AN ABRASION RESISTANT MATERIAL AND METHOD OF CONSTRUCTION
20170251734 · 2017-09-07
Assignee
Inventors
Cpc classification
B32B27/12
PERFORMING OPERATIONS; TRANSPORTING
B32B5/26
PERFORMING OPERATIONS; TRANSPORTING
B32B2307/726
PERFORMING OPERATIONS; TRANSPORTING
F41H5/0485
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B32B7/12
PERFORMING OPERATIONS; TRANSPORTING
B32B2307/718
PERFORMING OPERATIONS; TRANSPORTING
B32B3/085
PERFORMING OPERATIONS; TRANSPORTING
B32B5/22
PERFORMING OPERATIONS; TRANSPORTING
B32B2307/54
PERFORMING OPERATIONS; TRANSPORTING
B32B2262/062
PERFORMING OPERATIONS; TRANSPORTING
A41D13/0002
HUMAN NECESSITIES
B32B5/028
PERFORMING OPERATIONS; TRANSPORTING
F41H5/0492
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B32B2307/724
PERFORMING OPERATIONS; TRANSPORTING
B32B2262/02
PERFORMING OPERATIONS; TRANSPORTING
International classification
A41D13/00
HUMAN NECESSITIES
B32B5/26
PERFORMING OPERATIONS; TRANSPORTING
B32B7/12
PERFORMING OPERATIONS; TRANSPORTING
B32B5/06
PERFORMING OPERATIONS; TRANSPORTING
B32B27/12
PERFORMING OPERATIONS; TRANSPORTING
Abstract
An abrasion resistant material for use in the fabrication of protective garments that has at least two layers, a first layer and a second layer, wherein the first layer is the layer that is exposed to and engages with the abrasive surface, such as a road surface. The second layer comprises of substantially high tensile and burst strength so as to act as a protective layer which covers or is at least located closest to the skin of the wearer. The first layer has a plurality of abrasion resistant members dispersed throughout the first layer that act to absorb the bulk of any abrasion force and reduce the exposure and degradation of the second layer
Claims
1. An abrasion resistant material for use in the fabrication of protective apparel comprising: at least a first layer; a plurality of abrasion members dispersed throughout the first layer; at least a second layer underlying the first layer, the second layer having substantially high tensile and burst strength; wherein the abrasion resistant material is exposed to an abrasive surface and force, the plurality of abrasion members of the first layer are adapted to engage with the abrasive surface and absorb the abrasive force, thereby minimizing exposure of the second layer to the abrasive surface and force and increasing resistance of the abrasion resistant material to tensile and burst failure.
2. The abrasion resistant material according to claim 1, wherein the plurality of abrasion members protrude beyond a substantially flat plane of the first layer.
3. The abrasion resistant material according to claim 1, wherein the plurality of abrasion members comprise of a plurality of fibres dispersed throughout the first layer.
4. The abrasion resistant material according to claim 1, wherein the plurality of abrasion members comprise of fibres selected from the group consisting of woven fibres, looped fibres, knitted fibres and combinations thereof
5. The abrasion resistant material according to claim 1, wherein the first layer is interconnected with the second layer.
6. The abrasion resistant material according to claim 5, wherein the first layer is interconnected with the second layer by a woven means comprising at least one interlocking thread passing through both the first and second layers.
7. The abrasion resistant material according to any one of claim 1, wherein the first and second layers are interconnected by an adhesive means.
8. The abrasion resistant material according to claim 1, wherein the first and second layers are chemically bonded.
9. The abrasion resistant material according to claim 1, wherein the first and second layer are thermally bonded.
10. The abrasion resistant material according to claim 1, wherein the first layer comprises a flexible textile material.
11. The abrasion resistant material according to claim 1, wherein the second layer comprises a flexible textile material.
12. The abrasion resistant material according to claim 1, wherein the first layer comprises a mesh so as to enable permeability of moisture and vapour.
13. The abrasion resistant material according to claim 1, wherein the second layer comprises a mesh so as to enable permeability of moisture and vapour.
14. The abrasion resistant material according to claim 1, wherein the abrasion resistant material comprises at least one outer layer overlaying the first layer.
15. The abrasion resistant material according to claim 14, wherein the outer layer comprises of a flexible textile material.
16. The abrasion resistant material according to claim 14, wherein the outer layer comprises a flexible polymeric material.
17. A method of construction of an abrasion resistant material according to claim 1, wherein the method comprises the steps of: a. selecting a first layer of material, the first layer having a plurality of abrasion members dispersed throughout the first layer; b. selecting a second layer of material, the second layer having substantially high tensile and burst strength; c. bonding the first and second layers together; and wherein the abrasion resistant material is exposed to an abrasive surface and force, the plurality of abrasion members of the first layer are adapted to engage with the abrasive surface and absorb the abrasive force, thereby minimizing exposure of the second layer to the abrasive surface and force and increasing resistance of the abrasion resistant material to tensile and burst failure.
18. The abrasian resistant material of claim 1, wherein the combination of the at least a first layer; a plurality of abrasion members dispersed throughout the first layer; at least a second layer underlying the first layer, the second layer having substantially high tensile and burst strength, is a synergistic combination.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0048] For a better understanding of the present invention and associated method of use, it will now be described with respect to the preferred embodiment which shall be described herein with reference to the accompanying drawings wherein:
[0049]
[0050]
[0051]
[0052]
[0053]
[0054]
[0055]
DETAILED DESCRIPTION OF THE INVENTION
[0056] Referring to
[0057] The abrasion resistant material 10 is formed of at least two layers: a first layer 20 and a second layer 30, wherein the first layer 20 is the layer that is exposed to and engages with the abrasive surface, such as a road surface. The second layer 30 comprises of substantially high tensile and burst strength so as to act as a protective layer which covers or at least located closest to the skin of the wearer.
[0058] The first layer 20 is adapted to absorb the abrasive force and energy of the initial impact and minimize the exposure of the second layer 30 to the abrasive surface without significantly reducing the structural integrity of the second layer 30 and thereby increasing the resistance of abrasion resistant material 10 to failure such as bursting, tearing, ripping and/or shearing during abrasion and protecting the wearer from significant injury. The interaction of the first layer 20 with the abrasive surface on the initial impact is particularly significant as it enables the first layer 20 to be exposed to and distribute the bulk of the abrasive force and thereby minimise the exposure of the second layer to the abrasive force. This interaction is achieved via the first layer 20 comprising of a plurality of abrasion members 40 dispersed throughout the first layer 20. The plurality of abrasion members 40 serve to absorb the bulk of the abrasion force when the abrasion resistant material 10 is exposed to an abrasive surface.
[0059] The plurality of abrasion members 40 of the first layer 20 protrude outwardly from the substantially flat plane of the first layer 20 to form the abrasion resistant first layer 20. Accordingly, on exposure to the abrasive force, the plurality of abrasion members 40 are adapted to degrade so as to minimises the exposure and degradation of the second layer 30. As the second layer 30 maintains sufficient structural integrity, overall the resistance of the abrasion resistant material 10 to tensile and burst failure is increased and serves to protect the wearer from significant injury.
[0060] To assist the resistance of the abrasion resistant material 10 to tensile and burst failure, the second layer 30 is formed of a material boasting a substantially high tensile and burst strength.
[0061] The first 20 and second 30 layers of the abrasion resistant material 10 can comprise of a flexible textile material, having substantially high tensile and burst strength, including but not limited to polyester, poly amines, polypropylene, polyethylene (including low density, high density and ultra high molecular weight), aramids (para and meta aramids) for example, Kevlal® or Twaron®, liquid crystal polymers, polybenzoxazole (PBO).
[0062] Advantageously, the first 20 and second 30 layers being of flexibile and pliable material enhances the versatility of the abrasion resistant material 10 in the manufacture of various types of clothing and apparel, including but not limited to protective apparel for motorcyclists and cyclists. Also, the flexbility of the abrasion resistant material 10 promotes a significant degree of comfort for the wearer, whereby the movement of the wearer is not substantially limited compared to that of conventional materials that are often particularly stiff or thick.
[0063] Additionally, the first 20 and second 30 layers may be formed of a mesh. The mesh configuration assists to promote the breathability of the abrasion resistant material 10 such that there is a degree of permeability within the abrasion resistant material 10 for moisture and vapour. The breathability of the abrasion resistant material 10 assists to promote comfort to the wearer.
[0064] A non-woven textile material could be used as a component of the first 20 and second 30 layers. The abrasion resistance of a non-woven textile material is moderate as the amount of surface fibres involved in abrasion is moderate.
[0065] The plurality of abrasion members 40 may comprise of a plurality of fibres, such as individual fibres, dispersed throughout the first layer 20, arranged in such a manner that a portion of the plurality of fibres protrudes from the substantially flat plane of the first layer 20 so as to be exposed to the abrasive surface and force.
[0066] Preferably, the plurality of abrasion members 40 comprise of fibres selected from the group consisting of woven fibres, looped fibres, knitted fibres, non-woven fibres and combinations thereof. It has been found that the configuration of woven fibres, looped fibres, knitted fibres, non-woven and combinations thereof, provides a greater surface area and increases the interaction of the plurality of abrasion members 40 with the abrasion surface. The greater surface area of the woven fibres, looped fibres, knitted fibres and combinations thereof, assist to distribute the abrasion force and load. Effectively, as the pressure distribution is over a larger surface area, the amount of abrasion force per fibre is lower resulting in a slower abrasion of the first layer 20 of the abrasion resistant material 10.
[0067] With reference to
[0068] Referring to
[0069] The distal tips of the peaks 80 of the woven configuration 50 are exposed to and come into contact with the abrasion surface during initial contact causing high loading on the individual fibres 90 forming the peaks 80 as the ratio of peak area to valley area is small. Once a percentage of the peak 80 is abraded away, the strength of the individual fibres 90 and subsequent strength of the first layer 20 is compromised resulting in fabric failure via tear or burst. Accordingly, this woven configuration 50 is not well suited but can be used as a part of the two layer technology.
[0070]
[0071] It would be readily appreciated that the knitted jersey configuration illustrated in
[0072] Referring now to
[0073] In particular, the plurality of abrasion members 40 having a smaller loop width and high loop volume, provides better abrasion resistance compared to a larger loop width and/or a low loop volume, as there are more loop structures 110 to interact with the abrasion surface and distribute the abrasion load. The first layer 20 having a plurality of abrasion members 40 formed of the knitted loop pile configuration 70 is very suited to abrasion resistance and is a two layer structure in its own right. The knitted loop pile configuration 70 could also include but not limited to, a woven terry fabric or as a loop pile or cut pile tufted knitted, woven or non woven fabric.
[0074]
[0075]
[0076] Alternativelty, the first 20 and second 30 layers may be chemically or thermally bonded to one another using any suitable means known within the art including but not limited toepoxies, melt polymer films, meltable membranes, meltable fibres, meltable sheath core/sheath fibres.
[0077]
[0078]
[0079]
[0080] Wherein the additional layer 180 overlay the first layer 20 it serves to resist the initial impact force reducing the force transferred to the first 20 and second 30 layers. The additional layer 180 would possess sufficient structural strength and resistance to impact abrasion induced failure including but not limited to tearing, bursting, ripping, tensile failure and shear failure either by the abrasion resistant material 10 itself or by the abrasion resistant material 10 in combination with additional layer 180.
[0081] The additional layer 180 can be formed of one or more textile, polymer or leather layers, or combinations thereof.
[0082] The following test examples illustrate the present invention. They are presented for illustrative purposes only, and should not be construed as limiting the invention in any way.
Example 1
[0083] This example illustrates the benefit that a correctly designed first layer provides in avoiding burst failure or the underlying second layer. A 230 g/m.sup.2double jersey 100% para-aramid fabric is placed under a 350 g/m.sup.2 100% cotton denim fabric to form a composite abrasion resistant material. When tested for abrasion resistance according to EN 13634:2010, the composite abrasion resistant material has a mean abrasion resistance of 4.01 and a standard deviation of 0.42 seconds.
[0084] The same 230 g/m.sup.2 double jersey 100% para-aramid fabric is placed under a under a 420 g/m.sup.2 knitted unbrushed fleecy loop pile 100% cotton fabric to make a composite composite abrasion resistant material. When tested for abrasion resistance according to EN 13634:2010, the composite abrasion resistant material has a mean abrasion resistance of 1.06 and a standard deviation of 0.23 seconds. The double jersey 100% para-aramid fabric is protected from bursting by the 100% cotton denim fabric so failure is by abrasion where the stretch of the knitted unbrushed fleecy loop pile outer fabric allows for stretch to occur in the double jersey 100% para-aramid fabric causing bursting and then rapid failure in abrasion.
Example 2
[0085] This example illustrates the synergistic effect of the first and second layers forming the abrasion resistant material, wherein the first and second layers combine to provide higher abrasion resistance compared to the addition of the abrasion resistance of each of the first and second layers tested by itself.
[0086] In the first part of this experiment a 350 g/m.sup.2 100% cotton denim fabric has a mean abrasion resistance of 0.41 and a standard deviation of 0.07 seconds and fails due to abrasion fatigue. A 400 g/m.sup.2 knitted terry loop pile 80% para-aramid/20% ultra high molecular weight polyethylene fabric has a mean abrasion resistance of 1.72 and a standard deviation of 1.13 seconds and fails due to a combination of fabric burst and abrasion fatigue.
[0087] A composite combination of these two fabrics with the 100% cotton denim fabric in contact with the abrasion surface and the knitted terry loop pile 80% para-aramid/20% ultra high molecular weight polyethylene fabric in contact with the skin has an abrasion resistance of 8.07 and a standard deviation of 1.01 seconds and fails due to abrasion fatigue. This result is over three times larger than the sum of the individual abrasion resistances of each fabric. This increased abrasion resistance is because the 100% cotton denim layer protects the composite structure from fabric burst.
[0088] This same effect is seen with different protective layers and in the second part of this experiment a 300 g/m.sup.2 100% cotton denim cargo fabric that had a mean abrasion resistance of 0.30 and a standard deviation of 0.04 seconds and fails due to abrasion fatigue. A 430 g/m.sup.2 knitted unbrushed fleecy loop pile 80% para-aramid/20% ultra high molecular weight polyethylene fabric had a mean abrasion resistance of 1.89 and a standard deviation of 0.20 seconds and fails due to a combination of fabric burst and abrasion fatigue. A composite combination of these two fabrics with the 100% cotton denim cargo fabric in contact with the abrasion surface and the knitted unbrushed fleecy loop pile 80% para-aramid/20% ultra high molecular weight polyethylene fabric in contact with the skin had an abrasion resistance of 4.72 and a standard deviation of 0.57 seconds and fails due to abrasion fatigue. This result is over twice as large as the sum of the two individual abrasion resistances.
Example 3
[0089] This example illustrates the benefit that a correctly designed abrasion resistant material provides in avoiding abrasion failure. Specifically this example shows the benefit of a well designed composite abrasion resistant material. All of the abrasion resistant materials tested in this example were tested for abrasion resistance according to EN 13634:2010. Each abrasion resistant material was tested having the same first layer which was a 470 g/m.sup.2 100% cotton denim fabric that had a mean abrasion resistance of 0.85 and a standard deviation of 0.19 seconds. This first layer was utilized in all tests to avoid bursting of the underlaying second layer influencing the results.
[0090] A single layer protective liner such as a 260 g/m.sup.2 100% para-aramid plain weave fabric had a mean abrasion resistance of 1.96 and a standard deviation of 0.30 seconds and failed due to abrasion. The protective layer wears through absorbing energy but because it is only a single layer it fails by burst or tearing once a proportion of the protective fibres are worn away. This results in a very low abrasion resistance time. This failure mechanism is the same for a single layer 280 g/m2 100% para-aramid twill weave fabric. It had a mean abrasion resistance of 2.03 and a standard deviation of 0.09 seconds and failed due to abrasion.
[0091] A double layer protective liner such as a 330 g/m.sup.2 100% para-aramid knitted double jersey fabric had a mean abrasion resistance of 3.75 and a standard deviation of 0.56 seconds and failed due to abrasion. The protective fabric layer wears through absorbing energy and the double layer structure increases the abrasion time as one side of the double layer structure can significantly abrade and absorb energy without failing by burst or tearing. The abrasion resistance result is better than a single layer fabric however the double jersey knit structure means that some of the face yarns are present in the back and some of the back yarns are present in the face compromising the fabric integrity when abraded. This fabric would perform better if the abrasion face had no interlocking yarns present from the back layer of the fabric. This failure mechanism is the same for a single layer 340 g/m.sup.2 100% para-aramid knitted double jersey fabric. It had a mean abrasion resistance of 4.01 and a standard deviation of 0.42 seconds and failed due to abrasion.
[0092] A double layer protective liner such as a 400 g/m.sup.2 100% para-aramid terry loop knitted fabric had a mean abrasion resistance of 8.07 and a standard deviation of 1.01 seconds and failed due to abrasion. The loop structure engages with the abrasion surface first and absorbs energy as it is worn away. Once the end of the loop is broken the number of fibres in the now exposed ends of the loop yarns increase the area of interaction with the abrasion surface. This engages far more fabric surface area with the abrasion surface absorbing more abrasion energy and reducing the force on each individual fibre. As the loop yarn is totally independent of the back fabric strength it abrades away without causing fabric bursting or tearing. This loop interaction with the abrasion surface provides a significant increase in abrasion time to failure. This failure mechanism is the same for a single layer 430 g/m.sup.2 100% para-aramid unbrushed fleecy loop knitted fabric. It had a mean abrasion resistance of 5.70 and a standard deviation of 0.11 seconds and failed due to abrasion.
Example 4
[0093] This example illustrates the benefit that an additional layer provides in avoiding premature failure of the inner protective layer. A 400 g/m.sup.2 terry knit 100% para-aramid fabric is placed under a under a 420 g/m.sup.2 knitted unbrushed fleecy loop pile 100% cotton fabric to make a two piece composite fabric. When tested for abrasion resistance according to EN 13634:2010 the composite fabric has a mean abrasion resistance of 3.12 and a standard deviation of 0.63 seconds. When the same 400 g/m.sup.2 terry knit 100% para-aramid fabric is placed under a under 100 g/m2 woven twill 100% cotton fabric in combination with the 420 g/m.sup.2 knitted unbrushed fleecy loop pile 100% cotton fabric to make a three piece composite fabric it has a mean abrasion resistance of 4.63 and a standard deviation of 0.16 seconds. Without the twill fabric present the 100% cotton unbrushed fleecy fabric bursts placing the protective layer under high impact abrasion loads causing premature failure with a high level of variation. When the twill fabric is present the 100% cotton unbrushed fleecy fabric still bursts on impact however the 100% cotton woven twill fabric remains intact and reduces the initial impact abrasion load on the protective layer and results in a higher and more consistent resistance to abrasion result.
[0094] Although the invention has been herein shown and described in what is conceived to be the most practical and preferred embodiment, it is recognized that departures can be made within the scope of the invention, which is not to be limited to the details described herein but it is to be accorded the full scope of the appended claims so as to embrace any and all equivalent devices and apparatus.