The instant invention relates generally to woven fabric preforms and to a process for making the same. More particularly, the instant invention relates to a process for producing tailored woven blanks for use in the manufacture of composite articles, and to the composite articles that are manufactured therefrom.
Composite materials are used routinely in the aerospace, automotive and sporting goods industries, to name just a few examples. Structural composite articles are lighter, offer better corrosion resistance, and display improved resistance to damage from cyclic loading (fatigue) compared to corresponding articles that are formed from machined metals. For instance, replacing an aluminum structure with graphite/epoxy composite may achieve a weight reduction of greater than 20%.
One common method of composite manufacture uses a pre-impregnated (prepreg) material made by applying a resin onto a reinforcement fiber. The resin, which is applied outside of a compression mold, may be a thermoplastic resin or a thermosetting resin applied onto a high tenacity reinforcement fiber. The fiber may be in the form of a non-woven fabric of short or long fiber length, or a woven or unidirectional fiber configuration of continuous fiber length. Typical reinforcing fibers include glass, carbon, aramid, basalt or another similar type of fiber. Alternatively, in the so-called Resin Transfer Molding or Resin Infusion Molding processes the reinforcement is placed into a mold and the thermoplastic or thermosetting resin is introduced after the mold is closed.
Reinforcing fibers in the form of woven fabrics exhibit excellent formability and result in composite articles with good mechanical properties. Woven fabrics are fabrics in which two distinct sets of reinforcing yarns or fibers are interwoven with each other to form the fabric. More specifically, woven fabrics include warp yarns that run lengthwise along the fabric and weft yarns that run across the length of the fabric, and which are interwoven with and generally perpendicular to the warp yarns. Typically, the size and density of the warps are equal to the size and density of the wefts, and the warps and the wefts cross each other at a right angle. Optionally, the warps and wefts are of different sizes and/or densities. Further optionally, different types of fiber are used for the warp yarns and for the weft yarns. Further optionally, the warps and wefts cross each other at other than a right angle.
A typical process for making a composite article based on prepreg material uses rectangular fabric blanks to build a preform, which is then wet out with resin and placed in a compression mold to form the finished composite article. In order to avoid wrinkling, binding, stretching or tearing, etc., the rectangular blanks are trimmed and layered up to optimize sheet usage. Additionally, the use of rectangular fabric blanks results in trimming being required around the entire perimeter of the finished composite article. It is therefore a disadvantage of the prior art process that the use of rectangular fabric blanks leads to a significant amount of wastage, of as much as 40% of the reinforcing fiber, since those portions of the blank that are trimmed do not wind up in the finished composite article. Further, the layering up of multiple plies and the trimming operations add to the process time and complexity, which results in overall higher costs for producing the composite articles.
It would be beneficial to provide a process that overcomes at least some of the above-mentioned limitations of the prior art.
According to one aspect, the invention is directed to a process for fabricating a reinforcing woven fabric for use in the manufacture of a composite article having a known three-dimensional shape, comprising: arranging a plurality of warps of reinforcing filamentary yarns extending in a longitudinal direction of said reinforcing woven fabric in parallel to one another and in a sheet-like form; selectively interweaving a plurality of wefts of reinforcing filamentary yarns extending in a direction across said warps and in parallel to one another, so as to form at least one first portion of the woven fabric having interwoven warps and wefts and so as to form at least one second portion of the woven fabric having other than interwoven warps and wefts, wherein the at least one first portion and the at least one second portion are arranged one relative to the other within said reinforcing woven fabric in dependence upon the known three-dimensional shape of the composite article.
According to another aspect, the invention is directed to a process for fabricating a composite article having a known three-dimensional shape, comprising: forming a reinforcing woven fabric having a plurality of warps of reinforcing filamentary yarns extending in a longitudinal direction and having a plurality of wefts of reinforcing filamentary yarns selectively interwoven with said warps so as to form at least one first portion of the reinforcing woven fabric having interwoven warps and wefts and so as to form at least one second portion of the reinforcing woven fabric having other than interwoven warps and wefts; wetting the tailored reinforcing woven fabric with a resin; and applying heat and pressure to the resin-wetted tailored reinforcing woven fabric during a molding cycle in a mold to form the composite article.
According to another aspect, the invention is directed to a reinforcing woven fabric for use in the manufacture of a composite article having a known three-dimensional shape, comprising: a plurality of warps of reinforcing filamentary yarns extending in a longitudinal direction of said reinforcing woven fabric and in parallel to one another; and a plurality of wefts of reinforcing filamentary yarns extending in a direction across said warps and in parallel to one another, said plurality of wefts of reinforcing filamentary yarns being selectively interwoven with said plurality of warps of reinforcing filamentary yarns so as to form at least one first portion of the woven fabric having interwoven warps and wefts and so as to form at least one second portion of the woven fabric having other than interwoven warps and wefts, wherein the at least one first portion and the at least one second portion are arranged one relative to the other within said reinforcing woven fabric in dependence upon the known three-dimensional shape of the composite article.
According to another aspect, the invention is directed to a preformed material for use in the manufacture of a composite article having a known three-dimensional shape, said preformed material having a plurality of reinforcing woven fabrics laminated and integrated to each other, each of said plurality of reinforcing woven fabrics comprising: a plurality of warps of reinforcing filamentary yarns extending in a longitudinal direction of said reinforcing woven fabric and in parallel to one another; and a plurality of wefts of reinforcing filamentary yarns extending in a direction across said warps and in parallel to one another, said plurality of wefts of reinforcing filamentary yarns being selectively interwoven with said plurality of warps of reinforcing filamentary yarns so as to form at least one first portion of the woven fabric having interwoven warps and wefts and so as to form at least one second portion of the woven fabric having other than interwoven warps and wefts, wherein the at least one first portion and the at least one second portion are arranged one relative to the other within said reinforcing woven fabric in dependence upon the known three-dimensional shape of the composite article, and wherein the reinforcing woven fabrics of said plurality of reinforcing woven fabrics are so laminated that the at least one first portion of the respective reinforcing woven fabrics are conformed to each other and the at least one second portion of the respective reinforcing woven fabrics are conformed to each other
According to another aspect, the invention is directed to a fiber reinforced composite material including a preformed material comprising a plurality of woven fabrics laminated and integrated to each other and a resin containing said plurality of reinforcing woven fabrics, each of said plurality of reinforcing woven fabrics comprising: a plurality of warps of reinforcing filamentary yarns extending in a longitudinal direction of said reinforcing woven fabric and in parallel to one another; and a plurality of wefts of reinforcing filamentary yarns extending in a direction across said warps and in parallel to one another, said plurality of wefts of reinforcing filamentary yarns being selectively interwoven with said plurality of warps of reinforcing filamentary yarns so as to form at least one first portion of the woven fabric having interwoven warps and wefts and so as to form at least one second portion of the woven fabric having other than interwoven warps and wefts, wherein the at least one first portion and the at least one second portion are arranged one relative to the other within said reinforcing woven fabric in dependence upon the known three-dimensional shape of the composite article, and wherein the reinforcing woven fabrics of said plurality of reinforcing woven fabrics are so laminated that the at least one first portion of the respective reinforcing woven fabrics are conformed to each other and the at least one second portion of the respective reinforcing woven fabrics are conformed to each other.
According to another aspect, the invention is directed to a process for fabricating a plurality of blanks for use in the manufacture of composite articles, each blank of the plurality of blanks comprising interwoven reinforcing fibers, the process comprising: arranging a first plurality of warps of the reinforcing fibers extending in a longitudinal direction and in parallel to one another so as to define a carrier layer; interweaving a first plurality of wefts of the reinforcing fibers extending in a direction across said first plurality of warps and in parallel to one another so as to form a first interwoven region and a second interwoven region, the first interwoven region separated from the second interwoven region by a non-interwoven region of the carrier layer; and arranging a second plurality of warps of the reinforcing fibers adjacent to and overlapping with the first interwoven region, and interweaving a second plurality of wefts of the reinforcing fiber with the second plurality of warps, so as to define a plurality of first blanks stacked one on top of the other and connected together along opposite edge segments thereof.
According to another aspect, the invention is directed to a process for fabricating a plurality of blanks for use in the manufacture of composite articles, each blank comprising interwoven reinforcing fibers, the process comprising: interweaving reinforcing fibers that extend in a warp direction with reinforcing fibers that extend in a weft direction, to define: a plurality of first blanks stacked one on top of the other and connected together along opposite edge segments thereof; a plurality of second blanks stacked one on top of the other and connected together along opposite edge segments thereof; and a connecting web extending between the plurality of first blanks and the plurality of second blanks and comprising a single layer of reinforcing fibers.
According to another aspect, the invention is directed to a blank assembly comprising a plurality of blanks for use in the manufacture of composite articles, the blank assembly comprising: a plurality of first blanks stacked one on top of the other and connected together along opposite edge segments thereof, each of the plurality of first blanks comprising interwoven reinforcing fibers; a plurality of second blanks stacked one on top of the other and connected together along opposite edge segments thereof, each of the plurality of second blanks comprising interwoven reinforcing fibers; and a connecting web extending between the plurality of first blanks and the plurality of second blanks and comprising a single layer of reinforcing fibers.
The instant invention will now be described by way of example only, with reference to the attached drawings, in which:
a is a top view showing a woven fabric blank having regions in which plural layers of the blank are stacked one on top of another and said regions are joined together by a single layer of a carrier fiber;
b is a side view of the woven fabric blank of
c is a side view showing the plural layers of the blank of
The following description is presented to enable a person skilled in the art to make and use the invention, and is provided in the context of a particular application and its requirements. Various modifications to the disclosed embodiments will be readily apparent to those skilled in the art, and the general principles defined herein may be applied to other embodiments and applications without departing from the scope of the invention. Thus, the present invention is not intended to be limited to the embodiments disclosed, but is to be accorded the widest scope consistent with the principles and features disclosed herein.
Referring to
The prepreg so formed is advanced through a curing station 114, which includes an energy source 116 for providing the energy that is required to partially cure the prepreg. By way of a few specific and non-limiting examples, the energy source 116 is one of an oven and an ultraviolet radiation source. After being partially cured in the curing station 114, the prepreg is either stored for later use or it is transferred into a compression mold 118 and used to form a finished composite article 120. Prior to being placed in the compression mold 118, the prepreg is arranged on a not illustrated preforming mold such that a shape of the prepreg, when so arranged, corresponds approximately to a final shape of the composite article 120. The preformed prepreg is subsequently transferred from the preforming mold to the compression mold 118, for instance using robot 122, and heat and pressure are applied during a molding cycle so as to form the composite article 120. Once formed, the composite article 120 is removed from the compression mold 118, and the compression mold 118 is charged with a next preformed prepreg prior to beginning a next molding cycle. Excess material, if any, is trimmed from the composite article 120 using conventional techniques, such as for instance waterjet cutting, router, laser, knife, ultrasonic knife, etc.
When the prepreg is not to be stored for later use, but rather it is to be transferred directly into the compression mold 118, then optionally the step of partially curing the prepreg is omitted. In this case, the curing of the prepreg is performed entirely within the compression mold 118. As such, according to at least one embodiment of the invention the curing station 114 that is shown in
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2 and 3, and the processes that are described with reference to
According to one optional variation, the prepreg that is formed is a thermoplastic prepreg. According to another optional variation, prepreg material is not formed but rather the woven reinforcement is produced and transferred into a mold prior to being wetted with the resin. In this latter case, the resin is introduced into the closed compression mold and Resin Transfer Molding or Resin Infusion Molding is used to produce the composite article.
In the description that is presented above, the loom 110 is used to produce tailored woven reinforcements having locally built up reinforced regions and/or an arrangement of woven and non-woven areas that is suitable for forming a composite article with a known three-dimensional shape. Alternatively, the tailored woven reinforcement is produced in such a way that plural layers of a same part-shape are formed one on top of another.
The blank assembly 600 comprises a plurality of first blanks, each first blank of the plurality of first blanks being one of the layers of the first shape 602. The first blanks of the plurality of first blanks are stacked one on top of the other and are connected together along opposite edge segments thereof via end-stitching 608. The blank assembly 600 further comprises a plurality of second blanks, each second blank of the plurality of second blanks being one of the layers of the second shape 604. The second blanks of the plurality of second blanks are also stacked one on top of the other and are also connected together along edge segments thereof via end-stitching 608. Each first blank and each second blank comprises interwoven reinforcing fibers. A connecting web 610 extending between the plurality of first blanks and the plurality of second blanks comprises a single layer of reinforcing fibers. The connecting web 610 is a part of a sheet-like carrier layer, which comprises a plurality of warps of reinforcing fiber extending in a longitudinal direction and parallel to one another. The reinforcing fibers are selected from the following group: glass fibers, carbon fibers, aramid fibers, basalt fibers, or another suitable type of fiber.
As is shown in
While the above description constitutes a plurality of embodiments of the present invention, it will be appreciated that the present invention is susceptible to further modification and change without departing from the fair meaning of the accompanying claims.
This PCT Patent Application claims the benefit of U.S. provisional application Ser. No. 61/586,270 filed Jan. 13, 2012, the entire disclosure of the application being considered part of the disclosure of this application, and hereby incorporated by reference.
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/CA2013/000018 | 1/10/2013 | WO | 00 | 7/14/2014 |
Number | Date | Country | |
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61586270 | Jan 2012 | US |