MANUFACTURED MATERIAL HAVING A COMBINATION OF A REINFORCEMENT MATERIAL AND A LOW MELT MATERIAL

Information

  • Patent Application
  • 20240175173
  • Publication Number
    20240175173
  • Date Filed
    November 27, 2023
    10 months ago
  • Date Published
    May 30, 2024
    4 months ago
  • Inventors
    • Hanna; Jennifer (Greer, SC, US)
    • Nadunayagam; Priyadharshan
  • Original Assignees
Abstract
A method of manufacturing a material, including a thermoset material, comprising: providing a reinforcement fiber; combining a low melt fiber with the reinforcement fiber using the method of plying, twisting, air texturing, air entanglement, yarn made via the coating extrusion process, whereas the coated area has a lower melt than the core and the reinforcement fiber, co-weaving, co-mingling, and any combination thereof; and, applying heat to the combination to melt the low melt fiber to form a fiber composite wherein a melting point of the reinforcement fiber is higher than the operational temperature resulting from the application of the heat. The fiber combination can be a fabric and can be hydrophobic. The fiber combination or fabric can include properties taken from the group consisting of lighter thermoplastic combination, fracture resistance or elimination, increased impact resistance, vibration damping, low conductivity, reduced structural failures, dielectric properties, and any combination thereof.
Description
BACKGROUND
(1) Field of Invention

Disclosed is a method of a reinforcement fiber and low melt material such as a thermoplastic polymer and polyester, resulting in a matrix having a low melt and configured for weaving into a fabric without the need for reliance on sheets, that can provide high performance properties in an end product that can include, lighter weight, increased flex, improved impact resistance, and any combination thereof.


(2) Background

The material, including a thermoplastic material and reinforcement material, of the present invention can include the combination of a first fiber and low melt fiber that can exhibit any of a high modulus, high tenacity. The material can include a unique crystalline structure including in the multifilament polyolefin fiber, including a reinforcement fiber, and can be combined with a resin or matrix material. The manufacturing process can generally include extruding a polymeric melt, including a polyolefin, at a relatively high throughput and low spin line tension and quenching the filaments in a liquid bath prior to drawing the fiber bundle at a relatively high draw ratio, for example greater than 10, in some embodiments. The filaments can be combined with a low melt fiber such as one with a melting point below 140° C. and process using one or more of automated fiber placement, thermoforming, collaborative composition manufacturing and robotic layup.


One problem with the current state of the art is that other thermoplastic materials need a manufacturing process where a fiber plus a liquid resin or a matrix system is used. It would be advantageous to have a thermoplastic that used two or more fibers.


SUMMARY OF THE INVENTION


text missing or illegible when filed





BRIEF DESCRIPTION OF THE FIGURES

A full and enabling disclosure of the present invention, including the best mode thereof, to one of ordinary skill in the art, is set forth more particularly in the remainder of the specification, including reference to the accompanying Figures in which:



FIG. 1 is a schematic of aspects of the Twisted material.



FIG. 2 is a flowchart of aspects of making the woven material.



FIG. 3 is a flowchart of aspects of making the Layup material.



FIGS. 4A through 4E are testing results for aspects of the material.



FIGS. 5A and 5B are testing results for aspects of the material.



FIGS. 6A and 6B are testing results for aspects of the material.



FIGS. 7A and 7B are testing results for aspects of the material.



FIGS. 8A and 8B are testing results for aspects of the material.



FIG. 9 is testing results for aspects of the material.



FIGS. 10A and 10B are testing results for aspects of the material.



FIG. 11 is testing results for aspects of the material.



FIG. 12 is testing results for aspects of the material.



FIG. 13 is a schematic of aspects of the material.



FIGS. 14 and 15 are schematics of one testing method.



FIGS. 16A and 16B are testing results for aspects of the material.



FIG. 17 is testing results for aspects of the material.



FIG. 18 is testing results for aspects of the material.





DESCRIPTION OF THE INVENTION

The current invention is a thermoplastic that can include polymer resins that soften when exposed to heat and hardens when cooled. The invention can be thermoplastic so that it can be recycled. In one embodiment, the first material can be a reinforcing fiber with properties that are taken from the group consisting of multi-filament olefin yarn, density 0.84/cc, hydrophobic, resistant to wear, ductile, durable, low dielectric properties, colored, low elongation, low creep, highly crystalline, recyclable and any combination thereof. When combined the resulting thermoplastic can be formed into a matrix material without having to rely upon a resin or matrix material for creation.


The use of the reinforcement material, including thermoplastics, can provide for the resulting fiber combination of a reinforcement fiber and second fiber, much as a low melt polyester to provide for properties that include the ability to reduce part fabrication timeline, low moisture uptake, toughness and damage resistance, no refrigeration or autoclave needed for large structure fabrication, ability to re-form parts, low void content, simplified manufacturing processes and methods, less wastage, support for automated manufacturing methods and any combination thereof.


Further benefit of the present fiber and fiber combination include less expensive raw material cost when compared to thermosets, lower processing temperatures than those current in use, improved thermoplastic composite processing options, and less expensive metal tools for processing, reduce or minimize structural failures, have high impact resistance, have a lighter weight than comparable fibers and fiber combinations, have vibration damping properties, dielectric properties, chemical resistance, and any combination.


The resulting fiber and fiber combination(s) of the present invention can provide for higher performance thermoplastic material, lower temperature processing, and improved physical and performance properties over existing technologies. In one embodiment, the reinforcement fiber can be combined with a low melt fiber wherein the low melt fiber can include a denier of less than about 1 grams/60 meters and the crystallinity according to WAXS measuring techniques can be greater than 50%. The reinforcement fiber can be taken from a group consisting of a polyolefin, a mixture of two or more polyolefins, a polyolefin having a nucleating agent. The low melt fiber can be a multifiber structure and can have a denier between about 10 Denier to 1000 Denier, but is not limited to this range. The reinforcement polyolefin can be polypropylene, polyethylene, polybutylene and can be a multifilament yarn. The reinforcement fiber can be any polymeric composition comprising propylene monomers, alone or mixture with other polyolefins, deniers, or other monomers including ethylene, butylene, and the like. The reinforcement fiber can have melt flow indices between about 0.2 and about 50 can be utilized in forming the disclosed multifilament yarns. The reinforcement fiber can be made with the process shown in U.S. Pat. No. 7,074,483 which is incorporated by reference.


In one embodiment, the present invention is created by combining two or more fibers into a resulting fiber. The combination can be accomplished by plying, twisting, air texturing, air entanglement, yarn made via the coating extrusion process, whereas the coated area has a lower melt than the core and the reinforcement fiber and the like. The first fiber can be a reinforcement fiber including a continuous filament yarn based on polypropylene resin. This fiber can be a UV-stabilized, opaque fiber with a general-purpose fiber sizing. The yarns are porous and generally cylindrical in form and are chemically stable. In one embodiment, the reinforcement fiber is made using a method that can include filament winding, weaving, knitting, braiding, and multiaxial construction. The reinforcement fiber, in embodiment, can be unwound for use. In one embodiment, the reinforcement fiber can include the following properties shown in Table 1:












TABLE 1





Properties
Values
Unit
Test Method







Weight per unit
1880 ± 8.00%
Denier
ASTM D1907


length


Filaments per tow
150
Count



Yield
2375
yd/lb



Breaking strength
39.4 (Min = 34.20)
lbF
ASTM D885


Tenacity
9.50 (Min = 08.50)
g/denier
ASTM D885


Elongation at
11.00 (Max = 12.00)
%
ASTM D885


break


Elastic modulus
170 (Min = 160)
g/denier
ASTM D885


Creep at 20%
3.20
%
1 year, RT


UTS


Maximum
150
° C.
DSC Data


Processing


Temperature


Dielectric
2.20
Dk



constant


Dielectric loss
0.0009
Df



Using Density
0.84
g/cc










In one embodiment, the second fiber can be a low melt fiber with a melting point that can be below 140° C. so that when heat is applied, the reinforcement fiber shrinkage is reduced or eliminated. The second fiber can include a high flow rate at low temperature including high flow rate at 110° C. or less. One or multiple low melt fiber(s) that can be used as the second fiber can include physical properties that are shown in TABLE 2.













TABLE 2





Item
Unit
Results
Min Value
Max Value



















Denier
DTex
219.5
219.3
219.8


Tenacity
CN/DTex
2.55
2.43
2.66


Elongation
Percentage
68.8
65.31
73.6.


60 Degree Dry
Percentage
8.08
8.03
8.11


Thermal


Shrinkage









The reinforcement fiber and the low melt fiber can be combined to form the resulting fiber by taking the reinforcement fiber and the low melt fiber, arranging them in an axial direction. The two or more fibers are then plied. In one embodiment, the reinforcement fiber and the low melt fiber are individually twisted, which can result in a ply twisted fiber. Prior to twisting or plying, loose fibers can be coalesced into a fiber strip. After twisting or plying, the outer fibers can be compressed towards the inner layers to create centripetal pressure, which can result in the strand gaining friction along the direction of the fiber elongation. Twisting or plying can create compact yarn structures, which have improved resistance to damage occurring from lateral external forces.


Once twisted, the outer fiber can be twisted back in an inclined spiral and the fibers twisted and deformed as the yarns are held together. The process can change the structural form and mechanical and physical properties of the fibers, as shown in FIG. 1.


In one embodiment, there is a wrap angle that is defined by the yarn strip where the fibers exert centripetal pressure on the yarn strip. The greater the wrap angle, the greater the centripetal pressure applied. Therefore, the greater the angle of encirclement, the greater the centripetal pressure. The centripetal pressure compresses or squeezes the outer fibers towards the inner layer that can result in a tightness of the yarn strip and results in friction between the fibers. Therefore, the structural form, physical properties, and mechanical properties of the yarn strip are modified. In one embodiment, the plying or testing process includes two reinforcement fibers and three low melt fibers that are combined to a yarn. The twist can be applied at 1.0-2.5 twist per inch S or Z at 40.0-100 twists per meter, but is not limited to this range. The resulting fiber can include a denier of 3080, a tensile strength of 38 lbs, and a tenacity of 5.59 g/d. The tensile strength can be in a range of 30 to 40 lbs. The tenacity can be in a range of 4.50 to 6.50 g/d in one embodiment.


In one embodiment, another next step in the process includes joining the plied yarn into a fabric that can be used in an application. The fiber can be woven into fabric form, that can consist of 20%-80% or 80-20 percent respectively of reinforcement fiber and low melt fiber. During this process, the low melt fiber can melt under heat and pressure to become the matrix of the resulting fiber, whereas reinforcement fiber retains as a reinforcement. The weaving process can be illustrated by reference to FIG. 2. In one embodiment, reinforcement fiber is supplied to a weaving process on bobbins on a creel and as filling yarns at 200. The low melt material, such as filaments or fiber, can be provided as 202 and then woven into a pattern at 204. The fabric can be woven on a loom (weaving machine). The weave can be a plain weave or other pattern. Heat can be applied at a temperature higher than the melt temperature of the low melt material but lower than the melt temperature of the core of the reinforcement material at 206 allowing the materials to combine. In one embodiment, the manufacturing specifications shown in Table 3 are used:












TABLE 3







Target
Tolerance (+/−)




















EPI
9.6
0.5



PPI
9.6
0.5



Width (Inches)
50
1



Gauge (Inches)
0.033
0.005



Weight (oz/yd2)
8
0.5



Weave
Plain



Edges
Leno (fringe)



Length (Yards)
100
50







Warp 1880 denier with 200 denier 6 ply Low Melt Polyester



Fill 1880 denier with 200 denier 6 ply Low Melt Polyester






Once the fabric is provided, the fabric can be thermoformed using an exemplary process that includes the steps referred to in FIG. 3. The composite layup techniques or Peel ply the part prior to bagging is used at 300. Once bagged, the collection is placed in a heater at 302. Heating the heater and the collection can be at about 10° C. per minute up to about 150° C. at 304. With this process, the collection can heat soak into the thickness at approximately 7 min per ⅛ inch thickness. The dwell time can be at 150° C. after a heat soak for about 10 minutes at 306. The heat is removed, and the collection is allowed to cool below 50° C. at 308 before removing the collection at 310. This process results in the collection or composition resulting in a desired part.


In one embodiment, the following layup schedule is used as shown in Table 3.












TABLE 3








Time Start ramp up
12:50 PM
28 mins



Time Dwell
 1:18 PM
10 mins



Time Cool down
13:28
15 mins


















Pressure
Pressure
Pressure




PLY
Orientation
Vac Pump
Vac Set
Absolute
Temp
Humidity





940/2Black Innegra 200/6
0/90
27 inhg
27 inhg
993 mb
140 C.
100%


low Melt Poly








940/2Black Innegra 200/6
0/90
27 inhg
27 inhg
993 mb
140 C.
100%


low Melt Poly








940/2Black Innegra 200/6
0/90
27 inhg
27 inhg
993 mb
140 C.
100%


low Melt Poly








200/3 Low Melt Poly
0/90
27 inhg
27 inhg
993 mb
140 C.
100%


940/2Black Innegra 200/6
0/90
27 inhg
27 inhg
993 mb
140 C.
100%


low Melt Poly








940/2Black Innegra 200/6
0/90
27 inhg
27 inhg
993 mb
140 C.
100%


low Melt Poly








940/2Black Innegra 200/6
0/90
27 inhg
27 inhg
993 mb
140 C.
100%


low Melt Poly








200/3 Low Melt Poly
0/90
27 inhg
27 inhg
993 mb
140 C.
100%


940/2Black Innegra 200/6
0/90
27 inhg
27 inhg
993 mb
140 C.
100%


low Melt Poly








940/2Black Innegra 200/6
0/90
27 inhg
27 inhg
993 mb
140 C.
100%


low Melt Poly








940/2Black Innegra 200/6
0/90
27 inhg
27 inhg
993 mb
140 C.
100%


low Melt Poly








940/2Black Innegra 200/6
0/90
27 inhg
27 inhg
993 mb
140 C.
100%


low Melt Poly









The resulting fabric can exhibit physical properties that can include those shown in FIGS. 4A to 4E. The resulting material has application for manufacturing part and other structures in industries that include automobile parts, sports equipment, aerospace parts, suitcases, battery enclosures for electric vehicles, impact sheets, ballistic applications, civil constructions, marine applications, plastic equipment (storage boxes, etc.).


In some embodiment, the reinforcement fiber can be combined with carbon, glass, aramid, and any combination in conjunction with a low melt fiber


The methods in which the reinforcement fiber can be added or combined with a second fiber for a resulting fabric can include adding a third fiber during the plying process that can create a single plied yarn which can be used for weaving. For example, carbon fiber and low melt polyester can be combined at the yarn level and woven. Further, a second reinforcement fiber can be added during the weaving process and can include using different wrap and fill fiber. Further, additional fibers and fabrics can be used in the layup schedule.


In one testing example, panels of a resulting fabric were created having difference layup order with the fiber orientation in each panel being orthogonal. Three tensile samples were taken from each panel. The tabs were cut from a glass fiber and epoxy composite and the area of the sample in which the tab is bonded was sanded lightly to introduce roughness and improve bonding to the low surface energy polymer samples. The tabs were rounded at the inner ends to limit stress concentrations and the samples were attached to the tabs. The samples were “double tabbed” to thicken the samples suitably for clamping in the tensile test machine.


In one tensile testing example, the test was performed using an MTS 647 Hydraulic Wedge Grips tensile machine with a test rate of 2 mm/min. An extensometer was used to measure strain over the first 0.005 mm/mm. Tensile modulus was calculated from 0.001 to 0.003 mm/mm strain. The results are shown in FIGS. 5A-B and Table 4.

















TABLE 4









Average


Average






Tensile
Tensile
Tensile
Tensile
Tensile
Tensile



Sample
Max
Strength
Strength
Strength
Modulus
Modulus
Modulus


Panel
#
Load (N)
(MPa)
(MPa)
COV (&)
(GPa)
(GPa)
COV (%)























1
1
13424.92
123.19
118.51
3.46
1.79
1.66
10.15



2
13050.10
115.57


1.73





3
13087.63
116.78


1.47




2
1
11672.55
130.72
125.79
5.85
2.12
1.98
9.19



2
11965.73
129.28


2.03





3
11259.58
117.37


1.77




3
1
11469.78
121.60
123.47
2.95
2.44
2.03
17.64



2
11994.96
121.15


1.76





3
11994.95
127.67


1.89




4
1
11701.48
129.68
124.37
4.06
1.84
1.67
9.35



2
11672.25
123.82


1.66





3
11469.67
119.62


1.53









In one testing example, panels were taken from the resulting fabric and flexure testing was performed using an MTS Three Points Bending machine (Instron model 1331) with a test rate of 1.9 mm/min. The span length of flexure testing is 70 mm. The results are shown in FIGS. 6A-B and Table 5.




















TABLE 5









Peak

Avg.
Strength


Avg
Modulus




Width
Thickness
Load
Strength
Strength
STD Dev.
Slope
Modulus
Modulus
STD Dev.


sample
ID
(mm)
(mm)
(N)
(MPa)
(MPa)
(MPa)
(N/mm)
(GPa)
(GPa)
(GPa)


























#1
1-1
12.44
4.44
42.58
18.23
18.63
0.34
12.90
1.02
1.00
0.08



1-2
12.37
4.43
43.63
18.86


13.49
1.08





1-3
12.32
4.40
42.58
18.78


11.24
0.92




#2
2-1
13.46
3.71
34.17
19.33
18.53
1.00
8.19
1.02
1.02
0.12



2-2
13.51
3.81
35.22
18.85


9.86
1.13





2-3
13.47
3.82
32.59
17.41


7.86
0.90




#3
3-1
12.66
3.79
37.32
21.54
20.88
1.65
9.22
1.15
1.16
0.12



3-2
12.78
3.70
36.79
22.10


9.65
1.28





3-3
12.77
3.87
34.69
19.01


9.03
1.04




#4
4-1
12.21
3.88
22.08
12.64
13.78
1.07
5.93
0.72
0.73
0.08



4-2
12.30
3.74
24.18
14.75


6.10
0.81





4-3
12.62
3.76
23.65
13.94


5.18
0.66









In one testing example, un-notched samples and notched samples were prepared from the results fabric. Izod Impact testing was performed using a Tinius Olsen Izod impact test machine and in accordance with ASTM D256-10. The result is shown in FIGS. 7A-B and Table 6.















TABLE 6






Sample
Break
Strength
Width
Thickness
Method of


Panel
#
(J)
(kJ/m2)
(mm)
(mm)
Break





















1
1
3.0168
57.6
11.82
4.43
NB, slipped


1
2
2.3871
42.7
12.36
4.52
NB


1
3
2.1734
39.6
12.32
4.45
NB


2
1
2.1405
40.5
13.55
3.90
NB


2
2
1.8738
36.4
13.53
3.80
NB


2
3


13.30
3.68



3
1
1.7488
34.4
12.79
3.97
NB


3
2
2.1045
42.2
12.53
3.98
NB


3
3
1.9708
38.5
12.83
3.98
NB


4
1
1.5128
30.9
12.88
3.80
NB


4
2
1.5128
31.6
12.82
3.73
NB


4
3
1.4017
29.0
11.90
4.06
NB









In one tensile testing method an Instron Model 1331 frame tensile machine was used having a test rate of 2 mm per minute. An extensometer was used to measure strain over the first 0.005 mm/mm. Tensile modulus was calculated from 0.001 to 0.003 mm/mm strain. The sample testing results as shown in FIGS. 8A and 8B. The results of the sample shown as the testing sample on FIGS. 8A and 8B compared with a sample (numbers 1 through 4) having a high-performance fiber, a high modulus material, a synthetic fiber made from polyolefin polypropylene, an olefin fiber, a hybridized yarn, a high strength to weight ratio, polyolefin, and any combination. In one example, the high-performance fiber can be a polypropylene yarn and can exhibit any of a high modulus, high tenacity, and a unique crystalline structure for multifilament polyolefin yarn. The high-performance fiber can be a monofilament fiber as well as multifilament yarn formed from various fibers such as polyolefin. The polyolefin can be a filament, fiber or yarn and can be polypropylene, copolymer, a mixture of two or more polyolefins. One of the filaments in a yarn can have a greater than 50% crystallinity when measured using wide-angle x-ray scattering (WAXS). One filament in a yarn can have a ratio of equatorial intensity to meridional intensity greater than about 1.0 according to measurements using small angle x-ray scattering (SAXS). One filament can have a ratio of equatorial intensity to meridionals intensity can be greater than about 3.0.


As shown, the tensile strength of the sample was found to be in the range of 210 to 239 MPa with an average of 230.08 MPa according to some tests. As shown the module of the sample was found to be in the range of 5.10 GPa to 6.4 GPa with an average of 5.55 according to some tests. Further testing results using the frame tensile machine as shown in FIG. 9.


A flexure test was performed using an MTS Three Points Bending machine, such as the Instron model 1331 with a test rate of 1 mm per minute. The span length of flexure testing was 28 mm. Using this flexure testing, the results as shown in FIGS. 10A and 10B. The flexure strength was compared with sample (numbers 1 through 4) as described above and found to have a flexure in the range of 88 to 96 MPa and 92.4 MPa as an average of some tests. The flexure module was compared with samples and found to be in the range of 3.10 GPa to 3.40 GPa and 3.2 GPa as an average of some tests. The test sample can be a thin panel. Further testing results as shown in FIGS. 11 and 12.


Referring to FIG. 13, an Izod Impact testing system, including a Tinius Olsen Izod impact test machine with a pendulum weight of 7.49 J with results shown as shown in FIGS. 14 and 15, use used to measure the impact resistance of the sample. In one embodiment planes C and D can be parallel to within a range of 0.025 mm (0.001 inches) and can be over a distance of 25 mm (1 inch). Testing was performed in accordance with testing standard ASTM D256-10. Panels 1 through 4 include the reinforcement material as described above with the testing sample being the comparative sample. The comparative panels 1 through 4 and the testing sample as shown in FIGS. 16A-B, 17 and 18 comparing panels 1 through 4 with the test sample. Both notched samples and un-notched samples were tested, and the results shown.


The invention can be configured so that it does not undergo chemical property changes when heated or cooled, even when heated and cooled multiple times, thereby allowing for improved recycling properties. Reference will now be made in detail to various embodiments of the invention, one or more examples of which are set forth below. Each embodiment is provided by way of explanation of the invention, not limitation of the invention. In fact, it will be apparent to those skilled in the art that various modifications and variations can be made in the present invention without departing from the scope or spirit of the invention. For instance, features illustrated or described as part of one embodiment, can be used in another embodiment to yield a still further embodiment. Thus, it is intended that the present invention cover such modifications and variations as come within the scope of the appended claims and their equivalents.

Claims
  • 1. A reinforced fabric comprising: a fiber composite having a reinforcement fiber and a low melt fiber wherein the low melt fiber is heated to above a low melt melting point forming a fiber composite wherein a reinforcement fiber melting point is higher than the low melt melting point; and,a coating on a coated area of the reinforcement fiber wherein the coated area includes a lower melt temperature than a core of the reinforcement fiber.
  • 2. The reinforced fabric of claim 1 wherein the reinforced fiber is a multifilament yarn having a polyolefin filament.
  • 3. The reinforced fabric of claim 2 wherein the polyolefin filament is a polypropylene filament.
  • 4. The reinforced fabric of claim 3 wherein the polypropylene filament has a crystallinity greater than 50% when measured using wide-angle x-ray scattering.
  • 5. The reinforced fabric of claim 1 wherein the fiber composite is hydrophobic.
  • 6. The reinforced fabric of claim 1 wherein the fiber composite includes micro voids.
  • 7. The reinforced fabric of claim 1 wherein the fiber composite can include material taken from the group consisting of carbon, glass, aramids, basalt, and any combination.
  • 8. The reinforced fabric of claim 1 wherein the reinforcement fiber can have a physical property taken from the group consisting of a denier of less than about 1 grams/30 meters, a filament drawn at a draw ratio of greater than about 6, a modulus greater than about 40 grams/denier, and any combination thereof.
  • 9. The reinforced fabric of claim 1 wherein a reinforcement fiber amount compared is in a range of 10% to 90% of a composition by volume.
  • 10. The reinforced fabric of claim 1 wherein a reinforcement fiber amount compared is in a range of 10% to 90% of a composition by weight.
  • 11. The reinforced fabric of claim 1 wherein the low melt fiber is a thermoplastic fiber.
  • 12. The reinforced fabric of claim 1 wherein the fiber composite is a combination of the reinforcement fiber woven with the low melt fiber prior to an application of heat to melt the low melt fiber.
  • 13. The reinforced fabric of claim 1 wherein the fiber composite is adapted to be included in a lay-up process for manufacturing an article wherein one of a layer is the fiber composite.
  • 14. The reinforced fabric of claim 13 wherein the lay-up process includes a ramp up rate of 10 degrees per minute or less to 140° C.
  • 15. The reinforced fabric of claim 13 wherein the lay-up process includes a dwell time of 10 minutes or more at 150° C.
  • 16. The reinforced fabric of claim 13 wherein the lay-up process includes a cooling cycle at or below 50° C.
  • 17. The reinforced fabric of claim 1 wherein the fiber composite has a denier in a range of 300 to 3250.
  • 18. The reinforced fabric of claim 1 wherein the fiber composite has a tensile strength in a range of 30 to 40 lbs.
  • 19. The fiber composite of claim 1 wherein the fiber composite has a tenacity in a range of 4.50 to 6.50 grams per denier.
  • 20. A reinforced thermoset fabric comprising: a reinforcement fiber;a low melt fiber integrated with the reinforcement fiber using a method of plying, twisting, air texturing, air entanglement, co-weaving, co-mingling, and any combination thereof;wherein the reinforcement fiber includes a coating applied to a coated area of the reinforcement fiber during an extrusion process;whereas the coating has a lower melt temperature than the reinforcement fiber; and,whereas the low melt fiber is adapted to melt upon an application of a heat to form a fiber composite wherein a melting point of the reinforcement fiber is higher than an operational temperature resulting from the application of the heat.
  • 21. The reinforced thermoset fabric of claim 20 wherein the low melt fiber has a melting point of less than 140° C. and the reinforcement fiber has a melting point of more than 140° C.
  • 22. The reinforced thermoset fabric of claim 20 wherein a reinforcement fiber amount is more than twenty percent of a composition by volume.
  • 23. The reinforced thermoset fabric of claim 20 wherein a reinforcement fiber amount is more than twenty percent of a composition by weight.
  • 24. The reinforced thermoset fabric of claim 20 wherein the reinforcement fiber can include a physical property taken from the group consisting of a denier of less than about 300 grams/9000 meters, a filaments drawn at a draw ratio of greater than about 6, a modulus greater than about 40 grams/denier, a ratio of equatorial intensity to meridional intensity greater than about 1.0 according to SAXS measuring techniques, a crystallinity greater than 50% when measured using wide-angle x-ray scattering and any combination thereof.
  • 25. A fabric material comprising: a reinforcement fiber;a low melt fiber combined with the reinforcement fiber using a method of plying, twisting, air texturing, air entanglement, co-weaving, co-mingling, and any combination thereof;whereas a coated area has a lower melting point than a core of the reinforcement fiber and,where the combination of the reinforcement fiber and the low melt fiber is heated to melt the low melt fiber to form a fiber composite wherein a melting point of the reinforcement fiber is higher than an operational temperature resulting from an application of a heat.
  • 26. The fabric material of claim 25 wherein the low melt fiber is combined with the reinforcement fiber using a method of a coating process.
  • 27. The fabric material of claim 26 wherein the method is a coating extrusion process.
RELATED APPLICATIONS

This application is a United States Patent Application claiming priority in U.S. Provisional Patent Application Ser. No.: 63/385,026 filed Nov. 27, 2022 and incorporated by reference.

Provisional Applications (1)
Number Date Country
63385026 Nov 2022 US