Patent Application
20220410495
The present disclosure relates to a prepreg, a preparation method thereof and a fiber-reinforced composite material prepared therefrom.
A fiber-reinforced composite material prepared by impregnating a matrix resin in a fiber material for reinforcement, followed by curing has been widely used in various fields such as electronic parts, automobile parts or the like.
Glass fiber or carbon fiber has been mainly used as the fiber material for reinforcement. However, glass fiber has a high specific gravity, thus making it difficult to reduce a weight, and is also harmful to the human body, while carbon fiber has a high specific stiffness and thus has poor machinability and impact resistance.
As an alternative to solve these problems, a technique for using an aramid fiber has been introduced. However, the aramid fiber has poor wettability, and compatibility with the matrix resin compared to the glass fiber or carbon fiber, thus resulting in another problem such as voids occurring after curing into a fiber-reinforced composite material.
In the present disclosure, there is provided a preparation method of a prepreg.
There are also provided a prepreg prepared from the preparation method of a prepreg and a fiber-reinforced composite material prepared therefrom.
Hereinafter, the preparation method of a prepreg, the prepreg prepared from the preparation method, and the fiber-reinforced composite material prepared from the prepreg according to specific embodiments of the present disclosure will be described.
According to one embodiment, there is provided a preparation method of a prepreg, including:
a first laminating step of laminating a resin film on an aramid fiber base material and applying a pressure; and a second laminating step of applying a pressure to a laminate obtained from the first laminating step,
wherein a lower pressure is applied at a lower temperature in the second laminating step than in the first laminating step.
As a result of studying to improve the wettability of the aramid fiber of the fiber-reinforced composite material to the resin, the present inventors have confirmed that a high-quality fiber-reinforced composite material can be obtained by improving the wettability of the aramid fiber base material to the resin during molding of a prepreg, when preparing the prepreg, which is an intermediate material for preparing the fiber-reinforced composite material, through a first laminating step performed under the conditions of high temperature and high pressure and a second laminating step performed under the conditions of low temperature and medium pressure.
Specifically, the present inventors have developed a preparation method of a prepreg with an appropriate resin content while increasing a thickness reduction rate during molding of the prepreg in consideration of elastic recovery property of the aramid fiber base material, viscosity property and curing property of a resin film, and the like under the conditions for preparing and molding the prepreg.
The first laminating step of the preparation method according to one embodiment may maximize permeability of the resin so that the resin film may penetrate deeply into the aramid fiber base material, and may be performed at a high temperature and under a high pressure so that an appropriate content of the resin may be impregnated into the aramid fiber base material.
Specifically, the first laminating step may be performed at a temperature of 80° C. to 90° C., 82° C. to 88° C., or 84° C. to 86° C. Within the above temperature range, the permeability of the resin may be maximized while the resin film does not harden, and an unimpregnated part may not occur inside the aramid fiber base material, thereby inhibiting the occurrence of problems such as a decrease in strength, and a high moisture absorption rate caused by an unimpregnated area or a dry area occurring during subsequent molding.
In addition, the first laminating step may be performed under a pressure of 2.6 to 5 bar, 2.8 to 4.5 bar, or 3 to 4 bar. As such, when a high pressure is applied to the resin film laminated on both sides of the aramid fiber base material at a high temperature, the viscosity of the resin may be lowered and the resin may easily penetrate between the fibers of the aramid fiber base material, and thus an unimpregnated part may not occur inside the aramid fiber base material, thereby inhibiting the occurrence of problems such as a decrease in strength, and a high moisture absorption rate. In addition, when a pressure is removed after applying a high pressure to the aramid fiber base material, relatively large voids may be formed inside the prepreg by the elastic recovery of the aramid fiber base material. Due to the large voids, the prepreg may have an improved thickness reduction rate during molding.
The second laminating step of the preparation method according to above one embodiment may be performed at a low temperature and under medium pressure in order to improve the resin adhesion, impregnation property and the like near a surface of the aramid fiber base material and to provide an appropriate level of resin content.
Specifically, the second laminating step may be performed at a temperature of 70° C. to 79° C., 70° C. to 75° C., or 70° C. to 73° C. In addition, the second laminating step may be performed under a pressure of 1.5 to 2.5 bar, 1.7 to 2.3 bar, or 1.8 to 2.2 bar. As such, when medium pressure is applied to a laminate at a low temperature, a degree of elastic recovery of the aramid fiber base material and a viscosity of the resin may be controlled to an appropriate level so as to improve adhesion and impregnation with the resin near a surface of the aramid fiber base material and improve surface quality while increasing a resin content in the prepreg.
The preparation method according to one embodiment may be performed as a continuous process. Specifically, the aramid fiber base material and the resin film may be continuously supplied so that the resin film is laminated on both sides of the aramid fiber base material. More specifically, the aramid fiber base material and the resin film may be continuously supplied by a roller and may be laminated through a pressure roller with a heated surface. As one example, the first and second laminating steps may be performed through at least two rollers, in which at least one roller may pressurize a resin film laminated on both sides of the aramid fiber base material under a high pressure (e.g., 2.6 to 5 bar, 2.8 to 4.5 bar, or 3 to 4 bar) in a state where the surface temperature is heated to a high temperature (e.g., 80° C. to 90° C., 82° C. to 88° C., or 84° C. to 86° C.), and at least another roller may pressurize a laminate under a medium pressure (e.g., 1.5 to 2.5 bar, 1.7 to 2.3 bar, or 1.8 to 2.2 bar) in a state where the surface temperature is heated to a low temperature (e.g., 70° C. to 79° C., 70° C. to 75° C., or 70° C. to 73° C.).
At this time, the resin film may be sufficiently impregnated down to the center of the aramid fiber base material by adjusting a feed rate in the first laminating step to 0.1 to 1.5 m/min, 0.1 to 1.0 m/min, or 0.1 to 0.8 m/min.
In the second laminating step, the feed rate of the laminate may be adjusted to be the same as in the first laminating step in that the second laminating step may be performed as a continuous process with the first laminating step.
The aramid fiber base material that can be used in the preparation method according to one embodiment may be a fabric woven with aramid fibers. In this case, a prepreg with excellent mechanical properties may be prepared by maximizing the impregnation property of the resin using a fiber of 1500 to 3500 denier as the aramid fiber.
In the preparation method according to one embodiment, it is possible to prevent the resin film from being cured in the first and second laminating steps by using a resin film cured at a temperature of about 90° C. to 130° C.
In addition, it is possible to improve the impregnation property of the resin film to the aramid fiber base material by using a resin film having an absolute viscosity of about 5 to 10 Pa·s at about 70° C.
The absolute viscosity may be a viscosity value measured at about 70° C. by using a rotational rheometer after preparing a specimen having a diameter of about 300 mm and a thickness of about 300 μm.
Such resin film may include a thermoplastic resin, a thermosetting resin, or a mixture thereof.
For example, the resin film may be formed from a thermosetting resin composition. A main resin of the thermosetting resin composition may be at least one selected from the group consisting of epoxy resin, phenol resin, unsaturated polyester resin, cyanate ester resin, and the like.
Out of them, the resin film may be formed from a thermosetting resin composition including epoxy resin.
The epoxy resin included in the thermosetting resin composition may mean a material having two or more epoxy groups in a molecule or a resin produced by polymerization of the material. As the epoxy resin, for example, at least one selected from the group consisting of bisphenol type epoxy resin such as bisphenol A type epoxy resin, bisphenol F type epoxy resin, bisphenol AD type epoxy resin, and bisphenol S type epoxy resin; brominated epoxy resin such as tetrabromobisphenol A diglycidyl ether; epoxy resin having a biphenyl skeleton; epoxy resin having a naphthalene skeleton; epoxy resin having a dicyclopentadiene skeleton; novolac type epoxy resin such as phenol novolac type epoxy resin and cresol novolac type epoxy resin; and glycidylamine type epoxy resin such as diaminodiphenylmethane type epoxy resin, diaminodiphenylsulfone type epoxy resin, aminophenol type epoxy resin, metaxylene diamine type epoxy resin, 1,3-bisaminomethyl cyclohexane type epoxy resin and isocyanurate type epoxy resin may be used.
In addition, the thermosetting resin composition may include a curing agent for curing the epoxy resin. A compound having an active group capable of cross-linking with an epoxy group may be used as the curing agent. Examples of the curing agent may include dicyandiamide, diaminodiphenylmethane, diaminodiphenylsulfone, aminobenzoic acid esters, various acid anhydrides, phenol novolac resin, cresol novolac resin, polyphenol compound, imidazole derivative, aliphatic amine, tetramethylguanidine, thiourea-amine, methyl hexahydrophthalic anhydride, other carboxylic acid anhydrides, carboxylic acid hydrazide, carboxylic acid amide, polymercaptan, boron trifluoride ethylamine complex, other Lewis acid complexes, etc.
The curing agent may be used in an amount of about 3 to 10 parts by weight based on 100 parts by weight of the epoxy resin so as to properly cure the epoxy resin without a residual curing agent.
The thermosetting resin composition may further include a thermoplastic resin, if necessary. For example, the thermoplastic resin may be at least one selected from the group consisting of polyamide, polycarbonate, polyacetal, polyphenylene oxide, polyphenylene sulfide, polyarylate, polyester, polyamideimide, polyimide, polyetherimide, polyimide having a phenyl trimethyl indane structure, polysulfone, polyethersulfone, polyetherketone, polyetheretherketone, polyaramid, polyethernitrile and polybenzimidazole.
The thermoplastic resin may be added in the form of particles or fibers. When added in the form of particles, a shape thereof may be a spherical, non-spherical, porous, whisker, or flake shape, and when added in the form of fibers, the thermoplastic resin may be added in a state of short fibers or long fibers.
The thermosetting resin composition may further include various additives known in the art to which the present disclosure pertains in addition to the above-described configuration, for example, a curing aid, etc.
Meanwhile, according to another embodiment of the present disclosure, there is provided a prepreg prepared according to the preparation method. The prepreg prepared according to the preparation method may include an aramid fiber base material and a resin impregnated in the aramid fiber base material. Since the aramid fiber base material and the resin have been described in detail above, a detailed description thereof will be omitted.
In particular, the prepreg is prepared through a two-step laminating process under specific conditions and impregnated with a resin down to a center of the prepreg, and thus may be provided with a minimized unimpregnated area. In addition, it may also have a relatively large void, thereby showing an appropriate resin content while exhibiting a large thickness reduction rate during molding into a fiber-reinforced composite material.
Specifically, the prepreg may have a high resin content of 35 to 45 wt %, 37 to 43 wt %, or 39 to 41 wt %.
In addition, the prepreg may provide a fiber-reinforced composite material by an out-of-autoclave process using only a vacuum pump and an oven without using an autoclave, which is an expensive pressurization facility.
Although the existing out-of-autoclave process has an advantage of not using expensive pressurization equipment, the method has a disadvantage of a high defect rate due to the formation of voids by volatile ingredients of the resin film.
However, the prepreg prepared according to the preparation method of one embodiment may provide a high-quality fiber-reinforced composite material even by the out-of-autoclave process.
Meanwhile, according to another embodiment of the present disclosure, there is provided a fiber-reinforced composite material prepared from the prepreg. The fiber-reinforced composite material may include an aramid fiber base material and a resin cured in a state of being impregnated in the aramid fiber base material. Since the aramid fiber base material and the resin have been described in detail above, a detailed description thereof will be omitted.
The fiber-reinforced composite material may be prepared from one or more prepregs, or a laminate in which two or more prepregs are laminated.
The fiber-reinforced composite material is prepared from the prepreg prepared through a two-step laminating process under specific conditions described above, so as to minimize an unimpregnated area or a dry area, thereby showing excellent strength, a low moisture absorption rate, and the like.
Specifically, the fiber-reinforced composite material may have a flexural strength of 250 to 400 MPa, 270 to 350 MPa, or 300 to 330 MPa as measured according to ASTM D790.
In addition, the fiber-reinforced composite material may have a moisture absorption rate of 0 wt % or more, and 3 wt % or less, 2 wt % or less, or 1.7 wt % or less, as calculated by the following Equation 1.
Moisture absorption rate=(Weight of sample after immersion−Weight of sample before immersion)/Weight of sample before immersion* 100 [Equation 1]
in the Equation 1, the weight of a sample before immersion is a weight before immersing the sample in distilled water, and the weight of a sample after immersion is a weight of the sample measured after being completely immersed in distilled water and taken out, wherein the weight is a value measured after primarily removing moisture from upper and lower portions and an edge of the sample with towel and secondarily removing moisture from the upper and lower portions with dry towel.
For details on the method of measuring the flexural strength and moisture absorption rate, refer to the contents described in Test Examples to be described later.
The fiber-reinforced composite material may exhibit the above-described excellent flexural strength and low moisture absorption rate even when molded by an out-of-autoclave process.
In addition, the fiber-reinforced composite material may show a high resin content of 35 to 45 wt %, 35 to 40 wt %, 36 to 38 wt %, or 37 to 38 wt %.
A preparation method of a prepreg according to one embodiment of the present disclosure may include an aramid fiber base material with improved wettability to resin, can increase a thickness reduction rate during molding of the prepreg, has an appropriate resin content, and can provide a prepreg suitable for molding by an out-of-autoclave process. In addition, the prepreg may provide a fiber-reinforced composite material that exhibits a thin thickness and a high resin content even by an out-of-autoclave process, and shows high strength and low moisture absorption rate.
Hereinafter, the function and effect of the present invention will be described in more detail with specific examples. However, these examples are for illustrative purposes only, and the invention is not intended to be limited by these examples.
A plain-woven aramid fabric was woven using aramid yarn having about 3000 denier as warp and weft yarns.
Meanwhile, an epoxy resin film prepared by applying an epoxy resin composition available as SCP-510 from EZ Composite to a release paper in an application amount of about 80±10 g/m2, followed by drying was used as the resin film.
While continuously supplying the aramid fabric, the epoxy resin film was continuously supplied so as to come into a contact with both sides of the aramid fabric. A feed rate of the aramid fabric and the resin film was controlled to about 0.5 m/min.
Then, a first laminating step was performed by applying a pressure of 3 bar to a resin film laminated on both sides of the aramid fabric with a pressure roller heated to 85° C. After that, a prepreg was prepared by impregnating the resin film in both sides of the aramid fabric through a second laminating step of applying a pressure of 2 bar to a laminate obtained in the first laminating step with a pressure roller heated again to 70° C.
A prepreg was prepared in the same manner as in Example 1, except for performing a first laminating step of applying a pressure to the resin film laminated on both sides of the aramid fabric with a pressure roller heated to 85° C.; a second laminating step of applying a pressure to the resin film laminated on both sides of the aramid fabric with a pressure roller heated to 70° C.; and a third laminating step of applying a pressure to the resin film laminated on both sides of the aramid fabric with a pressure roller heated to 100° C. instead of the first and second laminating steps.
10
Test Examples: Evaluation of Physical Properties of Prepreq
The physical properties of the prepregs prepared in Examples and Comparative Examples were evaluated by the method described below, and the results thereof are shown in table 1.
1) Resin Content before Molding
A percentage of mass per unit of a resin film to mass per unit of a prepreg ((Mass per unit of prepreg−Mass per unit of aramid fabric)/Mass per unit of prepreg*100) was measured and defined as a resin content (unit: wt %).
2) Thickness after Molding, Rate of Change in Thickness and Resin Content
Four prepregs were laminated in four layers and then sufficiently compressed with a roller. Then, the laminate was placed on a release-treated flat mold, and a release film was laminated. And, a breather serving as an air flow path inside a vacuum bag was laminated on the release film with or without the lamination of a caul plate (steel) having the same size as that of the prepreg having a thickness of 2 mm, and finally wrapped with the vacuum bag, followed by sealing with sealant. Then, a fiber-reinforced composite material was prepared by curing the prepreg while maintaining at 125° C. for 30 minutes under a vacuum pressure of 28 inchHg.
A thickness, a rate of change in thickness, and a resin content were measured, respectively for the fiber-reinforced composite material prepared by using the caul plate and the fiber-reinforced composite material prepared without the caul plate.
The thickness was measured by measuring a thickness at eight points of total four corners with two points for each corner of a sample, and then obtaining an average value thereof, the rate of change in thickness was calculated from a percentage of difference in thickness before and after molding to a thickness before molding (Difference in thickness before and after molding/Thickness before molding*100), and the resin content was measured by the method described above.
3) Flexural Strength
A flexural strength of the fiber-reinforced composite material prepared by using the caul plate and the fiber-reinforced composite material prepared without the caul plate was measured with a universal tensile tester at a temperature of 23±2° C. according to ASTM D790.
4) Moisture Absorption Rate
A moisture absorption rate of the fiber-reinforced composite material prepared by using the caul plate and the fiber-reinforced composite material prepared without the caul plate was measured by completely immersing a sample in distilled water. Then, the moisture absorption rate was calculated by substituting a weight before immersion and a weight after immersion in the following Equation 1.
Moisture absorption rate (wt %)=(Weight of sample after immersion−Weight of sample before immersion)/Weight of sample before immersion *100 [Equation 1]
At this time, the weight before and after immersion was measured after primarily removing moisture from upper and lower portions and an edge of the sample with towel (five sheets of Kimwipes, dry fabric, etc.) and secondarily removing moisture from the upper and lower portions again with dry towel to completely remove the moisture visually.
| Number | Date | Country | Kind |
|---|---|---|---|
| 10-2019-0179683 | Dec 2019 | KR | national |
| 10-2020-0166676 | Dec 2020 | KR | national |
| Filing Document | Filing Date | Country | Kind |
|---|---|---|---|
| PCT/KR2020/018014 | 12/10/2020 | WO |
