Pad comprising an extruded mesh and method of making thereof
10173391 ยท 2019-01-08
Assignee
Inventors
Cpc classification
Y10T428/24107
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B29D28/00
PERFORMING OPERATIONS; TRANSPORTING
B29C48/21
PERFORMING OPERATIONS; TRANSPORTING
B32B5/26
PERFORMING OPERATIONS; TRANSPORTING
Y10T428/24099
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B29C48/13
PERFORMING OPERATIONS; TRANSPORTING
B29L2031/50
PERFORMING OPERATIONS; TRANSPORTING
B29K2077/00
PERFORMING OPERATIONS; TRANSPORTING
B29D28/005
PERFORMING OPERATIONS; TRANSPORTING
A43B3/0026
HUMAN NECESSITIES
B29K2075/00
PERFORMING OPERATIONS; TRANSPORTING
B29K2995/0091
PERFORMING OPERATIONS; TRANSPORTING
B32B37/153
PERFORMING OPERATIONS; TRANSPORTING
B32B5/028
PERFORMING OPERATIONS; TRANSPORTING
B32B2250/20
PERFORMING OPERATIONS; TRANSPORTING
B29C48/12
PERFORMING OPERATIONS; TRANSPORTING
B29C48/0014
PERFORMING OPERATIONS; TRANSPORTING
B32B5/12
PERFORMING OPERATIONS; TRANSPORTING
International classification
B32B5/12
PERFORMING OPERATIONS; TRANSPORTING
B32B37/15
PERFORMING OPERATIONS; TRANSPORTING
B29D28/00
PERFORMING OPERATIONS; TRANSPORTING
B32B5/26
PERFORMING OPERATIONS; TRANSPORTING
B32B5/02
PERFORMING OPERATIONS; TRANSPORTING
B32B25/10
PERFORMING OPERATIONS; TRANSPORTING
Abstract
A structure for use in a compressible resilient pad. The structure contains both axially elastomeric strands and relatively inelastic strands co-extruded in various patterns. The structure has a high degree of both compressibility under an applied normal load and excellent recovery (resiliency or spring back) upon removal of that load.
Claims
1. A pad comprising: a bicomponent extruded mesh, the mesh including: a first layer of parallel strands running in a longitudinal direction (LD); a second layer of parallel strands on one side of the first layer, the second layer's strands running in a transverse direction (TD) and comprising elastomeric strands; and a third layer of parallel strands on an opposite side of the second layer as the first layer and running in the same direction as those of the first layer, wherein the first, second, and third layers are co-extruded at substantially the same time such that the strands in the first layer are positioned or aligned within the space between strands in the third layer, wherein materials for the first, second, and third layers are bonded together as a result of being co-extruded; and one or more layers of a woven fabric, membrane, LD or TD yarn arrays attached to a top and/or bottom surface of the extruded mesh.
2. The pad of claim 1, further comprising: one or more layers of a spunbond nonwoven or batt material attached to a top and/or bottom layer of the woven fabric, membrane, LD or TD yarn array and/or the extruded mesh.
3. A pad comprising: a bicomponent extruded mesh, the mesh including: a first layer of parallel strands running in a longitudinal direction; a second layer of parallel strands on one side of the first layer, the second layer's strands running in a transverse direction and comprising elastomeric strands; and a third layer of parallel strands on the opposite side of the second layer as the first layer and running in the same direction as those of the first layer, wherein the first, second, and third layers are co-extruded at substantially the same time such that the strands in the first layer are positioned or aligned within the space between strands in the third layer, wherein materials for the first, second, and third layers are bonded together as a result of being co-extruded; and one or more layers of a spunbond nonwoven or batt attached to the extruded mesh.
4. A pad comprising: a bicomponent extruded mesh including: a first layer of parallel strands running in a longitudinal direction; a second layer of an elastic material on one side of the first layer; and a third layer of parallel strands on an opposite side of the second layer as the first layer and running in the same direction as those of the first layer, wherein the first, second, and third layers are co-extruded at substantially the same time such that the strands in the first layer are positioned or aligned within the space between strands in the third layer, wherein materials for the first, second, and third layers are bonded together as a result of being co-extruded; and one or more layers of a nonwoven or batt attached to the extruded mesh.
5. A pad comprising: a bicomponent extruded mesh including: a first layer of parallel strands running in a longitudinal direction (LD); a second layer of an elastic material on one side of the first layer; and a third layer of parallel strands on an opposite side of the second layer as the first layer and running in the same direction as those of the first layer, wherein the first, second, and third layers are co-extruded at substantially the same time such that the strands in the first layer are positioned or aligned within the space between strands in the third layer, wherein materials for the first, second, and third layers are bonded together as a result of being co-extruded; and one or more layers of a woven fabric, membrane, LD or transverse direction (TD) yarn arrays attached to a top and/or bottom layer of the extruded mesh.
6. The pad of claim 5, further comprising: one or more layers of a nonwoven or batt attached to a top and/or bottom layer of the woven fabric, membrane, LD or TD yarn array and/or the extruded mesh.
7. A pad comprising: a bicomponent extruded mesh including: a first layer of parallel strands running in a longitudinal direction (LD); a second layer of parallel strands on one side of the first layer, the second layer's strands running in a transverse direction (TD) and comprising elastomeric strands; and a third layer of parallel strands on an opposite side of the second layer as the first layer and running in the same direction as those of the first layer, wherein the first, second, and third layers are co-extruded at substantially the same time such that the strands in the first layer are positioned or aligned within the space between strands in the third layer, wherein materials for the first, second, and third layers are bonded together as a result of being co-extruded; and wherein the first, second and third layers are extruded together or sequentially.
8. A pad comprising: a bicomponent extruded mesh including: a first layer of parallel strands running in a longitudinal direction (LD): a second layer of an elastic material on one side of the first layer; and a third layer of parallel strands on an opposite side of the second layer as the first layer and running in the same direction as those of the first layer, wherein the first, second, and third layers are co-extruded at substantially the same time such that the strands in the first layer are positioned or aligned within the space between strands in the third layer, wherein materials for the first, second, and third layers are bonded together as a result of being co-extruded, and, wherein the first, second and third layers are extruded together or sequentially.
9. A pad comprising bicomponent extruded mesh including: a first layer of parallel strands running in a longitudinal direction; a second layer of the parallel strands on one side of the first layer, the second layer's strands running in a transverse direction and comprising elastomeric strands; and a third layer of parallel strands on an opposite side of the second layer as the first layer and running in the same direction as those of the first layer, wherein the first, second, and third layers are co-extruded at substantially the same time such that the strands in the first layer are positioned or aligned within the space between strands in the third layer, wherein materials for the first, second, and third layers are bonded together as a result of being co-extruded, wherein the first, second, and third layers form a structure having a desired thickness, wherein under a compressive load the second layer stretches to enable the strands of the first and third layers to nest between each other in substantially the same plane, and wherein upon release of the compressive load an elasticity of the second layer is selected to cause the first and third layers to spring back to return the structure to substantially the desired thickness.
10. A pad comprising bicomponent extruded mesh including, a first layer of parallel strands running in a longitudinal direction; a second layer of an elastic material on one side of the first layer; and a third layer of parallel strands on an opposite side of the second layer as the first layer and running in the same direction as those of the first layer, wherein the first, second, and third layers are co-extruded at substantially the same time such that the strands in the first layer are positioned or aligned within the space between strands in the third layer, wherein materials for the first, second, and third layers are bonded together as a result of being co-extruded, wherein the first, second, and third layers form a structure having a desired thickness, wherein under a compressive load the second layer stretches to enable the strands of the first and third layers to nest between each other in substantially the same plane, and wherein upon release of the compressive load an elasticity of the second layer is selected to cause the first and third layers to spring back to return the structure to substantially the desired thickness.
Description
BRIEF DESCRIPTION OF DRAWINGS
(1) The accompanying drawings, which are included to provide a further understanding of the invention, are incorporated in and constitute a part of this specification. The drawings presented herein together with the description serve to explain the principles of the invention. In the drawings:
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DETAILED DESCRIPTION
(11) For purposes of the present invention, the term transverse direction is synonymous and sometimes simply referred to as TD, as is the term longitudinal direction, sometimes simply referred to as LD. However, the term transverse is sometimes also used to refer to strands/members/components which extend in a direction opposite to that of strands/members/components previously referred to. The meaning will be clear from the context in any particular instance.
(12) The invention, according to one embodiment, is a shock-absorbing pad that utilizes a unique structure which provides excellent elastic behavior under a normal pressure load with as high thickness recovery (resiliency).
(13) One embodiment of the invention is shown in
(14) Turning now to
(15) In another embodiment, strands 14 have the same position and relative orientation/spacing as above, but strands 12 are extruded and oriented at less than 90 degree angle to strands 14, preferably at a 45 degree angle.
(16) According to one exemplary embodiment, there can be more than two layers of is functional LD strands and more than one layer of TD strands. With three layers of LD strands and two layers of TD strands in between, two of the three LD strand layers, for example, must be spaced apart relative to each other to allow nesting. For example, top and middle LD layers can be oriented such that strands in the middle layer fit in the space between two adjacent strands of the top LD, and strands in the bottom LD layer are stacked in vertical orientation with either the top or middle LD layers. Furthermore, the two layers of TD strands can be elastomeric, or only one layer can be and the other layer can be a functional strand layer to provide a greater degree of void volume, for example, under compressive load.
(17) Also the degree of compression/resiliency is controlled by the elasticity of the required strands, size and number of strands, number of layers of the strands, and of course the totality of the structure itself. The inventive structure can also be part of a laminate with other strand arrays (MD and/or CD) or woven fabrics attached thereto.
(18) The invention, according to one embodiment, is a method of forming a bicomponent extruded mesh or netting structure 10, as shown in
(19) Preferably, the elastomeric 12 and hard (incompressible and inelastic) strands 14 are orthogonal to each other, but this is not required. It should be noted that when this structure is uncompressed in the through thickness direction, that structure appears as shown in
(20) Note the hard (or relatively inelastic) strand 14 diameter, or sizes if nonround, can be equal to the elastomeric strand 12 diameter or sizes. However, the hard strand diameter or size may, in some instances, be greater than the elastomeric strand diameter or size, or vice versa. The diameters of round strands can range from 0.1 mm to 150 mm; however the preferred range is 0.2 mm to 70 mm.
(21) Note strand systems (1) and (3) can be the same as each other or they can be different in terms of material, form, shape, etc. It is only required that the strands in layer (3) are spaced to fit between adjacent strands of layer (1) or vice versa. Strand shapes can include square, rectangular, elliptical or oval, triangular, star-shaped, grooved or any polygonal shape, and the dimension of the longest axis can be up to at least 250 mm.
(22) Also note there does not have to be a one to one relationship between the number of strands of layers (1) and (3), but the number of strands in layer (3) can be only a fraction of the number of strands in layer (1) or vice versa. For example, layer (3) may contain only half the strands of layer (1) so that there are spaces between the strands of layer (3) in use, creating additional void volume. Strand spacing (from center to center) can be equal for both LD (hard) and TD (elastomeric) strands. However, the strand spacing may be varied based on the desired air or water permeability, open area, and void volume of the end structure. Maximum strand density can be based upon strand spacing being equal to two times the strand diameter, and minimum strand density can be based upon strand spacing being equal to three or more times the strand diameter. A bicomponent extruded mesh 10 with spacing being equal to three times the strand diameter is shown in
(23) Several materials can be used as the elastomeric strand material 17 which occupies the middle layer (2) of the three layer bicomponent extruded mesh. Examples include styrene block copolymer, elastomeric copolyesters, elastomeric copolyamides, elastomeric polyolefins and thermoplastic polyurethanes. Similarly, several materials can be used as the hard or inelastic strand material 14. Examples include polypropylene, polyethylene, polybutene, polyesters, polyamides, hard polyurethanes, and copolymers of such resins. Whatever materials are selected for the elastomeric and hard strands, these materials must be bonded together as a result of the extrusion process. One knowledgeable in polymeric materials knows that polymers can be formulated with additives to promote bonding between two different polymers. Clearly, forming bonds during the extrusion of the netting is required so selection of appropriate materials is paramount.
(24) A high bond strength for the nodes (where the LD and TD strands cross and contact each other) of the strands is required. It is especially important if the extruded netting or mesh is oriented (like in monofilament extrusion processing) in a second processing step. In this process step, high forces are transferred and distributed through the netting joints/nodes to and from netting strands in all directions. Without a good strand to strand bond at the joint/node, the product will tear apart and fail.
(25) Advantages of the bicomponent elastomeric mesh of the present invention over all-elastomeric netting are many. For instance, the product may be designed with one set of properties in one direction, and another set of properties in the opposite direction. Specifically, high yield strength and dimensional stability can be designed by using a relatively inelastic polymer such as polypropylene in one direction, while the elastomeric (compression and recovery) properties of the mesh netting are ensured by the use of a good elastomeric material in the opposite direction.
(26) According to one embodiment, the inventive structure can be shock-absorbing pad that utilizes a unique structure which provides excellent elastic behavior under a normal pressure load with high caliper or thickness in the through direction (normal to the structure plane) recovery. This structure 100, shown in
(27) A schematic of a compressible resilient bicomponent extruded mesh formed according to this exemplary embodiment is shown in
(28) An elastic extruded film or sheet that is defined as elastic, resilient, and compressible in its thickness direction and extensible, bendable, and resilient in its length and transverse directions is required for this embodiment. The elastic extruded film or sheet can optionally be perforated, as shown in
(29) According to one embodiment of the present invention, structure 20 can include one or more layers of a woven fabric 22 attached to a top and/or bottom surface of the bottom surface of the bicomponent extruded mesh 10. An example is shown in
(30) According to one embodiment, the extruded mesh can be structurally integrated with one or more layers of a nonwoven material 24 of textile fibers attached to the top and/or bottom surface of the woven layer 22 and/or the co-extruded structure itself by for example, needling (needle punching), or use of adhesives or thermal fusion. The nonwoven material 24 attached to the bicomponent extruded mesh may be made up of any conventional textile fibers. Representative of such textile fibers are staple fibers of polyesters, polyamides and the like.
(31) According to another embodiment, one or more layers of nonwoven, textile fibers such as batt or spunbonded webs can be adhered to the outer surface of the bicomponent extruded mesh 10 itself, for example. The adherence of an additional layer(s) to the bicomponent extruded mesh 10 can also be by needling, adhesion, or thermal fusion. For simplicity, the embodiment described has only two nonwoven fibrous layers. However, those skilled in the art will appreciate that any number of nonwoven fibrous layers such as layer 24 may be built up to obtain a desired structure of a particular thickness, density and void volume.
(32) The bicomponent extruded mesh can be processed, if necessary, to produce a smooth surface, and can be coated with foams, or impregnated with resins or foams that are also compressible and resilient in nature. Other forms including one or more layers of a membrane, or yarn arrays can be laminated to the bicomponent extruded mesh. The structure which includes the compressible, resilient bicomponent extruded mesh must be constructed to have a sufficient degree of compressibility as well as have sufficient elasticity as well as strength to allow the structure to rebound, or spring back, as required upon exposure to, and removal of, an applied load normal to the structures surfaces for the end use. For example, for use as a component of the support pad in the bottom of a shoe, stepping would cause the pad to compress at a desired rate and to a desired degree, giving some support and cushion to the foot, and lifting the foot would cause the pad to rebound to its original thickness. The compression and rebounding of the is structure has at least the following benefits:
(33) 1.) Improved recovery characteristics over memory foams, gels, spring systems, etc;
(34) 2.) Smooth and uniform surface characteristics to allow, for example, improved support of the shoe and the foot;
(35) 3.) Excellent retention of the recovery/dampening characteristics due to the mesh structure's full recovery;
(36) 4.) Excellent compression recovery vs. weight ratio, allowing significant dampening capability with a light weight structure;
(37) 5.) Excellent breathability of the shock absorbing structure, allowing perspiration and other moisture to evaporate and/or be removed at each compression.
(38) For any of the embodiments of the bicomponent mesh or netting, while two layers of inelastic strands are taught, only one layer of inelastic (LD) tensile strands may be necessary for the structure to function in use, and the other layer on the other surface can also be elastic.
(39) Furthermore, for any of the embodiments taught of the bicomponent (may be different elastomers or the same) mesh netting, all three layers may be elastic as long as the mesh is laminated to a LD load (tensile) bearing structure, such as a woven fabric made from inelastic polyester or polyamide. According to one embodiment, the bicomponent mesh or netting in any of the previous embodiments can be turned 90.degree. so that the relatively inelastic functional LD strands are now in the TD and the elastic TD strands or elastic material are in the LD as long as the mesh or netting is laminated to a LD load (tensile) bearing structure, such as a woven fabric made from inelastic polyester or polyamide.
(40) Modifications to the present invention would be obvious to those of ordinary skill in the art in view of this disclosure, but would not bring the invention so modified beyond the scope of the appended claims.