阅读说明：本技术 用于复合增强物的混合的织造纺织品 (Hybrid woven textile for composite reinforcement ) 是由 R·布莱克本 S·J·希尔 于 2015-08-11 设计创作，主要内容包括：一种混合的、织造的纺织材料,该纺织材料可以用于制造纤维增强的复合材料。该混合的纺织材料是由在编织图案中与非织造纤维的条带交织的单向纤维构成的织造织物。在实施例中,该混合的纺织材料是多孔的或相对于在树脂传递模制(RTM)方法中使用的液体树脂是可渗透的,并且由这种纺织材料形成的预成型件可以在此类RTM方法期间用液体树脂灌注。(A hybrid, woven textile material that can be used to make fiber reinforced composites. The hybrid textile material is a woven fabric comprised of unidirectional fibers interwoven with strips of non-woven fibers in a weave pattern. In embodiments, the hybrid textile material is porous or permeable with respect to liquid resins used in Resin Transfer Molding (RTM) processes, and preforms formed from such textile material may be infused with liquid resin during such RTM processes.)

1. A preform adapted to receive a liquid resin in a liquid molding process, the preform comprising layers of reinforcing fibers laid in a stacking arrangement, wherein at least one of the layers of reinforcing fibers is a woven fabric comprising:

unidirectional fiber bundles arranged parallel to one another in a sheet-like configuration; and

strips of non-woven fibers interwoven with these unidirectional fiber bundles in a weave pattern,

wherein each unidirectional fiber bundle is composed of a plurality of continuous carbon fiber filaments, and

wherein each strip of non-woven fibers is self-supporting, is a single layer of material that is not attached to another layer of fibers, and is comprised of randomly arranged and/or randomly oriented carbon fibers.

2. The preform of claim 1, having an areal weight of from 50gsm to 380 gsm.

3. The preform of claim 1 or 2, wherein each strip of nonwoven fibers has an areal weight of from 2gsm to 34 gsm.

4. The preform of claim 1, wherein each strip of nonwoven fibers has a width of about 5mm to 40 mm.

5. The preform of claim 1, wherein each strip of nonwoven fibers has a thickness in the range of 10 μ ι η -50 μ ι η (or 0.01-0.05 mm).

6. The preform according to claim 1, wherein the majority of the nonwoven fibers in the strips have a cross-sectional diameter in the range of about 3 to 40 μm, preferably in the range of about 5 to 10 μm in diameter.

7. The preform of claim 1, wherein each unidirectional fiber bundle is comprised of 1000 to 100,000 fiber filaments.

8. The preform of claim 7, wherein the fiber filaments in each fiber bundle have a cross-sectional diameter in the range of 3-15 μ ι η, preferably 4-7 μ ι η.

9. The preform according to claim 1, wherein the strips of nonwoven fibers have a sufficient amount of binder to hold the fibers together but allow the strips to be permeable to liquids and gases.

10. The preform according to claim 1, wherein the weave pattern is selected from the group consisting of plain weave, satin weave, and twill weave.

11. A composite material comprising a woven fabric impregnated or infused with a matrix resin, wherein the woven fabric comprises:

unidirectional fiber bundles arranged parallel to one another in a sheet-like configuration; and

strips of non-woven fibers interwoven with these unidirectional fiber bundles in a weave pattern,

wherein each unidirectional fiber bundle is composed of a plurality of continuous carbon fiber filaments, and

wherein each strip of non-woven fibers is self-supporting, is a single layer of material that is not attached to another layer of fibers, and is comprised of randomly arranged and/or randomly oriented carbon fibers.

12. A method of forming a composite structure comprising injecting a liquid resin into the preform of claim 1.

Background

Three-dimensional polymer composite parts can be manufactured using different methods, one of which is autoclave molding. In this autoclave molding method, a fabric, typically composed of carbon fibers, is pre-impregnated with a resin matrix. The prepreg is typically placed in a mold and then heated under vacuum to cure the impregnated resin and produce the final composite part. Prepregs to be moulded into composites have the advantage of ease of use and high reliability. However, these prepregs also have the following disadvantages: have limited drapability (i.e., the ability to drape).

Another composite manufacturing method is liquid molding. Resin Transfer Moulding (RTM) and Vacuum Assisted Resin Transfer Moulding (VARTM) are some specific examples. In the liquid molding process, a layer of dry reinforcing fibers (without matrix resin) is shaped and compressed into an adhesive shaped structure called a "preform". Such preforms are then often infused with uncured liquid resin in a closed mold or closed vacuum bag. After the resin infusion phase is completed, the resin is cured, producing a solid composite part. Liquid molding techniques are particularly useful in the manufacture of complex shaped structures that are otherwise difficult to manufacture using conventional prepreg techniques. Furthermore, the dry, flexible fibrous material used to form the preform may have significant advantages over standard resin impregnated prepreg materials due to its longer shelf life and suitability for more complex geometries.

SUMMARY

It is an object of the present disclosure to provide a hybrid, woven textile material that can be used to make fiber reinforced composites. The hybrid textile material is a woven fabric comprised of unidirectional fibers interwoven with strips of non-woven fibers in a weave pattern. In an embodiment, the hybrid, woven textile material is porous and permeable with respect to liquid resin used in the RTM method, and a preform formed from such a woven textile material may be infused with liquid resin during the RTM method.

Brief description of the drawings

Figure 1 is a top view of a textile structure based on a woven unidirectional construction, also known as single Weave (Uni-Weave).

FIG. 2 is a cross-sectional view of the woven fabric shown in FIG. 1, showing crimping.

Figure 3 schematically illustrates a textile structure based on a stitched unidirectional construction, also known as single Stitch (Uni-Stitch).

Figure 4 illustrates a seam anchoring mechanism for the fabric structure shown in figure 3.

FIG. 5 schematically illustrates a hybrid woven fabric according to an embodiment of the disclosure.

FIG. 6 is a cross-sectional view of the woven fabric shown in FIG. 5.

FIG. 7 is a photographic image of a plain woven fabric made according to one embodiment of the present disclosure.

Fig. 8 is a graph showing a comparison of in-plane permeability performance of three different fabric constructions used in the manufacture of resin infused preforms.

Detailed Description

Some available techniques for making unidirectional fiber-based textiles include: braided, sewn or bonded.

Woven unidirectional construction (also known as single weaving) is a method of weaving. Here, auxiliary yarns may be woven in the second shaft to anchor the structural fibers in the main shaft. These secondary yarns are typically fine fibers in order to minimize fiber crimp. Examples of single weave constructions and crimp patterns are shown in figures 1 and 2, respectively. Common types of auxiliary fibers used in such constructions are glass, polyester, and copolyamides. This type of construction is more suitable for a 0 ° oriented reinforcing fabric, but can also be used to construct a 90 ° and polar oriented fabric. Typically, a single woven fabric is found to have 95% of the fiber mass in the primary orientation and 5% in the secondary orientation. This type of fabric was found to be characterized by good permeability and drape (i.e., ability to drape) at the expense of poor textile integrity and low in-plane mechanical properties. It is typically observed that the 0 ° tensile and compressive properties are subject to the curling effect caused by the weft-assist fibers. Adjusting the weave pattern of the fabric may help reduce the frequency of the curling effect, but this is typically accompanied by a further reduction in textile stability. Solving the low stability can sometimes be achieved in the case of polymer-based auxiliary yarns by heat treatment or by adding a stabilizing medium such as a powder binder or laminated fluff, but these solutions will then often reduce the permeability of the final fabric and introduce additional problems with respect to environmental and solvent resistance.

The unidirectional construction of the stitch, also known as single stitch, is based on the use of a warp knitting machine to anchor the structural fibers to the main shaft by using full thickness stitches interlocked with floating weft auxiliary yarns and thereby constrain the main fibers between the stitch line and auxiliary yarns. Examples of single suture configurations and suture anchoring mechanisms are illustrated in fig. 3 and 4, respectively. The stitching thread used in this process is typically either polyester or copolyamide, while the secondary threads are either identical or made of glass, it being found that the mass of stitching thread and secondary yarn in these constructions is typically 2-6% of the total mass. This type of unidirectional textile is suitable as a 0 ° oriented reinforcement fabric, however a 90 ° oriented reinforcement is also possible. Single stitch constructions typically show an improvement over woven structures in mechanical performance due to the relatively reduced level of out-of-plane crimp, but still show a reduction due to the interbraie gaps and residual crimp from the stitches when compared to the prepreg tape product. Thus, it is generally found that the permeability of these fabrics is higher than their woven equivalent, while the handling stability is also improved due to the local anchoring efficiency of the suture.

Another fabric construction is created by bonding or laminating the unidirectional fibers in place with a polymeric material. Some bonding methods include the use of epoxy adhesives, thermoplastic face yarns, and polymeric yarns. This method for producing dry unidirectional fabrics provides undoubtedly the mechanical properties closest to those of pre-impregnated tapes due to the high level of fibre filaments and near zero intra-bundle gaps that can be achieved. This very high level of fiber nesting, despite having a significant reduction in permeability to these fabric constructions, is several orders of magnitude lower than the full-thickness permeability of alternative versions. This makes the use of such textile constructions more suitable for narrow unidirectional tapes, where permeability adjustments can be achieved within the preform structure. Another problem sometimes observed with these textiles is that a lower level of stability is a phenomenon known as "fiber wash". This is an effect observed after the resin infusion process, where it can be seen that the bundles (tow bundles) have in-plane deviations due to the pressure difference at the flow front during the infiltration process causing local bending of the fibers. This adhesive type of construction is suitable as a 0 ° oriented reinforcement.

It has typically been found that as the mechanical properties are increased by reducing fiber crimp and gaps, the permeability, and in particular the through-thickness permeability, is significantly reduced. In view of the problems created with dry unidirectional fiber products in which there is a compromise between mechanical properties, permeability and textile integrity, unique hybrid woven textiles have been designed to address these problems.

Fig. 5 depicts an exemplary hybrid woven fabric having unidirectional fibers in the form of continuous fiber bundles 10 interwoven with non-woven strips 11. FIG. 6 is a cross-sectional view of the woven fabric shown in FIG. 5. Referring to fig. 6, the unidirectional fiber bundles 10 are arranged parallel to each other in a sheet-like configuration and extend in a first direction (e.g., the warp direction), and the nonwoven strips 11 extend in a second direction (e.g., the weft direction) transverse to the first direction. Each nonwoven strip floats above and then below the plurality of bundles in a weave pattern. Each fiber bundle 10 is a bundle of a plurality of fiber filaments. The nonwoven strips 11 are formed from lightweight nonwoven veil composed of randomly arranged and/or randomly oriented fibers. Preferably, the nonwoven fibrous veil is of 1gsm (g/m)²) To 40gsm, more preferably 3gsm to 1A light weight material of 0gsm areal weight. Each nonwoven strip is flexible and has a narrow width relative to its length. In one embodiment, the width of the nonwoven strip is from 5mm to 40mm, preferably 10mm to 30mm, and the thickness is from 10 μm to 60 μm (0.01-0.05 mm). The weave pattern may have any conventional weave structure, such as a plain weave (shown in fig. 5), a satin weave, or a twill weave.

As discussed above, these unidirectional fibers are in the form of continuous fiber bundles. Each fiber bundle is made up of hundreds of smaller continuous fiber filaments. These fiber bundles may have 1000 to 100,000 fiber filaments per bundle, and in some embodiments 3000 to 24000 filaments per bundle. These fiber filaments may have a cross-sectional diameter in the range of 3-15 μm, preferably 4-7 μm. Suitable fibers are those used as structural reinforcements for high performance composites, such as composite parts for aerospace and automotive applications. These structural fibers may be made of high strength materials such as carbon (including graphite), glass (including E-glass or S-glass fibers), quartz, alumina, zirconia, silicon carbide, and other ceramics, and tough polymers such as aramids (including Kevlar), high modulus Polyethylene (PE), polyester, poly-p-phenylene-benzobisoxazole (PBO), and mixed combinations thereof. For the manufacture of high strength composite structures, such as the primary parts of aircraft, these unidirectional fibers preferably have a tensile strength greater than 500 ksi. In a preferred embodiment, the unidirectional fibers are carbon fibers.

The unidirectional fibers may be coated with a sizing composition and/or finish (finishes) for a number of purposes including facilitating handling, protecting the fibers from damage caused by pressing and processing, aiding compatibility and wetting of the fibers by the resin, and overall enhancement of the composite properties.

The nonwoven strips described above may be formed by cutting larger nonwoven veils, and the cut nonwoven material is then used for weaving. The nonwoven veil is composed of intermingled, randomly arranged fibers and a small amount of polymeric binder to hold the fibers together. It is desirable to provide a nonwoven veil with a sufficient amount of binder to hold the fibers together, and yet the amount of binder is small enough to make the resulting veil porous and permeable to liquids and gases, particularly liquid resins. Suitable polymeric binders include polyvinyl alcohol (PVA), polyesters, copolyesters, crosslinked polyesters, styrene acrylic, phenoxy, and polyurethanes, combinations and copolymers thereof. Preferably, the amount of binder is 5% to 25% by weight based on the total weight of the veil. The nonwoven veil is flexible and self-supporting, meaning that the nonwoven veil does not need a support carrier. Further, the nonwoven veil is a single layer of material that is not attached to another layer of fibers. The fibers of the nonwoven veil may be chopped or continuous fiber filaments or a combination thereof. The nonwoven fibrous material for the nonwoven veil may be selected from the group consisting of carbon, glass, metal, quartz, polymers and copolymers thereof, mixtures thereof (e.g., carbon/glass mixtures), and combinations thereof. The polymeric material used for these fibers may be selected from: an aromatic polyamide; a polyester; polyamides, including aliphatic polyamides, cycloaliphatic polyamides, and aromatic polyamides; polyphthalamides; polyamide-imide; polyarylsulfones, including polyethersulfones and polyethersulfones; polysulfones; a polyphenylsulfone; polyaryletherketones, including polyetheretherketone and polyetherketoneketone; polyphenylene sulfide; an elastomeric polyamide; polyphenylene ether; a polyurethane; liquid Crystal Polymers (LCP); a phenoxy group; polyacrylonitrile, acrylate polymers, and copolymers thereof. The fibers of the veil may also be metal coated. In a preferred embodiment, the non-woven strips are constructed of carbon fibers.

Most nonwoven fibers have a cross-sectional diameter in the range of about 1 μm to 40 μm, with the majority of these fibers more preferably having a diameter in the range of about 4 μm to 20 μm.

In one embodiment, the woven fabric (based on a combination of unidirectional fiber bundles and nonwoven strips) has an areal weight of 50gsm to 400gsm, preferably 100gsm to 200 gsm.

Benefits of the hybrid textile materials described herein include: the extremely low crimp of these structural fibers due to the low thickness of the nonwoven veil; improved permeability due to the porous structure of these nonwoven strips; improved fracture behavior of the nonwoven strips from the interlaminar region of the reinforcement preform or the final composite laminate; improved laydown efficiency during the preparation of preforms having off-axis fibers in a continuous woven form; potentially improved handling behavior if the nonwoven contains a stabilizing binder and the textile is laminated. Further, the fabrics disclosed herein may be produced in different configurations to provide 0 °, 90 °, + θ °, or- θ ° fiber orientations.

Method for making non-woven veil

As an example, the nonwoven veil discussed above may be produced by a conventional wet-laid process. In the wet-laid process, the wet chopped fibers are dispersed in an aqueous slurry containing one or more binders, one or more surfactants, one or more viscosity modifiers, one or more defoamers, and/or other chemical agents. Once the chopped fibers are introduced into the slurry, the slurry is vigorously agitated so that the fibers become dispersed. The slurry containing these fibers is deposited onto a moving screen where a substantial portion of the water is removed to form a web. The resulting mat is dried to remove any residual water and cure the binder or binders. The nonwoven mat/veil formed is a collection of discrete, individual fiber filaments arranged in a random orientation. When uniform distribution of fiber and/or weight is desired, wet-laying is typically used.

The final nonwoven veil contains at least about 90 wt.% fibers on a dry basis (excluding sizing/binder chemicals), for example from about 93 wt.% to about 99 wt.% fibers on a dry basis (excluding sizing/binder).

Additional binder may be applied to the nonwoven veil after it is manufactured but before weaving to improve the stability of the veil and to aid in preform compaction during the manufacture of composite parts. Suitable binders for stabilizing the nonwoven veil include epoxy resins, thermoplastic polymers, or combinations thereof. A particularly suitable adhesive for stabilizing the nonwoven veil is a polyarylether thermoplastic epoxy adhesive disclosed in U.S. patent No. 8,927,662, the contents of which are incorporated by reference herein in their entirety. The adhesive may be applied to the veil in the form of a powder using conventional coating techniques such as dry bar coating whereby a dry powder is coated onto a release paper using a roll-over-roll or knife-over-roll coater and the powder is then transferred to the veil. Another suitable adhesive for stabilization is a liquid adhesive composition described in U.S. publication No. 2014/0179187, the contents of which are incorporated by reference herein in their entirety. Liquid binders disclosed in U.S. patent application No. 14/750,327 filed on 25/6 of 2015 are also suitable. As an example, the liquid adhesive may be applied to the face yarn by dip coating.

If additional binder is used, the total amount of binder in the final veil should not exceed 25% by weight.

Method for producing a hybrid woven fabric

The hybrid woven fabrics disclosed herein can be manufactured on standard rapier looms. These unidirectional (e.g., carbon) fibers are stretched offline to the appropriate width based on FAW requirements. The nonwoven is produced in the process detailed above in wide form and cut to the desired width. The stretched fibers and nonwoven strips were wound on a single box and mounted on an engine shaft. Multiple fiber boxes are required in the warp direction to achieve the target textile width, while a single box of nonwoven tape is required when weft insertion is done separately during the weaving process. As warp fibers are fed through the loom, adjacent fibers are pulled in opposite directions (i.e., up or down) and the weft nonwoven strip is pulled through the shed to create the weave pattern. Once the weft nonwoven strip is positioned, the warp fibers are released and pulled under tension to consolidate the weave.

Applications of

The hybrid woven textile material disclosed herein is particularly suitable for forming preforms to be used in RTM processes because the textile material is porous and permeable with respect to the liquid resin used in such RTM processes. To form the preform, multiple layers of textile material are laid down to a desired thickness.

It would be desirable to provide a fibrous preform having a binder content sufficient to hold the fibers in the desired shape and position, but small enough to make the resulting preform porous so that it can be impregnated with a matrix resin during a subsequent molding process. Furthermore, it would be desirable to provide unidirectional fiber preforms having improved permeability relative to RTM resins to reduce injection time and improve fiber wet out. For this reason, the amount of binder in the preform is preferably less than 15% by weight, based on the total weight of the preform.

The preform is placed in a closed mold. The mold is heated to a predetermined temperature and a low viscosity resin is injected into the mold to infuse the preform with resin. The resin is then cured to form the composite part.

Alternatively, the hybrid woven textile material may be used to form prepregs using conventional resin impregnation techniques.

Examples of the invention

Figure 7 illustrates a hybrid veil-woven fabric made according to one embodiment of the present disclosure. Unidirectional carbon fiber bundles (IMS 65 from Toho Tenax) were woven with strips of non-woven carbon fibers in a plain weave structure using a conventional weaving method. The carbon bundle had a width of 8mm and the nonwoven carbon strip had a width of 16 mm. The non-woven carbon strip had an areal weight of 8gsm and was coated with 5gsm of a powder form7720 adhesive (from Cytec Engineered Materials). The woven fabric had an areal weight of 110 gsm.

Ten (10) layers of the hybrid veil-woven fabric described above were laid down to form the preform. The preform was heated to 130 ° in a convection oven for 15 minutes under vacuum bag and cooled to 25 ℃ under vacuum to consolidate the layers.

For comparison, two additional preforms were constructed in the same manner using conventional single knit fabric (supplied by sigma Ltd) and dry unidirectional tape (supplied by sigma).

By usingEP2400 (from cyanogen-Technological materials) pours half of the preform and cures. The resulting composite laminate was then cut into coupon coupons using a diamond tip cooling saw and tested according to EN test method standard on a Zwick testing machine. The results from these tests are recorded in table 1. In table 1, laminate codes DT, UW and VW refer to cured composite laminates formed with dry tape, single knit fabric and veil-woven fabric, respectively.

Other portions of the preform were used to measure in-plane permeability. The preforms were bagged without any flow aid to ensure in-plane flow behavior. The flow front and volume of the infused resin were monitored over time. Furthermore, knowing the viscosity of the resin and the fiber volume achieved at the infusion temperature, the permeability of the preform can be calculated using Darcy's law:

wherein

K-Permeability (10)^-xm²)

X is the length of perfusion (m)

η ═ resin viscosity (m.pas)

FVF ═ fiber volume fraction (%)

Δ ρ ═ differential pressure (mbar)

time (hour)

The results are illustrated in fig. 8. From fig. 8, it is evident that the UD tape shows very poor in-plane permeability due to the highly aligned fibers restricting the resin flow through the preform. In contrast, the woven UD showed more crimp, resulting in superior permeability performance. The novel veil-woven construction exhibits the highest permeability performance due to the inclusion of non-woven strips that enhance flow characteristics within the textile while maintaining a high degree of alignment within the carbon fibers.

The RTM method injects the resin in an in-plane direction from one end side toward the other end side of the dry fibrous preform. It has been found that the incorporation of non-woven carbon fibers in a base fabric structure of unidirectional fibers improves permeability and in-plane properties (0 ° mechanical properties). A significant increase in the permeability of the preform formed by the hybrid veil-woven fabric (VW) was found compared to the preform formed by the Dry Tape (DT) and the single woven fabric (UW):

+ 56% compared to a single knit fabric (UW)

+ 782% compared to Dry Tape (DT).

TABLE 1