NZ749887B2 - Flexible optical-fiber ribbon - Google Patents

Abstract

The flexible optical-fiber ribbon can be reversibly adapted to both planar and non-planar shapes (e.g., packed via folding or rolling) without damaging the optical-fiber ribbon or its constituent optical fibers. This is achieved by bonding the plurality of optical fibres with a cured ribbon matrix (14) having elongation to break of at least 200% and a low Young's modulus of 1-20 MPa at 20 C. 14) having elongation to break of at least 200% and a low Young's modulus of 1-20 MPa at 20 C.

Description

FLEXIBLE OPTICAL-FIBER RIBBON FIELD OF THE INVENTION The present invention relates to optical-fiber ribbons.

BACKGROUND Optical fibers provide ages over conventional ication lines.

As compared with traditional wire-based networks, l-fiber communication ks can transmit cantly more information at significantly higher speeds. Optical fibers, therefore, are being singly employed in communication networks. US. Patent No. 5,682,454, which is hereby incorporated by nce in its entirety, discloses an exemplary optical-fiber cable, Optical fibers can be bonded together to form a planar, optical-fiber ribbon, which itself may be ble into subunits (e. g., a twelve-fiber ribbon that is splittable into six—fiber ts). Multiple optical-fiber ribbons may be aggregated to form a ribbon stack, which can have various sizes and shapes, such as a rectangular ribbon stack or a trapezoidal ribbon stack in which the uppermost and/or lowermost optical-fiber ribbons have fewer optical fibers than those toward the center of the stack. The ribbon-stack configuration helps to increase the density of optical elements (e. g., ribbonized optical fibers) within a round buffer tube and/or a round optical-fiber cable. Even so, the placement of planar, optical-fiber ribbons as rectangular or trapezoidal ribbon stacks within round tubes is spatially inefficient.

Mass-fusion splicing of optical-fiber ribbons requires a planar ribbon geometry, however, rendering non—planar, optical—fiber ribbons unsuitable for mass—fusion ribbon splicing operations.

SUMfl Accordingly, in one aspect, the present invention embraces a flexible optical-fiber ribbon that can be adapted to both planar and non-planar shapes (e. g., packed via g or g) without damaging the l-fiber ribbon or its constituent optical fibers.

The optical-fiber ribbon may be manufactured as a substantially planar optical-fiber ribbon that can be reversibly folded or rolled into a compact configuration to facilitate efficient packing within an optical-fiber cable. In a planar configuration, the optical-fiber ribbon is suitable for mass-fusion spicing.

In an exemplary embodiment, the flexible optical-fiber ribbon includes a plurality of l fibers bonded in a side-by-side arrangement via a predominantly one-sided application of ribbon-matrix material. The substantially cured ribbon-matrix material has elongation—to-break and modulus teristics that promote reversible folding and rolling of the optical-fiber ribbon.

The foregoing illustrative summary, as well as other exemplary objectives and/or advantages of the invention, and the manner in which the same are accomplished, are further explained within the following detailed description and its accompanying drawings.

BRIEF DESCRIPTION OF THE DRAWINGS Figure 1 depicts a cross-sectional perspective of an exemplary two-side, edge—bonded optical—fiber ribbon.

Figures 2 and 3 depict cross-sectional perspectives of exemplary one-side, edge-bonded optical-fiber ribbons having predominantly one-side edge bonding.

Figure 4 depicts a sectional ctive of another exemplary two—side, edge-bonded optical-fiber .

Figure 5 depicts Young’s modulus as a function of temperature for various ribbon-matrix materials.

Figure 6 depicts an exemplary one-side, onded ribbon efficiently packed within a micromodule.

Figures 7 and 8 depict cross-sectional perspectives of an exemplary one-side, edge-bonded optical-fiber ribbon having predominantly one-side edge bonding in a planar configuration and a folded configuration, tively.

Figure 9 depicts dimensional parameters for exemplary optical—fiber ribbons.

DETAILED DESCRIPTION In one aspect, the present invention embraces a flexible optical-fiber ribbon that can be folded or rolled into a t shape and then unfolded or unrolled to a planar arrangement of parallel optical fibers without breaking the ribbon structure or damaging the constituent optical fibers. In a substantially planar geometry, the flexible optical-fiber ribbon tates mass-fusion spicing. In a substantially non-planar geometry, the flexible optical-fiber ribbon facilitates increased spatial efficiency within a fiber optic cabling structure, such as a odule or a buffer tube.

As depicted in s 1—4, exemplary, flexible optical-fiber ribbons 10 each include a plurality of optical fibers 11 arranged side—by-side such that the optical fibers 11 are substantially parallel to one another. Each optical fiber 11, which includes a component glass fiber 12 and one or more surrounding coating layers 13, may be closely spaced or uous with an adjacent optical fiber 11 but typically should not cross over one another along the length of the optical-fiber ribbon 10. The optical fibers 11 may be ched, encapsulated, edge , joined, or otherwise aggregated by a substantially cured ribbon-matrix material 14. The resulting optical-fiber ribbon has a substantially planar (i.e., flattened) geometry that defines a relatively narrow height, a relatively wide width, and a substantially continuous length (e. g., over 1,000 meters, such as 5,000 meters or more).

As used herein, an optical-fiber ribbon 10 as depicted in Figures 1—4 inherently defines an upper side (i.e., the top), a lower side (i.e., the bottom), a left edge, and a right edge. The respective upper and lower sides define the major surfaces of the optical-fiber ribbon. Those having ordinary skill in the art will appreciate that flipping the optical-fiber ribbon 180 degrees over its major transverse axis will e the top and bottom, and so the terms can be used interchangeably herein depending on the frame of reference. Similarly, those having ordinary skill in the art will appreciate that yaw rotating the optical-fiber ribbon 180 degrees will reverse the right edge and left edge, and so the terms can be used interchangeably herein depending on the frame of nce. Accordingly, as used herein the terms “first side” and “second, opposite side” refer to the tive upper and lower sides of the optical-fiber ribbon, or vice versa depending on the frame of reference.

As used herein, the term “cured” refers to a ribbon-matrix material that has achieved at least 90 t of its maximum attainable modulus (e.g., Young’s modulus). In exemplary ments of the flexible optical-fiber ribbon, the cured ribbon-matrix material is at least 95 percent cured (i.e., the ribbon—matrix al has ed at least 95 percent of its maximum able Young’s modulus).

An exemplary, flexible optical-fiber ribbon may be manufactured using a die to selectively apply a -matrix material to one or both major surfaces of a side-by-side array of optical fibers. Thereafter, the ribbon-matrix material is cured upon the optical fibers, typically via UV-curing lamp(s) to initiate curing, to form the optical-fiber ribbon. Curing of the ribbon-matrix material may be enhanced using in-line thermal ovens, too.

In one ary embodiment depicted in Figure l, the optical—fiber ribbon 10 es optical fibers 11 dual-edge bonded with a cured ribbon-matrix material 14 (i.e., a two—side, edge-bonded optical-fiber ribbon). Ribbon-matrix material 14 is applied (1’) to the first side of the parallel optical fibers 11 (i.e., the upper side as depicted in Figure 1) to fully fill the curved, triangular regions defined by adjacent optical fibers 11 and (ii) to the second, opposite side of the parallel optical fibers 11 (i.e., the lower side as depicted in Figure l) to fully fill the curved, triangular regions defined by adjacent optical fibers 11.

In another exemplary embodiment, the optical -fiber ribbon includes optical fibers one-side, edge bonded with a cured —matrix material (i.e., at least 90-percent cured). In this regard, “one-side edge g” refers to an optical-fiber-ribbon geometry in which the ribbon-matrix material is surficially applied to one side of the arrangement of parallel optical fibers (e. g., via a inantly one-sided application of ribbon-matrix material to the parallel l fibers). Those having ordinary skill in the art will appreciate that some leakage can occur when applying the ribbon-matrix material to one side of the side-by-side arrangement of parallel l fibers.

Typically, the cured ribbon-matrix material edge bonds the plurality of optical fibers in a side-by—side arrangement such that at least 70 percent (e. g., 75 percent or more) of the cured ribbon-matrix material is present on one side of the optical-fiber ribbon (i.e., either on the optical-fiber ribbon’s upper side or lower side). In some ments of the optical-fiber ribbon, the cured ribbon-matrix material edge bonds the plurality of optical fibers in a side-by-side arrangement such that at least 80 percent (e. g., 90 percent or more) of the cured ribbon-matrix material is oned on one side of the optical-fiber ribbon (i.e., either on the optical-fiber ribbon’s upper side or lower side).

As depicted in Figures 2 and 3, respectively, the ribbon-matrix material 14 may be applied to only one side of the parallel optical fibers 11 to partly fill (Figure 2) or to fully fill (Figure 3) the curved, triangular regions defined by nt optical fibers 11. In this way, WO 22031 the cured ribbon-matrix material 14 one-side, edge bonds the parallel optical fibers 11 in a side-by-side arrangement. Those having ordinary skill in the art will appreciate that, even with the selective application of ribbon-matrix material 14 predominantly to only one side of the l-fiber ribbon 10 (i.e., either the top or bottom of the optical-fiber ribbon 10), some ribbon-matrix material 14 may migrate between adjacent optical fibers 11 or ooze around the t optical fibers 11 such that some cured ribbon-matrix material 14 is present on both sides of the l-fiber ribbon 10 (e. g., 85 percent on the upper side and 15 percent on the lower side, or vice versa depending on the frame of nce).

In another exemplary embodiment depicted in Figure 4, the optical-fiber ribbon 10 includes optical fibers 11 dual-edge bonded with a cured -matrix al 14.

Ribbon-matrix material 14 is applied (1') to the first side of the parallel optical fibers 11 (i.e., the upper side as depicted in Figure 4) to fully fill the curved, triangular regions defined by adjacent optical fibers 11 and (ii) to the second, opposite side of the parallel optical fibers 11 (i.e., the lower side as depicted in Figure 4) to partially fill the curved, triangular regions defined by adjacent optical fibers 11. Optionally, ribbon-matrix material can be applied to the first and second sides of the parallel optical fibers to partly fill the curved, triangular regions on both the optical-fiber ribbon’s upper side and lower side.

The substantially cured ribbon-matrix material has tion—to-break and modulus characteristics that promote reversible g and/or rolling of the optical—fiber ribbon. As used herein, the properties for the ribbon-matrix material are reported at standard temperature and pressure (STP), namely room temperature (i.e., 20°C) and atmospheric pressure (i.e., 760 torr).

In exemplary embodiments, the cured ribbon-matrix material has elongation-to- break (i.e., fracture strain) of at least 200 percent at 20°C, such as at least 300 percent at 20°C (e.g., 350 percent or more). Typically, the cured ribbon-matrix material has elongation-to- break of at least 400 percent at 20°C, such as at least 500 percent at 20°C (e.g., 600 percent or more). In some embodiments of the optical-fiber ribbon, the cured ribbon—matrix material has elongation-to-break of at least 700 t at 20°C, such as between about 800 percent and 1,500 percent (e. g., between about 1,000 percent and 1,200 percent), If elongation-to— break is too low, the -matrix material will crack and te when the l-fiber ribbon is folded or rolled (e.g., if the ribbon—matrix material is not cured before folding or rolling). Elongation-to-break (i.e., fracture strain) for ribbon-matrix materials can be determined via either ISO 527-3 : 1995 (Determination of Tensile Properties) or ASTM D882 - 12 (Standard Test Method for Tensile Properties of Thin Plastic Sheeting), each of which is hereby incorporated by nce in its entirety.

The cured ribbon-matrix material typically has low Young’s modulus over a broad temperature range. In ary embodiments, the cured ribbon-matrix material has Young’s modulus of between about 0.5 and 20 MPa at 20°C (e.g., 1—20 MPa), such as between 1 and 15 MPa at 20°C inclusively. Typically, the cured ribbon-matrix material has Young’s modulus of between 1.5 and 10 MPa at 20°C inclusively, such as between 2 and MPa at 20°C inclusively. In some embodiments of the optical-fiber ribbon, the cured ribbon-matrix material has Young’s modulus of less than 3 MPa at 20°C. Modulus (e.g., Young’s s) for ribbon—matrix materials can be ined via either ISO 527-3:l995 (Determination of Tensile Properties) or ASTM D882 - 12 (Standard Test Method for Tensile Properties of Thin Plastic Sheeting).

Moreover, the cured -matrix material typically maintains low Young’s s even at low temperatures. In exemplary embodiments, the cured ribbon-matrix material has Young’s modulus of 100 MPa or less at —40°C, such as 75 MPa or less at —40°C (e.g., 60 MPa or less at —40°C). Typically, the cured -matrix al has s modulus of 50 MPa or less at —40°C, such as 25 MPa or less at —40°C. In some ments of the optical-fiber ribbon, the cured ribbon-matrix material has s modulus of less than 15 MPa at —40°C (e.g, between 1 and 10 at —40°C). In notable, exemplary embodiments of the optical-fiber ribbon, the cured -matrix material maintains Young’s modulus of between 1 and 20 MPa over the temperature range of —40°C and 20°C.

Low-temperature Young’s modulus can be determined via dynamic mechanical is (DMA), also referred to as dynamic mechanical thermal analysis (DMTA), such as by using a TA 2980 Dynamic Mechanical Analyzer.

By way of contrast, folding or rolling a conventional optical-fiber ribbon having a high-modulus ribbon-matrix material tends to impart high, localized stresses to the constituent optical fibers, especially at low temperatures (between 0°C and —50°C). Such extreme ribbon deformation can cause not only increased l-fiber attenuation but also ace delamination, such as between the optical fiber’s glass and surrounding primary coating or between the optical fiber’s outer coating (e.g., a secondary coating or tertiary ink layer) and the surrounding ribbon-matrix material. On the other hand, if the modulus of the ribbon-matrix material is too low, the folding and rolling of the optical-fiber ribbon tends to be irreversible (e.g., the optical-fiber ribbon resists returning from a compact configuration to a planar configuration as is necessary to facilitate mass-fusion splicing operations).

In other exemplary embodiments of the optical—fiber ribbon, the cured ribbon-matrix material has Shore A hardness between 40 and 75, such as Shore A hardness n 50 and 70. Hardness (e.g., Shore A hardness) for -matrix materials can be determined via ISO 868:2003 (Determination of indentation hardness by means of a durometer (Shore hardness), which is hereby incorporated by reference in its entirety.

Suitable compositions for the ribbon-matrix material include low-modulus elastomers and silicones, such as able silicones and RTV silicones (i.e., room temperature—vulcanization silicone). The UV-cured silicones have some advantages over RTV silicones, including faster curing and reduced shrinkage. In addition, unlike UV-cured silicones, RTV silicones require exposure to humidity and high temperatures for ed time periods and can generate unwanted byproducts (e.g., acetic acid) during curing. Suitable UV-curable silicones include E® SI 5240““ UV-cured silicone and Addisil UV-cured silicones (e.g., UV 50 EX, UV 60 EX, and UV 7O EX). As will be appreciated by those having ordinary skill in the art, UV curing can be enhanced by modifying UV-lamp configurations, introducing more photoinitiator, introducing a different photoinitiator, making slight chemical modifications (e.g., hybrid silicone/acrylate systems), and/or employing supplemental thermal curing. For silicone acrylates, an exemplary photoinitiator is 2-hydroxymethyl-l- phenylpropane-l-one (HMPP) (e.g., Ciba ves’ DAROCUR® 1173). Other photoinitiators with similar photodecomposition mechanisms are TEGo® PC 750 or TEGO® A16.

Figure 5 depicts Young’s modulus as a function of temperature for various ribbon—matrix materials, including a suitable able silicone (i.e., LOCTITE® SI 524OTM UV-cured silicone) and conventional able tes (i.e., DSM 4 and DSM 9D9-518, respectively). Modulus was measured via c al analysis (DMA). >l< >l< >l< The flexible optical-fiber ribbon may be manufactured as a planar optical-fiber ribbon. In its substantially planar geometry, the optical-fiber ribbon is le for mass-fusion spicing. Unlike conventional optical-fiber ribbons, which will become damaged if forcibly folded or , the t flexible optical-fiber ribbon is capable of being reversibly folded or reversibly rolled into a compact configuration without sustaining damage. In its substantially non-planar, compact geometry, the optical-fiber ribbon may be more efficiently packed (e.g., folded or ) within optical-fiber cablings, such as a le micromodule or a buffer tube. In ary cabling embodiments, one, two, three, or four flexible optical-fiber ribbons (e.g., twelve-optical-fiber ribbons) may be positioned within a micromodule, such as Prysmian’s FLEXTUBE® micromodule.

Figure 6 depicts a flexible, de, edge-bonded twelve-optical-fiber ribbon 10 efficiently packed within a tearable FLEXTUBE® micromodule 20 having an approximately 1.2-millimeter inner diameter. Those having ry skill in the art will appreciate that the flexible l-fiber ribbon reverts to its planar geometry when unpacked from the micromodule, thereby facilitating mass-fusion spicing.

In its planar geometry, the optical-fiber ribbon defines a maximum ribbon cross-sectional width (Wmax) (e.g., a major transverse axis). The l-fiber ribbon is sufficiently flexible and durable to withstand — without ng the structure of the optical-fiber ribbon, including its constituent optical fibers — repeated transverse folding or rolling from its maximum ribbon cross-sectional width (Wmax) to a significantly reduced ribbon cross—sectional width (Wf) (i.e., Wmax >> Wf). In this regard, damage to the optical-fiber ribbon would include cracks or splits to the cured ribbon-matrix al, as well as delamination at the interface of the optical fibers and the cured ribbon-matrix material.

As noted, the ribbon-matrix material may be applied to only one side of the parallel optical fibers to partially fill the curved, triangular regions defined by adjacent optical fibers to achieve an exemplary one—side, edge-bonded optical-fiber ribbon. Figure 7 s such an exemplary de, edge-bonded optical-fiber ribbon in a planar ribbon configuration. Figure 8 depicts the same exemplary one-side, edge—bonded optical—fiber ribbon in a compact ribbon configuration after transverse folding about the length of the optical-fiber ribbon.

In one exemplary embodiment, the optical-fiber ribbon is reversibly, transversely foldable (or reversibly, transversely rollable) from a planar ribbon configuration defining a maximum ribbon cross-sectional width (Wmax) to a anar ribbon configuration defining a reduced ribbon cross-sectional width (Wf) that is 75 percent or less (e.g., 60 percent or less) of the maximum ribbon cross—sectional width (Wmax) without damaging the ure of the optical-fiber ribbon. er, the optical-fiber ribbon can withstand such reversible packing for at least three cycles (e.g., five cycles or more), typically for at least ten cycles (e.g., 20 cycles or more).

In r exemplary embodiment, the optical-fiber ribbon is reversibly, transversely foldable (or reversibly, transversely rollable) from a planar ribbon configuration defining a maximum ribbon cross-sectional width (Wmax) to a non—planar ribbon configuration defining a reduced ribbon sectional width (Wf) that is 50 percent or less (e.g., 40 percent or less) of the maximum ribbon cross-sectional width (Wmax) without damaging the ure of the optical-fiber ribbon. Moreover, the optical-fiber ribbon can withstand such reversible packing for at least three cycles (e.g., five cycles or more), typically for at least ten cycles (e.g., 20 cycles or more).

In yet another exemplary embodiment, the optical-fiber ribbon is ibly, transversely foldable (or reversibly, transversely rollable) from a planar ribbon configuration defining a maximum ribbon cross-sectional width (Wmax) to a non—planar ribbon configuration defining a reduced ribbon cross-sectional width (Wf) that is 35 percent or less (e.g., 25 percent or less) of the maximum ribbon cross-sectional width (Wmax) without damaging the structure of the optical—fiber ribbon. Moreover, the optical -fiber ribbon can withstand such reversible packing for at least three cycles (e.g., five cycles or more), typically for at least ten cycles (e.g., 20 cycles or more).

Those having ordinary skill in the art will ize compacting larger—count l-fiber ribbons (e.g., twelve-optical-fiber s, 24-optical-fiber ribbons, or 36-optical-fiber ribbons), such as depicted in Figure 8, is typically more efficient than compacting smaller-count optical-fiber ribbons (e.g., four-optical-fiber ribbons or six-optical-fiber ribbons).

Alternatively, similar flexibility and lity can be calculated using as the starting measurement a transverse major axis that is defined by the opposite, outermost optical fibers within the optical-fiber ribbon (e. g., the distance n the first and twelfth optical fibers in a lZ-fiber ribbon).

The t flexible optical-fiber ribbon may be manufactured to comply with the c requirements set forth in Telcordia Technologies GRCORE (Issue 4, July 2013), namely Section 5 (“Requirements for l Fiber Ribbons”), which itself references Publication No. ANSI/ICEA S640-2011 for ard for Optical Fiber Outside Plant ication Cable,” (Fifth Edition — 2011), such as section 7.14 (“Ribbon Dimensions”), CORE (Issue 4, July 2013) and Publication No. ANSI/ICEA S—87— 640-2011 (Fifth Edition, 2011), each of which is hereby incorporated by reference in its entirety, provide the following maximum dimensions for optical—fiber ribbons: Table l gMaximum Ribbon Dimensions) optical-fiber optical-fiber ribbon width (W) ribbon height (h) alignment alignment 0pt1calf1bers(n) (pm) (pm) extreme fibers (b) planarity (p) Accordingly, in an exemplary embodiment, the optical-fiber ribbon conforms to the ribbon-dimension requirements ed in Table 1 (above) as disclosed in both GRCORE (Issue 4, July 2013) and Publication No. ANSI/ICEA S640-2011 (Fifth n, 2011). Figure 9 depicts the dimensional ters presented in Table l.

Alternatively, optical-fiber planarity within an optical-fiber ribbon may be expressed as a function of optical-fiber width (i.e., optical—fiber er). For example, optical-fiber planarity can be defined as the normal distance between the extreme upper and lower optical fibers within the optical-fiber ribbon relative to a transverse ne defined by the opposite, outermost optical fibers within the optical-fiber ribbon (e.g., a baseline ting either the respective centers of the two outermost optical fibers or the corresponding glass cladding edges of the two outermost optical fibers). See Figure 9. After establishing an appropriate transverse baseline and identifying the uppermost and lowermost optical fibers in the optical-fiber ribbon, optical-fiber planarity can be determined as the sum of the perpendicular distance from the defined transverse baseline (1') to the respective centers of the glass cores of the uppermost and lowermost l fibers or (ii) to the corresponding glass cladding edges of the uppermost and lowermost optical fibers. Those having ordinary skill in the art will iate that, in determining optical-fiber planarity using glass cladding edges, the same corresponding position (e.g., six o’clock) must be selected for the opposite, outermost optical fibers within the optical-fiber ribbon (i.e., in establishing the ne) and for the respective glass cladding edges of the uppermost and lowermost l fibers (i.e., in determining normal distance to the baseline).

In exemplary embodiments of the optical-fiber ribbon, the normal distance between the e upper and lower optical fibers is less than 40 percent of the mean width of the optical fibers (i.e., optical-fiber diameter) within the optical—fiber ribbon. In other exemplary embodiments of the optical-fiber ribbon, the normal ce between the e upper and lower optical fibers is less than 30 percent (e.g., less than 20 percent, such as percent or less) of the mean width of the optical fibers within the optical-fiber ribbon.

This normalized l-fiber planarity should be measured from a transverse baseline defined by the te, outermost l fibers within the optical-fiber ribbon, namely from the respective centers of the optical fibers’ glass cores or from the tive, corresponding glass cladding edges of the optical fibers (e. g., the respective six-o’clock ons). This concept is discussed at Section 5 (“Requirements for Optical Fiber Ribbons”) in Telcordia Technologies GR—20-CORE (Issue 4, July 2013).

Similarly, optical-fiber spacing within an optical-fiber ribbon may be expressed as a function of optical—fiber width (i.e., l—fiber diameter), such as by mean separation between adjacent optical fibers (e.g., from the optical fibers’ tive outermost coating layers) within the l-fiber ribbon. In exemplary embodiments of the optical-fiber , the mean separation between adjacent optical fibers within the optical-fiber ribbon is less than 15 percent (e.g., less than 10 percent) of the mean width of the optical fibers (i.e., optical—fiber diameter) within the optical-fiber ribbon. In exemplary embodiments of the optical-fiber ribbon, the mean separation between adjacent optical fibers within the optical-fiber ribbon is less than 5 percent of the mean width of the optical fibers within the l-fiber ribbon, such as where nt optical fibers are substantially contigmous to one another within the optical-fiber ribbon.

By way of contrast, some conventional optical-fiber ribbons achieve flexibility via intermittent bonding with a high-modulus ribbon-matrix material (e. g., 300 MPa), such as disclosed in US. Patent No. 9,086,555, which is hereby incorporated by reference in its entirety. The l fibers within such intermittently bonded l-fiber ribbons, such as a “spider web ribbon,” can freely move when not clamped or otherwise secured. Whether the optical fibers are clamped or not, intermittently bonded optical-fiber ribbons employ complex bonding patterns and typically fail to satisfy the spacing and planarity requirements disclosed in both GR-ZO-CORE (Issue 4, July 2013) and Publication No. ANSI/ICEA S-87—640-2011 (Fifth Edition, 2011). This renders conventional, intermittently bonded optical-fiber ribbons (e.g., “spider web ribbon”) poor candidates for mass-fusion splicing.

It is desirable to increase the density of optical-fiber ribbons in buffer tubes or cables, subject to other constraints (e. g., cable or mid-span attenuation). In this regard, the l fibers themselves may be designed for increased packing density. For example, the optical fiber may possess modified properties, such as ed refractive—index profile, core or cladding dimensions, or primary-coating thickness and/or modulus, to improve microbending and macrobending characteristics.

In one embodiment, the optical fibers employed in the t optical-fiber ribbons may be conventional standard single-mode fibers (S SMF). Suitable single-mode optical fibers (e.g., enhanced single—mode fibers (ESMF)) that are compliant with the ITU-T G.652.D recommendations are commercially available, for instance, from an Group (Claremont, North na, USA). The ITU-T G652 (November 2009) endations and each of its attributes (i.e., A, B, C, and D) are hereby orated by reference in their entirety.

In r embodiment, bend-insensitive —mode optical fibers may be employed in the optical-fiber ribbons according to the present invention. Bend-insensitive optical fibers are less tible to attenuation (e.g., caused by microbending or macrobending). Exemplary single-mode glass fibers for use in the present optical-fiber ribbons are commercially available from Prysmian Group (Claremont, North Carolina, USA) under the trade name BendBright®, which is compliant with the ITU-T G.652.D recommendations. That said, it is within the scope of the present invention to employ a bend—insensitive glass fiber that meets the ITU-T G.657.A recommendations (e.g., the ITU-T G.657.Al (November 2009) and the ITU-T G.657.A2 (November 2009) egories) and/or the ITU-T G.657‘B recommendations (eg., the ITU-T G.657.B2 (November 2009) and the ITU-T G.657.B3 (November 2009) subcategories). In this regard, the ITU-T G.657.A1 (November 2009) subcategory fully encompasses the former ITU—T G657.A (December 2006) category, and the ITU-T G.657.B2 (November 2009) subcategory fully encompasses the former ITU-T G.657.B (December 2006) category. The ITU—T G.657.A/B recommendations are hereby orated by reference in their entirety.

In this regard, exemplary bend-insensitive -mode glass fibers for use in the present invention are commercially available from an Group mont, North Carolina, USA) under the trade names BendBrightXS® and BendBright-EliteTM.

BendBrightXS® optical fibers and BendBright-EliteTM optical fibers are not only compliant 2016/044182 with both the ITU-T G.652.D and ITU-T G.657.A/B recommendations, but also demonstrate significant improvement with respect to both ending and microbending. As compared with such bend-insensitive single-mode optical fibers, conventional single-mode optical fibers typically do not comply with either the ITU-T G.657.A recommendations or the ITU-T B recommendations, but do typically comply with the ITU-T G.652 recommendations (e. g, the ITU-T G.652.D recommendations).

As set forth in commonly assigned US. Patent No. 8,265,442, US. Patent No. 8,145,027, US. Patent No. 8,385,705, and International Patent Application Publication No. A1, pairing a bend-insensitive glass fiber (e.g., Prysmian Group’s single-mode glass fibers available under the trade name BendBrightXS®) and a primary coating having very low modulus achieves optical fibers having exceptionally low losses (e. g., reductions in end ivity of at least 10X as compared with a single—mode optical fiber employing a conventional coating system). The optical-fiber ribbons according to the present invention may employ the optical-fiber coatings disclosed in US. Patent No. 8,265,442, US. Patent No. 8,145,027, US. Patent No. 8,3 85,705, and International Patent Application Publication No. A1, which are hereby incorporated by reference in their entirety, with either single-mode optical fibers or multimode l fibers.

In another embodiment, the l fibers employed in the present optical-fiber ribbons are conventional multimode l fibers having a 50-micron core (e.g, 0M2 multimode optical fibers) and complying with the ITU-T G.651.1 recommendations. The ITU—T G.651.1 (July 2007) recommendations are hereby orated by reference in their entirety. Exemplary multimode optical fibers that may be employed include MaxCapTM multimode optical fibers (OM2+, 0M3, or 0M4), which are commercially available from Prysmian Group (Claremont, North Carolina, USA).

Alternatively, the present l-fiber s may e bend-insensitive multimode optical fibers, such as MaXCapTM-BB—OMX multimode optical fibers, which are commercially available from Prysmian Group (Claremont, North Carolina, USA). In this regard, bend-insensitive multimode optical fibers typically have macrobending losses of (i) no more than 0.1 dB at a wavelength of 850 nanometers for a g of two turns around a spool with a bending radius of 15 millimeters and (it) no more than 0.3 dB at a wavelength of 1300 nanometers for a winding of two turns around a spool with a bending radius of millimeters.

In contrast, conventional multimode optical fibers, in accordance with the ITU-T G.651.1 recommendations, have macrobending losses of (i) no more than 1 dB at a wavelength of 850 nanometers for a g of two turns around a spool with a bending radius of 15 millimeters and (ii) no more than 1 dB at a ngth of 1300 nanometers for a winding of two turns around a spool with a bending radius of 15 millimeters. Moreover, as measured using a winding of two turns around a spool with a bending radius of millimeters, conventional multimode optical fibers typically have macrobending losses of (i) greater than 0.1 dB, more typically greater than 0.2 dB (e.g., 0.3 dB or more), at a wavelength of 850 nanometers and (ii) greater than 0.3 dB, more typically greater than 0.4 dB (e.g., 0.5 dB or more), at a wavelength of 1300 nanometers.

Multimode optical fibers can be advantageous, because their relatively large core diameter facilitates easy torization. Accordingly, it is within the scope of the present invention to employ multimode optical fibers having enlarged core diameters (e.g., 62.5 microns or greater), such as n about 70 microns and 100 s (e.g., about 80 microns). An exemplary multimode l fiber having an enlarged core diameter is disclosed in commonly assigned US. Patent No. 771 for a Bend-Resistant Multimode Optical Fiber, (Molin et al.), which is hereby incorporated by reference in its entirety. In particular, US. Patent No. 771 discloses a trench-assisted multimode l fiber having ed bend resistance.

The optical fibers typically have an outer diameter of between about 235 microns and 265 microns, although optical fibers having a smaller diameter may be employed in the present optical-fiber ribbons.

By way of example, the component glass fiber may have an outer diameter of about 125 microns. With respect to the optical fiber’s surrounding coating layers, the y coating may have an outer diameter of between about 175 microns and 195 microns (i.e., a primary coating thickness of between about 25 microns and 35 microns), and the secondary coating may have an outer diameter of between about 235 microns and 265 microns (i.e., a secondary coating thickness of between about 20 microns and 45 microns).

Optionally, the optical fiber may include an outermost ink layer, which is typically between two and ten microns.

In one alternative embodiment, an optical fiber may possess a reduced diameter (e.g., an outermost er between about 150 microns and 230 microns). In this ative optical fiber ration, the thickness of the primary coating and/or secondary coating is reduced, while the diameter of the component glass fiber is maintained at about 125 microns.

(Those having ordinary skill in the art will appreciate that, unless otherwise specified, er measurements refer to outer diameters.) By way of illustration, in such exemplary embodiments, the primary coating layer may have an outer diameter of between about 135 microns and about 175 microns (e. g., about 160 microns), typically less than 165 s (e.g., between about 135 microns and 150 microns), and usually more than 140 microns (e.g., between about 145 microns and 155 microns, such as about 150 s).

Moreover, in such exemplary embodiments, the secondary coating layer may have an outer diameter of between about 150 microns and about 230 microns (e.g., more than about 165 microns, such as 190—210 microns or so), typically between about 180 microns and 200 microns. In other words, the total diameter of the optical fiber is reduced to less than about 230 microns (e.g., between about 195 microns and 205 microns, and especially about 200 microns). By way of further ration, an optical fiber may employ a ary coating of about 197 microns at a tolerance of +/- 5 microns (i.e., a secondary-coating outer diameter of between 192 microns to 202 microns). Typically, the secondary coating will retain a thickness of at least about 10 microns (e.g., an optical fiber having a reduced thickness secondary coating of between 15 s and 25 microns).

In another alternative embodiment, the outer er of the ent glass fiber may be reduced to less than 125 microns (e.g., between about 60 microns and 120 microns), perhaps between about 70 microns and 115 microns (e. g., about 80—1 10 microns). This may be achieved, for instance, by ng the thickness of one or more cladding . As compared with the prior alternative embodiment, (1') the total diameter of the optical fiber may be reduced (i.e., the thickness of the primary and secondary coatings are maintained in accordance with the prior alternative ment) or (ii) the respective esses of the y and/or secondary coatings may be increased relative to the prior alternative embodiment (e.g., such that the total diameter of the optical fiber might be maintained).

By way of illustration, with respect to the former, a component glass fiber having a er of between about 90 and 100 microns might be combined with a y coating layer having an outer diameter of between about 110 microns and 150 microns (e.g., about 125 microns) and a secondary coating layer having an outer diameter of between about 130 microns and 190 microns (e. g., about 155 microns). With respect to the latter, a component glass fiber having a diameter of between about 90 and 100 microns might be combined with a primary g layer having an outer diameter of between about 120 microns and 140 s (e.g., about 130 microns) and a secondary coating layer having an outer er of between about 160 microns and 230 microns (e. g., about 195-200 microns).

Reducing the diameter of the component glass fiber might make the resulting optical fiber more susceptible to microbending attenuation. That said, the advantages of further reducing optical-fiber diameter might be worthwhile for some optical-fiber applications.

As noted, the present optical fibers may e one or more coating layers (e.g., a primary coating and a secondary coating). At least one of the coating layers — typically the secondary coating — may be colored and/or possess other markings to help identify individual fibers. Alternatively, a tertiary ink layer may surround the primary and secondary coatings.

In the cation and/or figures, typical embodiments of the invention have been disclosed. The present invention is not limited to such exemplary embodiments. The use of the term “and/or” includes any and all combinations of one or more of the associated listed items. The figures are schematic representations and so are not necessarily drawn to scale. Unless otherwise noted, specific terms have been used in a generic and descriptive sense and not for es of limitation.

Claims (14)

1. An optical-fiber ribbon, comprising: a ity of optical fibers; and a cured ribbon-matIiX material edge bonding the plurality of optical fibers in a side-by-side ement such that at least 70 percent of the cured ribbon-matrix material is oned on one side of the optical—fiber ribbon, the cured ribbon—matrix material having (1') elongation-to-break of at least 200 percent at 20°C, (ii) Young's modulus of 1—20 MPa at 20°C, and (iii) Young's s of 100 MPa or less at —40°C‘

2. The optical-fiber ribbon according to Claim 1, wherein the cured ribbon-matrix material has elongation-to-break of at least 300 percent at 20°C.

3. The optical-fiber ribbon according to either Claim 1 or Claim 2, wherein the cured ribbon-matrix material has s modulus of 75 MPa or less at —40°C.

4. An optical-fiber ribbon, sing: a plurality of optical fibers; and a cured ribbon—matrix material bonding the plurality of optical fibers in a side-by-side arrangement, the cured ribbon-matrix material having (1') elongation-to-break of at least 350 percent at 20°C, (ii) Young's modulus of 1—15 MPa at 20°C, and (iii) Young’s modulus of 60 MPa or less at —40°C; wherein the optical-fiber ribbon is reversibly, transversely foldable from a planar ribbon configuration defining a m ribbon cross-sectional width (Wmax) to a non-planar ribbon configuration defining a reduced ribbon sectional width (Wf) that is 75 percent or less of the maximum ribbon cross-sectional width (Wmax) without damaging the structure of the optical-fiber ribbon.

5. The optical-fiber ribbon according to any one of the prior claims, wherein the cured ribbon-matrix material edge bonds the plurality of optical fibers in a side-by-side arrangement such that at least 75 percent of the cured -matrix material is positioned on one side of the optical-fiber ribbon.

6. The optical-fiber ribbon ing to any one of the prior claims, wherein the cured ribbon-matrix material edge bonds the plurality of optical fibers in a y-side ement such that at least 80 percent of the cured ribbon-matrix material is oned on one side of the optical-fiber ribbon.

7. The optical-fiber ribbon ing to any one of the prior claims, wherein the cured -matrix material edge bonds the plurality of optical fibers in a side-by-side arrangement such that at least 90 percent of the cured ribbon-matrix material is positioned on one side of the optical-fiber ribbon.

8. The optical-fiber ribbon according to any one of the prior claims, wherein the cured ribbon-matrix al bonds the plurality of optical fibers in a side-by-side arrangement via the application of ribbon-matrix material predominantly to only one side of the optical-fiber ribbon to at least partly fill the curved, triangular regions defined by adjacent optical fibers.

9. The optical-fiber ribbon according to any one of the prior claims, wherein the optical-fiber ribbon is reversibly, transversely foldable from a planar ribbon configuration defining a maximum ribbon cross-sectional width (Wmax) to a non—planar ribbon configuration defining a reduced ribbon cross-sectional width (Wf) that is 60 percent or less of the maximum ribbon cross-sectional width (Wmax) without damaging the structure of the optical-fiber ribbon.

10. The optical-fiber ribbon according to any one of the prior , wherein the optical-fiber ribbon is reversibly, transversely foldable from a planar ribbon configuration defining a maximum ribbon cross-sectional width (Wmax) to a non—planar ribbon configuration defining a reduced ribbon cross-sectional width (Wf) that is 50 percent or less of the maximum ribbon cross-sectional width (Wmax) without damaging the structure of the optical-fiber ribbon.

11. The optical-fiber ribbon according to any one of the prior claims, wherein the optical-fiber ribbon is reversibly, transversely le from a planar ribbon configuration defining a maximum ribbon cross-sectional width (Wmax) to a non—planar ribbon configuration g a reduced ribbon cross-sectional width (Wf) that is 35 percent or less of the m ribbon cross-sectional width (Wmax) without damaging the structure of the optical-fiber ribbon.

12. The l-fiber ribbon according to any one of Claims 9—1 1, wherein, for at least five folding cycles, the optical-fiber ribbon is reversibly, ersely foldable from the planar ribbon ration defining the maximum ribbon sectional width (Wmax) to a non-planar ribbon configuration defining the reduced ribbon cross—sectional width (Wf) without damaging the structure of the optical-fiber .

13. The optical-fiber ribbon according to any one of Claims 9—11, wherein, for at least ten folding cycles, the optical-fiber ribbon is reversibly, transversely foldable from the planar ribbon configuration defining the maximum ribbon cross-sectional width (Wmax) to a non-planar ribbon configuration g the reduced ribbon cross-sectional width (Wf) without damaging the structure of the optical-fiber ribbon.

14. The optical-fiber ribbon according to any one of Claims 9—11, wherein, for at least twenty g cycles, the optical-fiber ribbon is ibly, transversely foldable from the planar ribbon configuration defining the maximum ribbon cross-sectional width (Wmax) to a non-planar ribbon configuration defining the reduced ribbon cross-sectional width (Wf) without damaging the structure of the optical-fiber ribbon.