF was introduced to reduce the average value of rlv in the solution. DMF was found to be a good drying control chemical additive, with a low rlv and a relatively low boiling point (153 C.).
(71) Using a mixture of DMF and HF was found to be a better chemical combination for fabrication of a crack-free gel. This is because DMF lowers the interfacial tension between the liquid and the vapor. More SiF bonds form during the gelation stage and cover the gel's surface and increase the contact angle and lowers capillary pressure leading to reduced cracking.
(72) A heating profile that may be used to process the gels is shown in
(73) The final design parameters for the UGRIP mold design (bend radius 7.5 cm) have been calculated and are included in Table 4 below.
(74) TABLE-US-00004 D.sub.i, inner d.sub.i, inner diameter of diameter of Row n.sub.eff, effective holes in the holes in the number refractive index mold, m fiber, m 9 1.4729 1020 2.55 8 1.4732 1000 2.50 7 1.4734 980 2.45 6(clad) 1.4737 960 2.40 5(clad) 1.4739 940 2.35 4(clad) 1.4742 920 2.30 3 1.4744 900 2.25 2 1.4747 876 2.19 1 1.4750 856 2.14 6(core) 1.4743 960 2.40 5(core) 1.4740 940 2.35 4(core) 1.4738 916 2.29
(75)
(76) While the foregoing written description enables one of ordinary skill to make and use what is considered presently to be the best mode thereof, those of ordinary skill will understand and appreciate the existence of variations, combinations, and equivalents of the specific embodiment, method, and examples herein. The disclosure should therefore not be limited by the above described embodiments, methods, and examples, but by all embodiments and methods within the scope and spirit of the disclosure.