EP3931380A1

EP3931380A1 - Micro/nano-layered filaments

Info

Publication number: EP3931380A1
Application number: EP20711324.2A
Authority: EP
Inventors: Kristy A. Jost; James M. Jonza; Brian L. Koster; William J. Kopecky; Jack KOCH; Ignatius A. Kadoma
Original assignee: 3M Innovative Properties Co
Current assignee: 3M Innovative Properties Co
Priority date: 2019-02-28
Filing date: 2020-02-27
Publication date: 2022-01-05
Also published as: CN113490773A; US20220136138A1; WO2020174438A1; CN113490773B

Abstract

The present invention is a process for converting a multilayer filament to a plurality of nano-ribbons. The process includes co-extruding a first layer and a second layer to form the multilayer filament, and separating the multilayer filaments to form a plurality of nano-ribbons having substantially flat cross-sections.

Description

MICRO/NANO-LAYERED FILAMENTS

Field of the Invention

The present invention relates generally to the field of nano-ribbons. In particular, the present invention relates to a nano-ribbon produced from a multilayer filament.

Background

Strong, light, and inexpensive materials are often sought after for their unique properties. For example, such materials have a high surface area and a low weight-to- strength ratio useful in light- weighting transportation, filtration, insulation, and apparel. In particular, nano-fibers (< 500 nm diameter) have unique characteristics compared to micro-fibers, such as higher surface area and extremely high porosity in non-woven fabrics. Their applications range from uses in batteries as porous membrane separators to biomedical applications as cellular scaffolds to high surface area filters. Current nano-fiber fabrication methods include electrospinning, centrifugal spinning, and melt-blowing. Although there are many benefits of nano-fibers, a key barrier in the wide-scale adoption of the material is their significantly higher cost compared to microfibrous meltblown media, which are produced an order of magnitude faster.

One of the challenges to electrospun and meltblown nano-fibers is that they have very little orientation and are thus typically weaker than a drawn/oriented fiber from traditional fiber processing. The strongest fully oriented filament microfibers currently found in the industry are spun and drawn from the extruder (for example, at about 7000 m/min) and are typically also post-drawn to further increase the orientation. These fibers are used in applications such as ropes, tent fabrics, boating sails, architectural textiles, and other industrial textiles that require high tensile strength.

Currently, electrospinning and melt blowing processes do not easily allow for nano-fibers to be length oriented to the degree of melt spun filament fibers, nor can yams and subsequently knitted/woven textiles be easily produced from the fibers made by these methods. Summary

In one embodiment, the present invention is a process for converting a multilayer filament to a plurality of nano-ribbons. The process includes co-extruding a first layer and a second layer to form the multilayer filament, and separating the multilayer filaments to form a plurality of nano-ribbons having substantially flat cross-sections.

In another embodiment, the present invention is a nano-ribbon yarn including ribbons having a thickness of between about 10 nanometers and about 10 microns, wherein the ribbons have a substantially flat cross-section.

Brief Description of the Drawings

FIG. 1A is cross-sectional view of an embodiment of a multilayer filament of the present invention.

FIG. 1B is a cross-sectional view of an embodiment of nano-ribbons produced by the method of the present invention.

FIG. 2 is a diagram of a method of producing the nano-ribbons of the present invention.

FIG. 3 A is a surface view of nano-ribbons of the present invention produced by delaminating multilayered filaments using compressed air.

FIGS. 3B is a surface view of nano-ribbons of the present invention produced by delaminating multilayered filaments using ultrasonication.

FIG. 4 is side perspective view of an embodiment of the nano-ribbons of the present invention having varying thicknesses along the length.

FIG. 5 is a perspective view of an embodiment of the nano-ribbons of the present invention having a porous structure.

FIG. 6 is a perspective view of an embodiment of the nano-ribbons of the present invention having blends of two resins.

Fig 7A shows a micrograph of a first polymer and a second polymer with layers having a major and minor phase.

Fig. 7B shows an enlarged, cross-sectional illustration of the matrix of FIG. 7A.

While the above-identified drawings and figures set forth embodiments of the invention, other embodiments are also contemplated, as noted in the discussion. In all cases, this disclosure presents the invention by way of representation and not limitation. It should be understood that numerous other modifications and embodiments can be devised by those skilled in the art, which fall within the scope and spirit of this invention. The figures may not be drawn to scale.

Detailed Description

The present invention is a nano-ribbon and a method of producing the nano-ribbon. In one embodiment, the nano-ribbons are highly oriented and have increased tensile strength and can be produced as bundles of ribbons or fibers (i.e., yarns), that can be woven or knitted into various textiles. Due to their increased tensile strength, the nano- ribbons can be used in a vast range of applications in addition to nonwovens. The layer thicknesses are also controllable with a narrow distribution. In addition, the resulting nano-ribbons can also be chopped and formed into a nonwoven fabric. The resulting nano- ribbons can provide a thin, yet warm material. Without being bound by theory, it is believed that the nano-ribbons provide warmth due to their inducement of the Knudsen Effect. Once pore sizes approach the size of the mean free path of air (73nm), air molecules collide with the matrix (nanofibers) more often, losing energy with each collision, making heat transfer slower, and resulting in much better insulation. Thus, less material is needed to provide a greater deal of warmth.

FIG. 1A shows a cross-sectional view of an embodiment of a multilayer filament 10 that is converted into the nano-ribbons 12 (FIG. 1B) of the present invention. The multilayer filaments 10 used to create the nano-ribbons include alternating layers of melt extrudable polymers or resin materials 14 and 16 that are immiscible with each other. The alternating layers of extrudable polymers or resins 14 and 16 have substantially no chemical affinity for each other but are still able to be extruded into a layered structure with each other. In one embodiment, the polymers may be length oriented at the same drawing temperatures, ratios and rates. The multilayer filaments 10 include at least two different melt extrudable polymers or resin materials, as depicted in FIG. 1A, but may include more than two alternating layers without departing from the intended scope of the present invention.

The alternating polymer or resin layers, or polymer or resin pairs 14 and 16, may include, but are not limited to: polyethylene terephthalate (PET) and polypropylene (PP), nylon 6 or 6,6 and PP, thermoplastic polyurethane (TPU) and PP, styrenic block copolymers (e.g, styrene-ethylene/butylene-styrene (SEBS)) and PP, transparent polymer (TPX) such as polymethylpentene (PMP) and PET, TPX and PP, PP and PE, PP and polybutylene terephthalate (PBT), polylactic acid (PLA) and PP, polybutylene succinate (PBS) and PP, PLA and dimer acid based (DAB) polyamide, polyhydroxyalkanoates (PHA) and PP, PHA and DAB polyamide, polyhydroxybutyrate (PHB) and PP, PHB and DAB polyamide, and hydrophobic/hydrophilic versions of the same polymer. Two particularly suitable polymer or resin pairs are PET and PP, and PLA and PP. If needed, in one embodiment, additives can be added to the base polymers that cause the alternating polymers to further reduce the chemical affinity to each other.

Each of the multilayer filaments 10 must include at least two layers. However, the multilayer filaments 10 can include any number of layers without departing from the intended scope of the present invention. In one embodiment, the multilayer filaments include up to about 1000 layers. In one embodiment, each of the layers of the multilayer filaments has a thickness of between about 1 and about 500 nm, particularly between about 50 and about 250 nm, and more particularly between about 50 and about 150 nm.

FIG. 2 generally shows a method 18 of producing the nano-ribbons of the present invention. In a first step of producing the nano-ribbons of the present invention, the first polymer or resin material 14 passes through a first extruder 20 and the second, incompatible polymer or resin material 16 passes through a second extruder 22 into a multilayer feedblock 24. In one embodiment, the multilayer feedblock 24 is about 250 layers. In one embodiment, the process includes using a fiber faceplate 26 (i.e., a spin pack) with small holes aligned in a single row perpendicular to the flow of the molten multi-layer stack coming from the feedblock 24. The number of layers can be further increased with the use of a multiplier 28. In one embodiment, the multiplier 28 increases the number of layers from about 250 to about 500. The rheology of the polymer or resin materials of the multilayer filament is an important consideration. Generally, the melt viscosities of the two resins at the temperature and shear rates of interest are within an order of magnitude or better to avoid flow instabilities (coextrusion defects). In one embodiment, the feedblock/fiber faceplate produces 31 to 32 nanolayered filaments 10, each containing about 250 or about 400 layers with at least about 70% of the filaments having excellent layering. The layers can either be the same size or of different sizes. Because the multilayer ribbons are formed from substantially flat layers of the extruded multilayer filaments, the resulting individual multilayered ribbons are substantially flat or ribbon-like, rather than having a cylindrical cross-section.

Once extruded, the multilayer filaments 10 may optionally be cooled in a water bath 30. The multilayer filaments 10 can also be length oriented to be drawn thinner. Orientation simply means that the long chains of polymers are oriented lengthwise in the same direction and can also impart higher crystallinity in the polymer. This improves the overall tensile strength of the material along the length because any force applied along the length is supported by the carbon backbone of the polymer, rather than the intertwining and entangling of the polymers chains.

In one embodiment, the multilayer filaments 10 are stretched to a maximum of fifteen times their original length. In one embodiment, the multilayered filaments are length oriented at a ratio of about 15: 1, particularly about 10: 1, and more particularly about 6: 1. The multilayer filaments can be length oriented by any method known to those of skill in the art. In one embodiment, orientation is achieved using a draw stand 32 which heats and stretches the continuous filament fibers across a series of godet rollers and winds them into a cone. This process also decreases the thickness of the multilayer filaments, and therefore the individual layers. Generally, the higher the feed rate of the resin, the thicker the resulting layers. If desired, the speeds can be adjusted in line to produce a first region having a specified degree of orientation, and a second region having a different degree of orientation. In one embodiment, the multilayer filaments are length oriented at a temperature of between about 60°C and about 290°C, and particularly at about 100 °C. Temperature is typically set at or above the glass transition temperature (Tg) of the polymers to make the material malleable enough to be stretched (i.e., length oriented).

The faster the multilayer filaments are being oriented, the higher the temperature can be increased in order to have sufficient heat transfer. For example, 290°C is higher than the melt temperature (Tm) of PET, but if running at 1000 m/min, the PET is not in contact with the rollers long enough to melt. In one embodiment, the multilayer filaments are being length oriented at a maximum speed of 100 m/min heated to 100°C. Once length oriented, the multilayer filaments 10 may pass through a pneumatic texturizer 34 and wound onto a bobbin 36.

The layers of the multilayer filaments 10 need to be physically separated, or delaminated, from each other to form single nano-ribbons. Because the alternating layers 14 and 16 of the multilayer film 10 are immiscible with each other and have very little chemical affinity for each other, the layers can be easily separated from each other. The incompatible layers allow for the materials to be coextruded together but to also easily come apart from each other once solidified and agitated. Upon delamination, there is a clear single layer separation for most layers, which are the continuous filament nano- ribbons. The multilayer filaments 10 are separated without the use of any sacrificial polymers that are dissolved away. In one embodiment, the multilayer filaments are separated by mechanical or chemical methods. An example of a suitable method for chemically separating the layers includes, but is not limited to, treating with a polar solvent.

Examples of suitable methods of mechanical separation include, but are not limited to: compressed air (i.e., pneumatic texturizer), high pressure water (hydroentanglement), sonication, and ultrasoni cation. It should be noted that it is the velocity and/or the kinetic energy of the fluid (gas, air, liquid, water, etc.) and not necessarily the set pressure on the separation device that causes the separation to occur. It should be noted that it may be preferred to delaminate the layers in a separate process and not in-line with the fiber making. FIGS. 3A and 3B show surface views of nano-ribbons that have been produced using compressed air and ultrasoni cation, respectively. As can be seen in FIGS. 3A and 3B, the different methods of separation yield differing nano-ribbons. The compressed air (FIG. 3A) appears to keep the entire nano-ribbon 12a layer intact and merely separates them, while the ultrasonication (FIG. 3B) appears to further fibrillate the layers along the width, making even finer nano-ribbons 12b and increasing the number of differently size fibers. It appears that the ultrasonication also primarily penetrates only the surface of the mulitlayered filaments, while the compressed air mostly delaminated the entire structure.

Upon orientation, the polymer chains are aligned, increasing crystallinity and density. The reduction in volume may contribute to a reduction in adhesion between the layers or between fibers within layers.

The nano-ribbons 12 produced by separating the multilayered filaments 10 have one or more layers. In the majority of the volume, each layer within the multilayer filament 10 is separated into single sheets comprising one resin. In other embodiments, particularly at extremely small scales < 500 nm, Van der Waals forces can become strong enough that some layers may remain together in groups of two or more. The nano-ribbons 12 can be designed to be composed of more than one layer, such as three layers, where the outermost layers are composed of polymers or resins that will separate from each other, but not from the innermost layers. These multilayer nano-ribbons can be designed to be functionally layered to perform other functions, such as having shape memory properties, wicking, charged filtration, or many others where a function can be derived using more than one layered resin and may or may not have different additives in each layer.

The individual nano-ribbons 12 are a thin, flexible material having a much longer length than width, with sufficient strength and length, and/or fiber-fiber friction when bundled in a yam, to be used in a textile. Each of the nano-ribbon layers have a continuous or cut length. The nano-ribbon width is dependent on the width of the multilayered filament, which can be as wide as about 200 mm. The thickness of the resulting nano-ribbons produced using the method of the present invention can be between about 1 and about 1000 nm, particularly between about 1 nm and about 500 nm, and more particularly between about 50 nm and about 150 nm. The layer thickness of the resulting nano-ribbons is determined by a number of factors including, but not limited to: the number of extruded layers, the total filament thickness, the density of the polymers or resins used, and the length orientation. Generally, the denser the resin, the thinner the resulting layers.

In one embodiment, the nano-ribbons have a thickness of between about 1 and about 500 nm and a width of between about 1 and about 200 mm.

The resulting nano-ribbons produced using the above method are highly fibrous with a look and feel similar to yarn and have high tensile strength and high surface area. The high tensile strength of the nano-ribbons is due to the length orientation step of the process of the present invention. In one embodiment, the nano-ribbons have a tensile strength of about between about 150 and about 480 MPa, particularly between about 360 and about 390 MPa, and more particularly between about 440 and about 480 MPa. In practice, because the nano-ribbons produced by the method of the present invention have a high surface area, they can stick easily to metal and other surfaces due to Van der Waals forces and static electricity. Thus, in one embodiment, a lubricant, such as a silicone lubricant, can be coated onto the nano-ribbons for smoother processing.

In one embodiment, the nano-ribbons can be designed to have a first region 38 with a first thickness and a second region 40 with a second, different thickness. FIG. 4 shows an embodiment of a nano-ribbon 12c having varying thicknesses along the length of the nano-ribbon. The varying thicknesses can be accomplished by drawing the multilayer filament at intermittent speeds. One benefit of nano-ribbons having varying thicknesses is the creation of controlled non-uniformity, potentially to keep the substantially flat fibers from collapsing on each other, as is commonly seen in electrospun fibers. The nano- ribbons of each polymer type can also have different thicknesses which can be

accomplished by varying the polymer type or the throughput of each polymer type from the extruders. For example, polypropylene can be run two times faster than polyester to obtain polypropylene layers that are thicker than the polyester layers.

In one embodiment, the nano-ribbons have a porous structure, as shown in FIG. 5. By including pores 42 in the nano-ribbons 12d, the surface area of the nano-ribbons increases. According to the Knudsen effect, as pore size decreases, the thermal resistance increases exponentially. Thus, the size of the pores within the entire volume of the nano- ribbon or nano-ribbon yarn will affect the overall warmth that the nano-ribbon provides, which can be advantageous when used to produce a textile. The pores can be created using any method known to those of skill in the art. In one embodiment, the pores can be created using resins that are blended with the matrix resin that are then removed, either by heat, solubilized in water or solvent. In another embodiment, materials such as fluids and particles which expand, foam, or decompose can be used during the extrusion process to create the pores. Microvoids may also be induced by the extrusion and drawing conditions, in some cases promoted by solid particles that cannot get longer during the orientation.

FIG. 6 shows yet another embodiment of the nano-ribbons 12e of the present invention, in which blends of two resins, a matrix 44 and a less dominant resin 46, are mixed in the extruders to create distinct regions of each resin. These layers are not only separated from each other, but the distinct regions of resin within the layers are also separated from each other to form even smaller, irregularly shaped nano-ribbons. To further aid in the separation of these even smaller segments of nano-ribbons, small amounts of a third material may be added. Block copolymers with both the A and B resins or other compatibilizers are known to those skilled in the art. Polystyrene (PS), (i.e., 5 wt.% of the total) has been shown to reduce the phase size of PP in a PET matrix. Similar effects are expected to be found with other pairs. FIGS. 7A and 7B depict an idealized case where the rheological match of polymers and the compatibilization are both excellent. FIG. 7A shows a micrograph with layers having a major phase 48 and minor phase 50. Long thin fibrils of the minor phase 50 are found in the major phase 48. After length orientation and delamination, the lateral dimensions of the minor phase 50 are small by the blending and flow, and the lateral dimensions of the major phase 48 can be small by cracking down the length of the fibers around and between the minor phase 50 fibrils. FIG. 7B depicts an illustration of the matrix of the major phase 48 breaking apart and fibrillating into smaller sections while allowing the fibrils of the minor phase 50 to be released.

The nano-ribbons produced by the method of the present invention can be formed into a yarn, which can then be formed into a textile, or a thin flexible sheet of material with sufficient strength and tear resistance (even when wet) to be used for clothing, interior fabrics, and other functional, protective or aesthetic applications. As used herein, “yarn” is defined as a thin material having a much longer length than width and is formed from many fibers to provide sufficient mechanical strength and flexibility to be converted to a textile (e.g., knit, woven, crochet etc.). Knitted, woven, crocheted, carpeted, and stitched textiles are made by looping and intertwining yarns together into sheets. The nano-ribbons can be used in any number of fields. For example, they can be used as thermal insulation, as a filtration medium, as a highly absorptive material, as a dusting and cleaning material, or as a scaffold for growing cells of plant, animal, human, bacteria.

It is important to note, in one embodiment, when the multilayered filament is mechanically separated with compressed air, the material is not blown apart into disparate pieces that need to be recombined to form a yarn. Rather, since the layers are continuous along the length of the multilayer filament, each layer could be described as a continuous filament nanofiber, they are just adhered and stacked together in a larger filament (the multilayer filament). The mechanical agitation causes the layers to become individually separate exposing their surface area, but are still intertwined together. Therefore, a single filament can become as many as 1000 nanofilaments. The separated nano-ribbons are still held together in a strand that is soft to the touch and yam-like instead. It is also important to note that to those skilled in the art, one could also chop the strand of yam into staple nano-ribbons and convert it to a calendared nonwoven web. Staple fibers are defined as short fibers typically 3 inches or less in length. Because the method of producing the nano-ribbon is a high throughput manufacturing process, is solvent free, and does not need to use a sacrificial polymer to separate nanofibers from bulk, it is an economical method for producing ultrafme nano ribbons or nano-fibers (<100 nm), particularly compared to electrospinning, melt blowing, and islands in the sea, which are inhibited by at least one of the above.

EXAMPLES

The present invention is more particularly described in the following examples that are intended as illustrations only, since numerous modifications and variations within the scope of the present invention will be apparent to those skilled in the art. Unless otherwise noted, all parts, percentages, and ratios reported in the following examples are on a weight basis.

Example 1

A multilayer stack having 500 alternating layers of PET and PP was extruded using a 250 layer feedblock, one multiplier, and a fiber faceplate having 2 rows of 16 holes. The PET grade used was 7352 supplied by Eastman Chemical Company (Kingsport, TN), and the PP grade was 1024 supplied by Exxon Mobil Corporation (Irving, TX). Two extruders were used, a first extruder for the PET layers, a second for the PP layers. The first extruder was set to 279°C with a first necktube set to 279°C, the second extruder was set to 279°C with a second necktube set to 279°C. The necktubes connected and directed the resin from the extruders to the feedblock and die. The feedblock and die were set at 279°C. The first extruder was a single screw with a barrel diameter of 32 mm and was operated at 50 rotations per minute (rpm), the second extruder was a single screw with a barrel width of 32 mm and was operated at 16.5 rpm. The multilayer filaments were passed through a chilled water bath and further directed to a level winder, Model 96B supplied by Leesona (Burlington, NC) and collected on a cone. The take up winder was set to 30, 43, and 49 m/min. The final multilayer filaments contained 375 - 398 layers. One embodiment containing a 398 layer stack was 841 mm by 300 mm and continuous in length. The individual layers were each measured to be 2.11 mm in thickness prior to any post drawing. The multilayer filaments were then length oriented on a draw stand supplied by Retech Aktiengesellschaft (Meisterschwanden, Switzerland) with 10cm wide godet rolls heated to 90°C. The fastest roll was set to 4x the speed of the slowest roll. The resulting multilayer filaments had cross-sections that were 332 mm by 115 mm and continuous in length. The individual layer thicknesses were measured to be ~830 nm.

In another embodiment having fibers containing 376 layers, the layer stack was 500 mm by 160 mm and continuous in length. The individual layers were measured to be about 1.32 mm prior to post drawing. The same fibers were then length oriented with the roll speed ratio at 4: 1 at 90°C. The resulting fibers were then 226 mm by 92 mm and continuous in length. The resulting individual layers were measured to be about 600 nm thick.

The length oriented multilayer filaments were then passed through a compressed air Heiberlein SLIDEJET DT15-2 (Wattwill Switzerland) nozzle with compressed air set at 30 psi and 10 m/min. The exposure to high velocity air caused the layers to separate, and the resulting material was a continuous fibrous string or nano-ribbon yarn. When compressed air was set above 80 psi, the material would often break.

In another embodiment, the multilayer filaments were separated through ultrasonication, which both separated and further fibrillated the nano-ribbons along their length.

The samples were observed under scanning electron microscopy (SEM) and using a Phenom ProX (Thermo Fisher Scientific, Waltham, MA). Based on individual observations, there is clearly a range of single layer nanofibers, as well as sets of 2-3 layers that remained adhered together, contributing to the distribution.

To determine mechanical properties, the multilayered filaments were prepared according to ASTM test method D2256 - 10(2015) with a 25.4 mm gauge length (separation distance between the grips). The samples were tested on the MTS RF100 load frame supplied by Instron (Norwood, MA) at 60 mm/min. Tensile testing results were calculated from 3 samples, and broke at an average load of 3.07 N, and had an average break tenacity of 167 Nm/g. The Youngs Modulus was calculated to be 217 MPa.

Example 2 A multilayer stack having 250 alternating layers of PL A and PP was extruded using a 250 layer feedblock, and a fiber faceplate having 1 row of 31 holes. The PLA grade used was 4032 supplied by NatureWorks LLC (Minnetonka, MN) and the PP grade was 1024 supplied by Exxon Mobil Corporation (Irving, TX). Two extruders were used, a first extruder for the PLA layers, a second for the PP layers. The first extruder was set to 226°C with a first necktube set to 226°C, the second extruder was set to 226°C with a second necktube set to 226°C. The necktubes connected and directed the resin from the extruders to the feedblock and die. The feedblock and die was set at 226°C. The first extruder was a single screw with a barrel diameter of 32 mm and was operated at 50 rotations per minute (rpm), the second extruder was a single screw with a barrel diameter of 32 mm and was operated at 38 rpm. The multilayer filaments were passed through a chilled water bath and further directed to a level winder Model 96B supplied by Leesona (Burlington, NC) and collected on a cone. The take up winder was set to 60 m/min. The final multilayer filaments contained 244 layers. One embodiment containing a 244 layer stack was 527 mm by 244 mm, and continuous in length. The individual layers were each measured to be 2.15 mm in thickness prior to any post-drawing.

The multilayer filaments were then length oriented on a draw stand supplied by Retech Aktiengesellschaft (Meisterschwanden, Switzerland) with 10cm wide godet rolls heated to 90°C and a 6: 1 speed ratio. The resulting multilayer filaments had cross-sections that were 193 mm by 91 mm and continuous in length. The individual layer thicknesses were measured to be ~790 nm.

The length oriented multilayer filaments were then passed through a compressed air Heiberlein SLIDEJET DT15-2 (Wattwill Switzerland) nozzle with compressed air set at 30 psi and 10 m/min. The exposure to high velocity air caused the layers to separate and the resulting material was a continuous fibrous string or nanoribbon yam.

The samples were observed under scanning electron microscopy (SEM) and using a Phenom ProX (Thermo Fisher Scientific, Waltham, MA). This sample was completely separated into single layers with only a few observable layers still stacked together.

To determine mechanical properties, the multilayered filaments were prepared according to ASTM test method D2256 - 10(2015) with a 25.4 mm gauge length

(separation distance between the grips). The samples were tested on the MTS RF100 load frame supplied by Instron (Norwood, MA) at 60 mm/min. Tensile testing results were calculated from 3 samples, and broke at an average load of 5.4 N, and had an average break tenacity of 279 Nm/g. The Youngs Modulus was calculated to be 363 MPa.

The nano-ribbon yarn was then coated in a water based Lurol ASM lubricant or spin finish supplied by Goulston Technologies (Monroe, NC) to improve processability during knitting. A single strand of the nano-ribbon yarn was then knitted on a SWG041N2 15-gauge knitting machine supplied by Shima Seiki USA (Monroe Twp, NJ), set with a stitch value of 33. No supporting yam was used to reinforce the nano-ribbon yam during knitting.

A multilayer stack having 500 alternating layers of PLA and PP was extruded using a 500 layer feedblock and a fiber faceplate having 1 row of 8 holes. The PLA grade used was 4060D supplied by NatureWorks LLC (Minnetonka, MN) and the PP grade was 1024 supplied by Exxon Mobil Corporation (Irving, TX). Two extruders were used, a first extruder for the PLA layers, a second for the PP layers. The first extruder was set to 232°C with a first endcap set to 224°C, the second extruder was set to 232°C with a first endcap set to 224°C. The extruders were connected directly to the feedblock, and no necktubes were used. The first extruder was a single screw with a barrel diameter of 8 mm and was operated at 265 rotations per minute (rpm), the second extruder was a single screw with a barrel diameter of 8 mm and was operated at 234 rpm. The multilayer filaments were passed through a chilled water bath and further directed to a draw stand supplied by Retech Aktiengesellschaft (Meisterschwanden, Switzerland) with 10 cm wide godet rolls heated to 90°C and collected on a cone. The take up roller was set to 70 m/min.

The multilayer filaments were then length oriented on the same draw stand at 90°C and a 6: 1 speed ratio.

The length oriented multilayer filaments were then passed through a compressed air Heiberlein SLIDEJET DT15-2 (Wattwill Switzerland) nozzle with compressed air set at 30 psi and 10 m/min. The exposure to high velocity air caused the layers to separate, and the resulting material was a continuous fibrous string or nanoribbon yarn.

(separation distance between the grips). The samples were tested on the MTS RF100 load frame supplied by Instron (Norwood, MA) at 60 mm/min. Tensile testing results were calculated from 3 samples, and broke at an average load of 12.4 N, and had an average break tenacity of 356 Nm/g. The Youngs Modulus was calculated to be 463 MPa. Although specific embodiments of this invention have been shown and described herein, it is understood that these embodiments are merely illustrative of the many possible specific arrangements that can be devised in application of the principles of the invention. Numerous and varied other arrangements can be devised in accordance with these principles by those of ordinary skill in the art without departing from the spirit and scope of the invention. Thus, the scope of the present invention should not be limited to the structures described in this application, but only by the structures described by the language of the claims and the equivalents of those structures.

Claims

What is claimed is:

1. A process for converting a multilayer filament to a plurality of nano-ribbons, the process comprising:

co-extruding a first layer and a second layer to form the multilayer filament; and separating the multilayer filaments to form a plurality of nano-ribbons having substantially flat cross-sections.

2. The process of claim 1, wherein the first layer and the second layer are resin or polymer layers.

3. The process of claim 1, further comprising length orientating the multilayer filaments.

4. The process of claim 1, further comprising a plurality of first layers and second layers alternately layered.

5. The process of claim 1, wherein the first layer is immiscible with the second layer.

6. The process of claim 1, wherein separating the multilayer filaments comprises mechanically or chemically separating the layers.

7. The process of claim 1, wherein separating the multilayer filaments comprises using compressed air, pressurized water, high velocity fluids or sonication.

8. The process of claim 1, wherein the nano-ribbons have a tensile strength of between about 150 and about 480 MPa.

9. The process of claim 1, wherein the first layer comprises polyester and the second polymer layer comprises polypropylene.

10. The process of claim 1, wherein the first layer comprises a combination of polymers.

11. The process of claim 1, wherein the first layer comprises a first polymer and a second polymer, wherein the first polymer comprises a majority by weight of the first layer, and wherein the first polymer is immiscible with the second polymer and the second layer.

12. The process of claim 1, wherein the first layer comprises a first polymer and a second polymer, wherein the first polymer of the first layer is immiscible with the second polymer of the first layer, and wherein the second layer comprises a first polymer and a second polymer, wherein the first polymer of the second layer is immiscible with the second polymer of the second layer.

13. A nano-ribbon yarn produced by the process of claim 1.

14. A nano-ribbon yam comprising ribbons having a thickness of between about 10 nanometers and 10 microns, wherein the ribbons have a substantially flat cross-section.

15. The nano-ribbon yarn of claim 14, wherein the ribbons comprise at least a first polymer and a second polymer.

16. The nano-ribbon yarn of claim 14, wherein the first polymer is immiscible with the second polymer.

17. The nano-ribbon yarn of claim 14, wherein the first polymer and the second polymer have little chemical affinity for each other.

18. The nano-ribbon yarn of claim 14, wherein the first polymer and the second polymer can be extruded into a layered structure with each other.

19. The nano-ribbon yarn of claim 14, wherein the first polymer comprises polyester and the second polymer comprises polypropylene.

20. The nano-ribbon yarn of claim 14, wherein the ribbons have a tensile strength of between about 150 and about 480 MPa.

21. A knitted fabric or nonwoven fabric comprised of the nano-ribbon yam of claim

13.