1. Field of the Invention
The present invention relates to the art of composite materials, and more particularly, to a composite layer having fasteners incorporated thereon for increased delamination characteristics.
2. Description of the Related Art
Hook and loop type fasteners have been formed on the surface of material substrate sheets within the composite material industry to strengthen the inter-laminar bond between adjacent plies of the composite material to prevent delamination of the plies in this invention. The fasteners also aid in stabilizing the plies to prevent their sliding and dislocation within a wet layup during the layering, rolling, and other molding processes. Additionally, after the curing process, the fasteners increase inter-laminar strength through the mechanical interlocking of the fibers of adjacent plies.
There are some problems encountered with the use of hook and loop fasteners. Often, the fiber plies and the substrate materials are soft and pliable in nature, using such materials as fiberglass, carbon fiber, aramid, and polyester. These materials may be woven or unwoven. The fasteners may be comprised of the same soft material as the substrate or a stiffer material may be used. It is preferred with a pair of mating plies that at least one of the mating fasteners be stiff to a certain level in nature, that is, substantially holding its fastener shape and not crushing for engagement process, but the fasteners may be deformed during the high pressure of the layup and curing process. This stiffness permits the interlocking of plies rather than the mere crushing of many of the fasteners for engagement, which inhibits effective fastening and interlocking. This crushing action during engagement may also be unpredictable, interlocking in some regions and crushing (not interlocking) is other regions, creating uncertainties in strength. Even if one of the mating plies has soft fasteners, the stiff mating fasteners can effectively engage the soft fasteners and still provide a mechanical connection.
Presently, the fasteners can be made stiff by using a second stiff material interwoven or anchored to the substrate, such as metal wire, thick woven fibers, carbon rods, and the like. This, of course, often introduces a secondary process or further difficulties, adding expense and complexity to the material manufacture. Yet another method includes saturating the ply with a binder such that the soft fasteners are submerged partially or fully beneath a layer of the binder in an upright configuration, so that opposing fasteners have an increased likelihood of connecting. However, the interlocking of the opposing fasteners is very limited and crushing still a problem.
Accordingly, there has been a long-felt need in the art for a composite ply having form-holding fasteners extending therefrom which are configured to effectively engage opposing fasteners without substantial crushing during engagement. What is also needed is a composite ply that is inexpensive to manufacture. Additionally, what is needed is a composite ply with fasteners having the ability to mechanically connect non-adjacent plies.
The present invention is directed to a composite ply with form-holding fasteners extending from therefrom that are configured to penetrate and engage the mating fasteners of another ply within a layup. The present invention permits the use of a soft fiber that is easily woven or otherwise anchored to a substrate, providing a means to stiffen the fiber to a certain level to permit effective fastening. The present invention also reduces costs and permits the fibers to be made of a similar material as the substrate.
In a preferred embodiment of the present invention a composite ply is provided comprising a substrate having a plurality of fibers extending from at least one side thereof and a plurality of fiber fasteners each being formed by the adhering together with a bonding agent of adjacent groupings of the fibers. The bonding agent increases the form-holding characteristics of the fiber fasteners, thereby enhancing their fastening qualities. There are numerous contemplated bonding agents, such as resin, adhesives, or metal, which can be applied on the surface of the fiber fasteners or may permeate the fibers of the fiber fasteners or both. The fibers may be attached to the substrate through known flocking processes. They may also be interwoven into the substrate through known weaving or knitting processes. The substrate may be a sheet material, a yarn material, or a strip material.
The term “fastener” as it is used in the specification and claims herein means a portion of the composite ply that is capable of engaging with features of another ply within the layup, through any means and including hooking, entanglement, and penetration. These fiber fasteners preferably enable the non-permanent attachment on two or more plies, such that they may be disassembled and adjusted in position, although an immediate permanent bonding may also be possible. The fiber fasteners can be shaped as either a hook, a loop, or a variation of the two. The bonding agent holds the desired shape.
One side of the substrate may be a cut pile and the opposing side may be formed into a loop or uncut pile. This can be achieved by utilizing a towel weaving process, where the loops on one side are cut, using mechanical, heat, or laser means well known in industry. The bonding agent can be selectively applied to the fiber fasteners of just one side, to just the hooks, or to just the loops. The bonding agent may be applied by dipping the fiber fasteners in the bonding agent (leaving the substrate and opposite side bare if desired), spraying the bonding agent, or brushing the bonding agent on the fiber fasteners. Other effective methods of applying the bonding agent are also permitted.
The substrate may have a variety of configurations, such as being made of two or more fiber sheets laid one on the other (plied). These fiber sheets may be bonded or mechanically fastened together by, for example, sewing, stapling, weaving, or knitting.
Two or more composite plies of the present invention may be stacked together where the fiber fasteners of adjacent plies interlock. This interlocking most usually occurs with a mold during the layup process, where the user may lay one composite ply upon another, possibly brushing on additional resin. The fiber fasteners may be further induced to interlock through rolling or compression. The layup may be vacuum bagged and heated to cure the bonding agent of the fiber fasteners, such that mating fiber fasteners or contiguous plies are permanently bonded to each other, thus enhancing the interlocking action and increasing interlaminar strength. The fiber fasteners on either ply may be hooks or loops, such that there is hook-to-hook mating or hook-to-loop mating.
In yet another composite assembly, one or more fiber articles may be interposed and sandwiched between two composite plies of the present invention. The fiber fasteners penetrate and pass through the fiber article to engage the composite ply on the opposite side of the fiber article. Or the fiber fasteners of each ply may engage a fastening feature of the fiber article and not fully penetrate. The fiber article and substrate may be selectively impregnated with one or materials, such as resin, polymer, glass, carbon, metal, or ceramic. A composite ply having multiple sheet can be made. A prepreg of the composite ply can also be made.
Hooks may also be formed in an uncut pile (loops) by the imparting of a hook shape in each loop, for example, by bending over the loops to form a hook shape, either maintaining or collapsing the hook shape. The bonding agent similarly substantially holds the hook shape.
The detailed descriptions set forth below in connection with the appended drawings are intended as a description of embodiments of the invention, and is not intended to represent the only forms in which the present invention may be constructed and/or utilized. The descriptions set forth the structure and the sequence of steps for constructing and operating the invention in connection with the illustrated embodiments. It is to be understood, however, that the same or equivalent structures and steps may be accomplished by different embodiments that are also intended to be encompassed within the spirit and scope of the invention.
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Yet another variation of the present invention can be seen in
An alternate embodiment is shown in
To illustrate one of the many conceived configurations of the fiber fasteners 24, one can look to
In tearing tests of the present invention, where one composite ply is pulled away from a mated and cured composite ply, it was shown that the fiber fasteners of the present invention can increase tear strength by 50 to 100%, increase compression strength by more than 20%, increase impact strength by 20%, and increase layup efficiency by 40%.
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An adhesive film sheet is laid beneath the fabric and particles are applied to the film to act as stand-offs to create a gap between the fabric and the film below. Then the fibers are flocked through the fabric; the gap permits the fibers to fully penetrate through the fabric, stopping at the film. The film and fabric are then later compressed, so that the gap collapses and the fibers are firmly implanted in the fabric. The vibration promotes the density of fastening components such as fibers and causes the flocking fastening components to adhere to the adhesive and pack into a layer. This process is a beater bar or gravity flocking system.
While particular forms of the invention have been illustrated and described, it will also be apparent to those skilled in the art that various modifications can be made without departing from the spirit and scope of the invention. Accordingly, it is not intended that the invention be limited except by the claims.
This application is a continuation-in-part of co-pending U.S. application Ser. No. 11/8925,752, filed on Oct. 27, 2007, entitled “Fiber Products, Prepregs, Composites and Method of Producing Same”, which claims the benefit of U.S. provisional patent application Ser. No. 60/854,632, filed on Oct. 27, 2006.
Number | Date | Country | |
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60854632 | Oct 2006 | US |
Number | Date | Country | |
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Parent | 11925752 | Oct 2007 | US |
Child | 12698130 | US |