The present invention relates to fiber-containing composites (e.g., natural fiber-containing composites), materials formed therewith, and methods for making the same.
A unitary, fiber-containing composite is described herein. In a first embodiment, the unitary, fiber-containing composite comprises a first region, a second region disposed above the first region, and a first transitional region disposed between the first region and the second region. The first region comprises a plurality of first thermoplastic binder fibers and a plurality of bast fibers, and the second region comprises a plurality of second binder fibers and a plurality of bast fibers. The first transitional region comprises concentrations of the first binder fiber, the second binder fiber, and the bast fiber. The concentration of the first binder fiber in the first transitional region is greatest proximate to the first region and least proximate to the second region, and the concentration of the second binder fiber in the first transitional region is greatest proximate to the second region and least proximate to the first region.
In another embodiment, the composite comprises a third region disposed above the second region, the third region comprising a binder material. In certain embodiments, the binder material in the third region comprises a third binder fiber, and the composite comprises a second transitional region disposed between the second region and the third region. In this embodiment, the second transitional region comprises concentrations of the second binder fiber, the bast fiber, and the third binder fiber. The concentration of the second binder fiber in the second transitional region is greatest proximate to the second region and least proximate to the third region, and the concentration of the third binder fiber in the second transitional region is greatest proximate to the third region and least proximate to the second region.
In a further embodiment of the unitary, fiber-containing composite described herein, the composite comprises a fourth region disposed above the third region, a third transitional region disposed between the third region and the fourth region, a fifth region disposed above the fourth region, and a fourth transitional region disposed between the fourth region and the fifth region. The fourth region comprises a plurality of the second binder fibers and a plurality of the bast fibers, and the fifth region comprises the first binder material and a plurality of the bast fibers. The third transitional region comprises concentrations of the second binder fiber, the bast fiber, and the third binder fiber. The concentration of the third binder fiber in the third transitional region is greatest proximate to the third region and least proximate to the fourth region, and the concentration of the second binder fiber in the third transitional region is greatest proximate to the fourth region and least proximate to the third region. The fourth transitional region comprises concentrations of the second binder fiber, the bast fiber, and the first binder fiber. The concentration of the second binder fiber in the fourth transitional region is greatest proximate to the fourth region and least proximate to the fifth region, and the concentration of the first binder fiber in the fourth transitional region is greatest proximate to the fifth region and least proximate to the fourth region.
A method for producing a unitary, fiber-containing composite is also described herein. In one embodiment, the method comprises the steps of providing a plurality of first binder fibers having a first linear density, a plurality of second binder fibers having a second linear density, and a plurality of bast fibers. The pluralities of first binder fibers, second binder fibers, and bast fibers are then blended to produce a fiber blend, and the fiber blend is then projected onto a moving belt such that a unitary, fiber-containing composite is formed. In this method, the second linear density can be greater than the first linear density, such that the fibers are deposited onto the moving belt in regions or strata comprising different relative concentrations of the fibers.
In a further embodiment of the method described herein, the first step comprises providing a plurality of third binder fibers having a third linear density, and the second step comprises blending the pluralities of first, second, and third binder fibers and the bast fibers to produce the fiber blend. The resulting fiber blend is then projected onto the moving belt in the same or similar manner as that utilized in the first method embodiment. In this embodiment, the third linear density can be greater than the first and second linear densities.
In another embodiment of the method described herein, the method further comprises the step of passing heated air through the unitary, fiber-containing composite produced by the above-described embodiments to at least partially melt the first, second, and third binder fibers.
In another embodiment of the method described herein, the method further comprises the steps of heating the unitary, fiber-containing composite produced in the above-described embodiments to further melt the first, second, and third binder fibers and compressing the composite to retain the fibers contained therein in a compressed state.
In a further embodiment of the method described herein, the method comprises the step of cutting the unitary, fiber-containing composite along a plane that is parallel to the z-direction of the composite to produce at least a first section and a second section. The first section is then placed on top of the second section, and the stacked sections are simultaneously compressed and heated. The first and second sections produced by the cutting step each comprise the first region, first transitional region, second region, second transitional region, and third region of the unitary, fiber-containing composite from which they are cut, and the first section is placed on top of the second section so that the first region of the first section opposes the first region of the second section or the third region of the first section opposes the third region of the second section. In the heating step, the first, second, and third binder fibers contained in the sections are further melted, and the opposing regions of the first and second sections are fused together. The composite is then compressed in order to retain the fibers in the first and second sections in a compressed state.
A unitary, fiber-containing composite is described herein. As utilized herein with reference to the fiber-containing composite, the term “unitary” refers to the fact that the enumerated regions of the composite do not form layers having distinct boundaries separating them from the adjacent region(s). Rather, the enumerated regions are used to refer to portions of the composite in which the different fibers are contained in different concentrations. More specifically, the enumerated regions are used to refer to portions of the thickness of the composite in which different fibers predominate or in which the concentration gradient of the fibers (e.g., how the concentration of a particular fiber changes with the thickness of the composite) differs from the adjacent portions (i.e., portions above and/or below) of the composite. Furthermore, while the composite will be described herein as containing particular fibers in specific regions, those of ordinary skill in the art will appreciate that each region of the composite can contain any of the fibers present in the composite. Nevertheless, particular fibers or combinations of fibers will predominate in particular portions of the thickness of the composite, and the enumerated regions described herein are intended to refer to those portions of the composite.
As depicted in
As utilized herein, the term “bast fiber” refers to strong woody fibers obtained chiefly from the phloem of plants. Suitable bast fibers include, but are not limited to, jute, kenaf, hemp, flax, ramie, roselle, and combinations thereof. Other suitable bast fibers include, but are not limited to, leaf fibers (e.g., fibers derived from sisal, banana leaves, grasses (e.g., bamboo), or pineapple leaves), straw fibers (e.g., fibers derived from wheat straw, rice straw, barley straw, or sorghum stalks), and husk fibers (e.g., fibers derived from corn husk, bagasse (sugar cane), or coconut husk). In certain embodiments, the bast fiber is jute. The fiber-containing composite can contain any suitable amount of the bast fiber(s). For example, the bast fibers can comprise about 30 to about 70 wt. %, about 30 to about 60 wt. %, or about 60 wt. % of the total weight of the fiber-containing composite. The bast fibers suitable for use in the disclosed fiber-containing composite and method can have any suitable linear density (i.e., denier). For example, the bast fibers can have a linear density of about 8.
The binders contained in the fiber-containing composite can be any suitable binder material. For example, the binder materials can be a thermoplastic material that is capable of at least partially melting when heated so that the fibers contained within the composite will be bonded together. Suitable thermoplastic binder materials include, but are not limited to, polyesters (e.g., polyethylene terephthalate (PET) or glycol-modified PET (PETG)), polyamides (e.g., nylon 6 or nylon 6,6), polyethylenes (e.g., high density polyethylene (HDPE) or linear low density polyethylene (LLDPE)), polypropylenes, polylactic acid, poly(1,4-cyclohexanedimethylene terephthalate) (PCT), and combinations thereof.
As noted above, the binder material contained in the unitary, fiber-containing composite can be provided in the form of binder fibers. The binder fibers contained in the fiber-containing composite can be any suitable binder fibers. For example, the binder fibers can comprise a thermoplastic material that is capable of at least partially melting when heated, thereby providing a means by which the binder fibers and bast fibers can become interconnected within the fiber-containing composite. Suitable thermoplastic binder fibers include polyester fibers (e.g., polyethylene terephthalate (PET) fibers or glycol-modified PET (PETG) fibers), polyamide fibers (e.g., nylon 6 or nylon 6,6), polyethylene fibers (e.g., fibers containing high density polyethylene (HDPE) or linear low density polyethylene (LLDPE)), polypropylene fibers, polylactic acid fibers, fibers containing poly(1,4-cyclohexanedimethylene terephthalate) (PCT), cellulose fibers (e.g., rayon fibers), fibers containing 1,3-propanediol terephthalate, and combinations thereof. Suitable binder fibers also include, but are not limited to, bicomponent binder fibers (e.g., bicomponent binder fibers comprising a thermoplastic sheath) and thermoplastic binder fibers having a relatively low melt flow rate. Suitable bicomponent fibers include bicomponent, sheath-core fibers in which the sheaths have a lower melting point than the cores of the fibers. For example, the bicomponent, sheath-core fiber can have a polyethylene sheath (e.g., a high density polyethylene sheath) and a polypropylene or polyester core. Other suitable bicomponent fibers include fibers having a PET copolymer sheath and a PET core, a PCT sheath and polypropylene core, a PCT sheath and a PET core, a PETG sheath and a PET core, a HDPE sheath and a PET core, a HDPE sheath and a polypropylene core, a LLDPE sheath and a PET core, a polypropylene sheath and a PET core, or a nylon 6 sheath and a nylon 6,6 core. When such fibers are used in the disclosed composite, the composite can be heated so that the sheaths of the bicomponent fibers are melted to provide links between adjacent fibers within the composite, while the cores of the bicomponent fiber retain their fibrous structure. As noted above, the binder fibers can be thermoplastic binder fibers in which the thermoplastic material has a relatively low melt flow rate. For example, the melt flow rate of the thermoplastic fibers can be about 18 g/10 min. or less (e.g., about 8 g/10 min.), as determined in accordance with, for example, ASTM Standard D1238 entitled “Standard Test Method for Melt Flow Rates of Thermoplastics by Extrusion Plastometer.” When such fibers are used in the disclosed composite, the composite can be heated so that the thermoplastic binder fibers are at least partially melted to provide links between adjacent fibers, while the relatively low melt flow rate of the thermoplastic material allows the binder fibers to retain their fibrous structure.
The binder fibers contained in the fiber-containing composite can have any suitable linear density or combination of linear densities. In certain embodiments, each of the different binder fiber types contained in the composite can have different linear densities. For example, as depicted in
The binder material contained in the third region can be any suitable binder material. For example, the binder material can comprise a layer of thermoplastic material that has been laminated to the upper surface of the second region. Such a layer can be formed, for example, by depositing thermoplastic particles onto the upper surface of the second region and at least partially melting the particles to bond them to the fibers contained in the second region. As depicted in
The binder fibers suitable for use in the above-described third region 110 of the composite 100 can be any suitable binder fibers, including those described above as suitable for use as the first and second binder fibers. As with the first and second binder fibers, the third binder fibers can have any suitable linear density. In certain embodiments, the third binder fibers 120 have a linear density that is greater than the linear density of the first and second binder fibers 114, 116. For example, the third binder fibers 120 can have a linear density of about 22.
The unitary, fiber-containing composite described herein can have any suitable weight and density. For example, the composite can have a weight of about 500 to about 2000 g/m2, about 500 to about 1500 g/m2, or about 600 to about 1200 g/m2. In certain embodiments, the unitary, fiber-containing composite can have a density of about 0.08 to about 2 g/cm3, about 0.08 to about 1.5 g/cm3, about 0.2 to about 1.5 g/cm3, about 0.2 to about 0.7 g/cm3, or about 0.25 to about 0.6 g/cm3.
In a further embodiment of the unitary, fiber-containing composite described herein, the composite comprises fourth and fifth regions and third and fourth transitional regions disposed above the third region of the composite. In such an embodiment, the additional layers of the composite (i.e., the fourth and fifth regions and third and fourth transitional regions) can resemble mirror images of the first and second regions and first and second transitional regions of the composite described above. For example, as depicted in
In addition to these regions, the composite 200 further comprises a fourth region 214 disposed above the third region 210, a third transitional region 212 disposed between the third region 210 and the fourth region 214, a fifth region 218 disposed above the fourth region 214, and a fourth transitional region 216 disposed between the fourth region 214 and the fifth region 218. As shown in
The unitary, fiber-containing composite can comprise other fibers in addition to those enumerated above. For example, in order to increase the flame resistance of the resulting composite, the composite can further comprise flame retardant fibers. As utilized herein, the term “flame retardant fibers” refers to fibers having a Limiting Oxygen Index (LOI) value of about 20.95 or greater, as determined by ISO 4589-1. Alternatively, the fibers contained in the composite (e.g., the bast fibers and/or the binder fibers) can be treated with a flame retardant in order to increase the flame resistance of the composite. Also, in certain other embodiments, the composite can comprise fibers derived from animal sources, such as wool, silk, or feathers (e.g., chicken feathers separated from the quill), in addition to or in place of the bast fibers.
The unitary, fiber-containing composite described above can be utilized in a variety of applications. For example, the composite can be used as the substrate for an automobile headliner, an automobile door panel, a panel used in office furniture, etc. In one embodiment, the composite comprises the structural support for an automobile headliner. In such an embodiment, the composite can have a fabric layer adhered to one surface with or without the use of an additional adhesive. For example, in certain embodiments, the binder material disposed on the surface of the composite can provide sufficient tack for the fabric to adhere to the surface of the composite. Such an automobile headliner can also comprise a layer of foam or other suitable material (e.g., batting) disposed between the composite and the fabric layer.
A method for producing a unitary, fiber-containing composite is also described herein. In one embodiment, the method comprises the steps of providing a plurality of first binder fibers having a first linear density, a plurality of second binder fibers having a second linear density, and a plurality of bast fibers. The pluralities of first binder fibers, second binder fibers, and bast fibers are then blended to produce a fiber blend, and the fiber blend is then projected onto a moving belt such that a unitary, fiber-containing composite is formed. In this method, the second linear density can be substantially equal to the third linear density and greater than the first linear density, such that the fibers are deposited onto the moving belt in regions or strata comprising different relative concentrations of the fibers.
An apparatus suitable for performing the above-described method is depicted in
In a further embodiment of the method described herein, the first step comprises providing a plurality of third binder fibers having a third linear density, and the second step comprises blending the pluralities of first, second, and third binder fibers and the bast fibers to produce the fiber blend. The resulting fiber blend is then projected onto the moving belt in the same or similar manner as that utilized in the first method embodiment. In this embodiment, the third linear density can be greater than the first and second linear densities.
The fibers suitable for use in the above-described methods can be any suitable binder fibers and bast fibers. For example, the first, second, third, and bast fibers suitable for use in the described methods can be the same as those discussed above with respect to the various embodiments of the unitary, fiber-containing composite.
In certain embodiments of the described methods, such as when at least one of the binder fibers is a thermoplastic binder fiber, the unitary, fiber-containing composite produced by the above-described steps can be heated to at least partially melt the thermoplastic binder fiber and bond together at least a portion of the fibers contained in the composite. For example, the method can further comprise the step of passing heated air through the unitary fiber-containing composite produced by the above-described embodiments to partially melt all or a portion of the binder fibers. As will be understood by those of ordinary skill in the art, the unitary fiber-containing composite can be heated by other means, such as infrared radiation. This step serves to set an initial thickness for the composite of, for example, about 5 to about 50 mm or about 10 to about 50 mm.
In another embodiment of the method described herein, the unitary, fiber containing composite can be compressed to produce a composite having a density and/or a rigidity that are high enough for the composite to act as a structural support, for example, for an automobile headliner. In such an embodiment, the method can further comprise the step of heating the unitary, fiber-containing composite produced in the above-described embodiments using, for example, a hot belt laminator, which concentrates heat on the surfaces of the composite. Such heating further melts the first, second, and third binder fibers, and the compressive forces exerted on the composite by the laminator serve to retain the fibers in a compressed state.
The unitary, fiber-containing composite can be further processed using convention “cold mold” thermoforming equipment in which the composite is first heated and then pressed to the appropriate shape and thickness using an unheated mold. In such an embodiment of the method, the composite can be heated to a temperature of about 170 to about 215° C. during a heating cycle of about 30 to about 120 seconds using, for example, infrared radiation. The heated composite is then placed inside a mold, which typically is maintained at a temperature of about 10 to about 30° C., and compressed to the appropriate shape and thickness. The compression step typically is about 1 minute in length, during which time the thermoplastic binder fibers will cool to such an extent that the composite will maintain substantially the compressed configuration upon removal from the mold. As will be understood those of ordinary skill in the art, owing at least partially to the rigidity of the bast fibers, the composite may expand (for example, in the z-direction) upon heating and before being placed in the mold.
In a further embodiment of the method described herein, the method comprises the step of cutting the unitary, fiber-containing composite along a plane that is parallel to the z-direction of the composite (i.e., the thickness of the composite) to produce at least a first section and a second section. The first section is then placed on top of the second section, and the stacked sections are heated and compressed. The first and second sections produced by the cutting step each comprise the first region, first transitional region, second region, second transitional region, and third region of the unitary, fiber-containing composite from which they are cut, and the first section is placed on top of the second section so that the first region of the first section opposes the first region of the second section or the third region of the first section opposes the third region of the second section. In the heating and compression step, the first, second, and third binder fibers contained in the sections are further melted, and the opposing regions of the first and second sections are fused together. The step of heating and then compressing the composite also serves to retain the fibers in the first and second sections in a compressed state.
The following example further illustrates the invention but, of course, should not be construed as in any way limiting its scope.
This example demonstrates a method for producing a unitary, fiber-containing composite as described above and the properties of a unitary, fiber-containing composite as described above. Three similar unitary, fiber-containing composites (Samples A-C) were produced by air laying a fiber blend using a K-12 HIGH-LOFT RANDOM CARD by Fehrer AG (Linz, Austria). In particular, the composites were produced from a fiber blend containing approximately 40 wt. % (based on the total weight of the fiber blend) of bicomponent binder fibers and approximately 60 wt. % of jute fibers, which had a linear density of approximately 8.
As noted above, the above-described fiber blend was air laid using the K-12 HIGH-LOFT RANDOM CARD by projecting the fibers onto a moving belt. Due to the difference in denier between the fibers contained in the fiber blend, the composites produced by the air laying step contained a greater concentration of the 1.
Sample A was then produced by passing a composite, which had been laid so that it had a weight of approximately 1100 g/m2, through a compression oven in which the belts were heated to a temperature of approximately 204° C. (400° F.). After passing through the compression oven, Sample A had a thickness of approximately 3.3 mm.
Samples B and C were produced by cutting two composites, which had been laid so that the composites had weights of approximately 537 g/m2 and approximately 412 g/m2, respectively, in the z-direction (i.e., along a plane parallel to the thickness of the composite) and stacking the resulting sections on top of each other so that the regions containing the greatest concentration of the 35.
Samples A-C were then tested to determine their physical properties, such as the stiffness, strength, toughness, flammability, and sound absorption at different frequencies. The results of these measurements, including the test methods used to determine the properties, are set forth in the Table below.
As can be seen from the results set forth in the Table above, Samples A-C exhibited physical properties which should render the composites suitable for use as, for example, the substrate for an automobile headliner, an automobile door panel, or a panel used in office furniture. In particular, the stiffness, strength, and toughness of the composites indicate that they should be able to span the width and/or length of a typical automobile passenger compartment without significant or observable sagging. In particular, the composites should be able to pass the climatic sag requirements of most automobile manufacturers. Furthermore, the sound absorption measurements demonstrate that the composites should be able to provide an amount of sound absorption that is desirable for certain applications, such as the substrate for an automobile headliner.
All references, including publications, patent applications, and patents, cited herein are hereby incorporated by reference to the same extent as if each reference were individually and specifically indicated to be incorporated by reference and were set forth in its entirety herein.
The use of the terms “a” and “an” and “the” and similar referents in the context of describing the invention (especially in the context of the following claims) are to be construed to cover both the singular and the plural, unless otherwise indicated herein or clearly contradicted by context. The terms “comprising,” “having,” “including,” and “containing” are to be construed as open-ended terms (i.e., meaning “including, but not limited to,”) unless otherwise noted. Recitation of ranges of values herein are merely intended to serve as a shorthand method of referring individually to each separate value falling within the range, unless otherwise indicated herein, and each separate value is incorporated into the specification as if it were individually recited herein. All methods described herein can be performed in any suitable order unless otherwise indicated herein or otherwise clearly contradicted by context. The use of any and all examples, or exemplary language (e.g., “such as”) provided herein, is intended merely to better illuminate the invention and does not pose a limitation on the scope of the invention unless otherwise claimed. No language in the specification should be construed as indicating any non-claimed element as essential to the practice of the invention.
Preferred embodiments of this invention are described herein, including the best mode known to the inventors for carrying out the invention. Variations of those preferred embodiments may become apparent to those of ordinary skill in the art upon reading the foregoing description. The inventors expect skilled artisans to employ such variations as appropriate, and the inventors intend for the invention to be practiced otherwise than as specifically described herein. Accordingly, this invention includes all modifications and equivalents of the subject matter recited in the claims appended hereto as permitted by applicable law. Moreover, any combination of the above-described elements in all possible variations thereof is encompassed by the invention unless otherwise indicated herein or otherwise clearly contradicted by context.
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