Epoxy resin system for manufacturing fiber-reinforced composites

文档序号：1549064 发布日期：2020-01-17 浏览：29次中文

阅读说明：本技术 用于制造纤维增强型复合材料的环氧树脂系统 (Epoxy resin system for manufacturing fiber-reinforced composites ) 是由 L·洛蒂 T·A·莫利 N·杰立卡 Z·西克曼 R·科尼哲于 2018-04-10 设计创作，主要内容包括：一种双组分可固化环氧树脂系统,其具有含有两种或超过两种环氧树脂的独特组合的环氧组分,所述环氧树脂中的至少一种为环氧酚醛清漆类型树脂。由这种树脂系统制得的复合材料显示出高玻璃化转变温度。(A two-part curable epoxy resin system having an epoxy component containing a unique combination of two or more epoxy resins, at least one of which is an epoxy novolac type resin. Composites made from such resin systems exhibit high glass transition temperatures.)

1. A curable resin system, comprising:

i. an epoxy resin component having two or more epoxy resins, wherein at least one of the two or more resins is a tetraglycidyl ether of an alkylenediphenylamine and another of the two or more resins is selected from the group consisting of: (a) diglycidyl ethers of bisphenol a or bisphenol F; (b) a novolac resin having an average glycidyl group per molecule in the range of more than 2 to 4; (c) a diglycidyl ether of a linear aliphatic diol or (d) a combination of two or more of (a) to (c), with the proviso that the amount of component (b) is less than 50 weight percent of the epoxy resin component;

a hardener component which is a cycloaliphatic compound having two or more amine groups.

2. The curable resin system of claim 1, wherein the composition further comprises a catalyst.

3. The curable resin system of claim 2, wherein the catalyst comprises at least one of an imidazole or a compound having an imidazoline ring structure, and the catalyst is part of the hardener component.

4. A curable resin system according to any preceding claim, wherein the epoxy resin component contains the tetraglycidyl ether of alkylenediphenylamine in an amount of 20 to 95 wt.%, based on the total weight of the epoxy resin component.

5. A curable resin system according to any one of claims 2 to 4, wherein the catalyst is present in an amount of from 0.1 to 20 wt% based on the total combined weight of the hardener and catalyst.

6. A curable resin system according to any preceding claim, wherein the epoxy resin component comprises 20 to 70 wt% of tetraglycidyl ether of alkylene diphenylamine, 5 to 60 wt% of diglycidyl ether of bisphenol a, and 5 to 50 wt% of a novolac resin having an average glycidyl group content per molecule in the range of 3 to 4, based on the total weight of the epoxy resin component.

7. A curable resin system according to any one of claims 1 to 5, wherein the epoxy resin component comprises 80 to 95 wt% of a tetraglycidyl ether of an alkylene diphenylamine and 5 to 20 wt% of a diglycidyl ether of a linear aliphatic diol.

8. The curable resin system of any one of claims 1 to 5 and 7, wherein the diglycidyl ether of the linear aliphatic diol is n-propylene glycol diglycidyl ether, n-butylene glycol diglycidyl ether, n-pentylene glycol diglycidyl ether, or n-hexylene glycol diglycidyl ether.

9. A curable resin system according to any one of the preceding claims, wherein the tetraglycidyl ether of alkylenediphenylamine is a tetraglycidyl ether of diaminodiphenylmethane.

10. A curable resin system according to any preceding claim, wherein the hardener component is 1, 2-diaminocyclohexane.

11. A curable resin system according to any preceding claim, which when the components are metered through an epoxy mixer and at a mould temperature of 135 ℃, has a gel time of less than 90 seconds.

12. The curable resin system of any of the preceding claims, wherein the epoxy blend exhibits a viscosity of less than 800 mPa.s at 80 ℃.

13. The curable resin system of any one of the preceding claims, wherein the composition further comprises one or more impact modifiers, internal mold release agents, pigments, or antioxidants.

14. A curable resin system according to any preceding claim, wherein (a) is bisphenol a.

15. A fiber-reinforced composite comprising the curable resin system according to any one of the preceding claims and a fiber composition, wherein the fiber composition is a continuous fiber material, a non-woven fiber material, a mat or a stack of two or more mats, or a material comprising continuous fibers and discrete fibers, and wherein the fiber composition is selected from carbon fibers, glass fibers, ceramic fibers, acrylonitrile fibers, aramid fibers, or hybrids thereof.

16. The fiber-reinforced composite of claim 15, having a glass transition onset greater than or equal to 200 ℃.

17. An automobile wheel rim produced by resin transfer molding or wet press molding using the fiber-reinforced composite material according to any one of claims 15 to 16.

Technical Field

The present invention relates to an epoxy-based composition and a method for preparing a fiber-reinforced composite material.

Background

Reinforced polymeric composites have several advantages over metal parts (e.g., parts in vehicles), including better corrosion resistance, the ability to produce parts with complex geometries, and in some cases superior strength to weight ratios. As a result, the transportation industry has begun to use such reinforced polymeric composites in place of metallic structural elements, such as chassis members and other structural supports.

Epoxy systems are sometimes used as the polymer phase in such composites. The cured epoxy is typically very strong and rigid and adheres well to the reinforcement. The advantage of epoxy resin systems compared to most thermoplastic systems is the use of low molecular weight and low viscosity precursors as starting materials. Low viscosity is an important attribute because it makes the resin system susceptible to penetration and wet-out between the fibers that typically form the reinforcement during such fiber injection processes (e.g., resin transfer molding or wet-pressing).

However, a resin system with improved resistance to heat-induced aging degradation, and in particular a system that better retains its mechanical properties, is desired.

Disclosure of Invention

The present invention is based on the discovery that: systems using two or more specific epoxy components show only a small reduction in mechanical properties after heat aging and after underwater aging (e.g. at 80 ℃).

Thus, according to one embodiment, the present invention is a curable resin system comprising i.an epoxy resin component having two or more epoxy resins, wherein at least one of the two or more resins is a tetraglycidyl ether of an alkylene diphenylamine and another of the two or more resins is selected from: (a) diglycidyl ether of bisphenol a, (b) a novolac resin having an average glycidyl group per molecule in a range of 3 to 4, (c) a diglycidyl ether of a linear aliphatic diol, or (d) a combination of two or more of (a) to (c), with the proviso that the amount of component (b) is less than 50% by weight of the epoxy resin component; a hardener component which is a cycloaliphatic compound having two or more amine groups. Preferably, the system also contains a catalyst, most preferably incorporated in the harder component.

Detailed Description

1. Epoxy component

In the present invention, the epoxy component contains two or more epoxy resins.

The first epoxy resin is a tetraglycidyl ether of an alkylene diphenylamine. Preferably, the resin is a tetraglycidyl ether of lower alkylene groups (1-3 carbon atoms), most preferably methylenedianiline. The amount of such first epoxy resin is preferably at least 20 wt%, and preferably not more than 95 wt%, more preferably not more than 75 wt%, even more preferably not more than 70 wt%, and most preferably not more than 65 wt%, based on the total weight of the epoxy resin.

The additional epoxy resin is selected from: (a) diglycidyl ethers of bisphenols (preferably bisphenol a or bisphenol F), (b) a novolac resin having an average glycidyl group per molecule in the range of 3 to 4, (c) a diglycidyl ether of a linear aliphatic diol, or (d) a combination of two or more of (a) to (c).

When epoxy resin (a) is used, epoxy resin (a) is preferably present in an amount of at least 15 wt.%, more preferably at least 20 wt.% and not more than 80 wt.%, preferably not more than 60 wt.%, based on the total weight of the epoxy resin.

The epoxy resin (b) is an epoxy novolac resin. Us patent No. 2,829,124 teaches the synthesis of similar epoxy novolac resins, which have since been widely used in a variety of different applications involving high glass transition temperature compounds. Epoxy novolac resins useful in the present invention can generally be described as methylene bridged polyphenolic compounds, in which some or all of the phenolic groups are capped with an epoxy-containing group, typically by reacting the phenolic groups with epichlorohydrin to form the corresponding glycidyl ethers. The phenol ring may be unsubstituted or may contain one or more substituents, which if present, are preferably alkyl groups having up to six carbon atoms, more preferably methyl groups. The epoxy novolac resins suitable for use in the present invention have an epoxy equivalent weight (in g/eq) of at least about 150, preferably at least 156, more preferably at least 170 and no more than 300, preferably no more than 225, and most preferably no more than 190. The epoxy novolac resin may contain, for example, an average of 2 to 4, preferably 3 to 4, epoxy groups per molecule. Suitable epoxy novolac resins are those having the general structure:

wherein l is an integer of at least 0, preferably at least 1 and not more than 8, more preferably not more than 4 and most preferably not more than 3, each R' is independently alkyl or inertly substituted alkyl, and each x is an integer of 0 to 4, preferably 0 to 2 and more preferably 0 to 1. If present, R' is preferably methyl.

When novolac epoxy resin (b) is used, novolac epoxy resin is present in an amount of no more than 50 wt.%, more preferably no more than 40 wt.% and at least 5 wt.%, more preferably at least 20 wt.%, based on the total weight of the epoxy resin.

According to a preferred embodiment, the epoxy component is a ternary blend of a tetraglycidyl ether of an alkylenediphenylamine, an epoxy resin (a), and an epoxy resin (b), and the combined total amount of epoxy resins (a) and (b) does not exceed 60 weight percent, based on the total weight of the epoxy resins.

The third epoxy resin (c) may also be used in combination with a tetraglycidyl ether of an alkylenediphenylamine. This third resin is a diglycidyl ether of a linear aliphatic diol. The linear dialiphatic diols preferably have from 2 to 6 carbon atoms. Specific examples include 1, 4-butanediol diglycidyl ether (BDDGE) commercially available as DER 731 from Olin Corporation (Olin Corporation) and 1, 6-hexanediol diglycidyl ether (HEXDGE) commercially available as DER 734 from Olin Corporation. When such an epoxy resin (c) is used, the epoxy resin is used in an amount of preferably at least 5% by weight and preferably not more than 20% by weight based on the total weight of the epoxy resin.

The viscosity of the resin component at 80 ℃ is less than 800 mPas, preferably less than 600 mPas. Viscosity is measured by astm d 2196.

2. Hardener component

The hardener component of the resin system of the present invention is a cycloaliphatic compound containing at least two amine groups for reaction with the epoxy resin. Typical examples of cycloaliphatic amines include isophorone diamine (CAS 2855-13-2), blends of 2-methylcyclohexane-1, 3-diamine and 4-methylcyclohexane-1, 3-diamine (CAS 13897-55-7), blends of cis and trans isomers of cyclohexane-1, 2-diamine (commonly referred to as DACH, CAS 694-83-7), 4' -diaminodicyclohexylmethane (CAS1761-71-3), 1, 4-cyclohexanediamine (CAS 2549-93-1), and others. In a preferred embodiment, the hardener component of the present invention contains more than 80 weight percent, and in a more preferred embodiment more than 90 weight percent, DACH, based on the total weight of the hardener component.

The hardener component is combined with the epoxy component in amounts such that at least 0.80 epoxy equivalents per amine hydrogen equivalent provided by the epoxy component is provided to the reaction mixture of the two components. Preferred amounts are at least 0.90 epoxy equivalents per amine hydrogen equivalent, and even more preferred amounts are at least 1.00 epoxy equivalents per amine hydrogen equivalent. The epoxy component may be provided in a large excess, such as up to 10 epoxy equivalents per amine hydrogen equivalent, but preferably does not provide more than 2.00 epoxy equivalents, more preferably not more than 1.25 epoxy equivalents and still more preferably not more than 1.10 epoxy equivalents per amine hydrogen equivalent. Thus, according to certain embodiments, the amount of hardener is at least 15 parts by weight, more preferably at least 20 parts by weight, and no more than 35 parts by weight, preferably no more than 30 parts by weight, based on 100 parts of epoxy resin.

3. Catalyst and process for preparing same

According to a preferred embodiment, the present invention also provides for the use of a separate catalyst to promote the polymerization reaction between the hardener and the epoxy resin, as opposed to relying on the hardener alone. In a preferred embodiment, the catalyst is first added to the hardener component before it is mixed with the resin component.

The catalyst may be used in combination with one or more other catalysts. If such added catalysts are used, suitable catalysts include those described in, for example, U.S. Pat. Nos. 3,306,872, 3,341,580, 3,379,684, 3,477,990, 3,547,881, 3,637,590, 3,843,605, 3,948,855, 3,956,237, 4,048,141, 4,093,650, 4,131,633, 4,132,706, 4,171,420, 4,177,216, 4,302,574, 4,320,222, 4,358,578, 4,366,295, and 4,389,520, and WO 2008/140906, all of which are incorporated herein by reference. Examples of suitable catalysts are molecules containing imidazole or imidazoline ring structures, such as 1-methyl-imidazole, 2-methylimidazole, 2-ethyl-4-methylimidazole, 2-phenylimidazole, 2-methyl-2-imidazoline, 2-phenyl-2-imidazoline; tertiary amines such as triethylamine, tripropylamine, N-dimethyl-1-phenylmethylamine, 2,4, 6-tris (dimethylamino-methyl) phenol and tributylamine; organophosphonium salts such as ethyltriphenylphosphonium chloride, ethyltriphenylphosphonium bromide and ethyltriphenylphosphonium acetate; ammonium salts such as benzyltrimethylammonium chloride and benzyltrimethylammonium hydroxide; various carboxylic acid compounds, and mixtures of any two or more thereof. In a preferred embodiment, the catalyst is from the class of imidazole or imidazoline compounds having phenyl substituents, such as 2-phenylimidazole or 2-phenyl-2-imidazoline.

The resin system of the present invention generally comprises at least 0.1 wt%, preferably at least 1 wt%, more preferably at least 2 wt% and not more than 20 wt%, more preferably not more than 5 wt% of the catalyst component, based on the total weight of the hardener component.

4. Other Components in the resin System

In addition, the resin system may contain optional components such as impact modifiers, mold release agents, pigments, dyes, inks, preservatives (e.g., uv blockers), and antioxidants.

In other embodiments, the resin composition may further comprise a toughening agent. The toughening agent functions by forming a second phase within the polymer matrix. This second phase is rubbery and/or softer than the polymer matrix formed in the absence of the toughening agent, and therefore can prevent crack growth, providing improved impact toughness. Toughening agents may include polysulfones, silicon-containing elastomeric polymers, polysiloxanes, elastomeric polyurethanes, and others.

Suitable toughening agents include natural or synthetic polymers having a Tg of less than-20 ℃. Such synthetic polymers include natural rubber, styrene-butadiene rubber, polybutadiene rubber, isoprene rubber, polyethers (e.g., polypropylene oxide, polytetrahydrofuran) and butylene oxide-ethylene oxide block copolymers, core-shell rubbers, elastomeric polyurethane particles, mixtures of any two or more of the foregoing, and the like. The rubber is preferably present in the form of small particles dispersed in the polymer phase of the resin system. The rubber particles may be dispersed in the epoxy resin and/or in the hardener.

It is generally preferred to cure the epoxy resin and hardener mixture in the presence of an internal mold release agent. Such internal mold release agents may comprise up to 5%, more preferably up to about 1% of the total weight of the resin composition. Suitable internal mold release agents are well known and commercially available, including those commercially available as Marbalase from Rex corporation of America (Rexco-USA)^TMAnd Mold-Wiz, commercially available from Axel Plastics Research Laboratories, Inc^TMChemlease, marketed by Kentucky (Chem-Trend)^TMPAT commercially available from W ü rtz GmbH^TMWaters Aerospace Release marketed by Zyvax and Kantstik marketed by Specialty Products Co^TM. In addition to (or instead of) adding the internal mold release agent during mixing, it is also possible to incorporate such an internal mold release agent into the epoxy component and/or the hardener component before the epoxy component and hardener component are mixed together.

Suitable particulate fillers have an aspect ratio of less than 5, and preferably less than 2, and do not melt or thermally degrade under the curing reaction conditions. Suitable fillers include, for example, pigments; a glass sheet; glass microspheres; aramid particles; carbon black; a carbon nanotube; various clays such as montmorillonite, halloysite, phillipsite; and other mineral fillers such as wollastonite, talc, mica, titanium dioxide, barium sulfate, calcium carbonate, calcium silicate, flint powder, emery, molybdenum silicate, sand, and the like. Some fillers are somewhat conductive, and the presence of such fillers in the composite material can increase the electrical conductivity of the composite material itself. In some applications, particularly automotive applications, it is preferred that the composite be sufficiently electrically conductive such that a coating can be applied to the composite using an electrophoretic coating (E-coat) process, wherein an electrical charge is applied to the composite and the coating is electrostatically attracted to the composite. This type of conductive filler comprises metal particles (such as aluminum and copper), graphene carbon black, carbon nanotubes, graphite, and the like.

5. Resin system

The hardener component is combined with the epoxy component in the amounts described above.

In some embodiments, the resin system of the present invention, when cured at a temperature comprised between 60 ℃ and 180 ℃, preferably 80 to 150 ℃, has a gel time of at least 15 seconds, at least 20 seconds, or preferably at least 30 seconds and a demold time of no more than 360 seconds, preferably no more than 300 seconds, and still more preferably no more than 240 seconds.

The thermosetting resin is formed from the resin system of the present invention by mixing the epoxy component, hardener component and preferably catalyst with any desired optional components in the proportions as described above and curing the resulting mixture. Any or all of the components can be preheated prior to mixing with each other, if desired. Preferably, the epoxy component is combined with the hardener component immediately prior to or simultaneously with forming the shaped article. It is often necessary to heat the mixture to an elevated temperature to achieve rapid curing.

In a molding process (e.g., a process for preparing a molded composite material), a curable reaction mixture is introduced into a mold, which may be preheated along with any reinforcing fibers and/or inserts as the curable reaction mixture may be included in the mold. The resin system of the present invention is particularly suitable for fiber injection to form composite materials, such as by resin transfer molding or wet press molding.

The resin system is used to form a resin composite material by resin transfer molding or wet compression molding using a fiber composite material selected from a continuous fiber material, a non-woven fiber material, a long strand fiber material (e.g., 10mm to 2000mm), a mat or stack of mats made of randomly arranged fibers having different lengths (5mm to 200mm), and combinations thereof. The fibers may be glass fibers, ceramic donors, carbon fibers, aramid fibers, acrylonitrile fibers, or combinations thereof. The weight ratio of the amount of fibres to resin system is 40 to 80 wt%, preferably 55 to 75 wt%.

The glass transition temperature of the composite material obtained by ASTM D5023(2015) is preferably at least 200 ℃, more preferably 215 ℃.

The cured resin system (neat, i.e., non-composite) has a tensile strength greater than 45MPa and a flexural strength greater than 90 MPa.

6. Thermal post-curing

The thermal post-cure process provides for cross-linking of the macromolecules outside of the mold used to make the composite. The advantages of a similar curing carried out outside the mold are related to the productivity and, in terms of possible room temperature ageing, include an increase of the glass transition temperature to values much higher than the initial Tg measured for the compound shortly after demolding.

The time for using the mould is very short, both in terms of productivity and in terms of possible cross-linking operating inside the mould, involving an external post-curing protocol (for example in an oven). Thus, many of the demolded parts can be sequentially cured together in a common oven while continuing to produce with the mold. A prerequisite for a high-temperature post-curing operation is that the part is removed from the mould without any appreciable deformation, i.e. after a predetermined suitable demoulding time.

On the other hand, the crosslinking must be carried out at a temperature which is in principle higher than the glass transition temperature of the polymer when it is released from the mold. Indeed, some mobility of the macromolecular chains will contribute to the kinetics of crosslinking; a similar situation of mobile macromolecular chains is achieved when the polymer is heated above its Tg. If curing is carried out below the Tg, only a slight improvement, or even no improvement at all, in the final Tg is observed, on the contrary.

The following examples are provided to illustrate the invention, but not to limit its scope. All parts and percentages are by weight unless otherwise indicated.

Examples of the invention

The resin system formulation was prepared by mixing the amounts of epoxy resins set forth in table 1a to form the epoxy component. The viscosity of the resin component was measured using a viscometer according to ASTM D2196. The purpose of measuring the neat resin viscosity is to see if it can be processed using a conventional epoxy meter. The 1, 2-diaminocyclohexane hardener was mixed with the stated catalyst (no catalyst used for hardener 3).

The gel time and open time (Tack-free time) were determined as follows: the mixture of epoxy component and curing agent component was mixed in a cup with a spatula, poured onto a hot plate thermostatted at 135 ℃ and pre-treated with a release agent (Muench-Chemie Mikon W-31 +). The gel time was defined as: when the spatula is repeatedly pulled through the poured liquid, the time at which the liquid no longer reorganizes into a horizontal surface, that is, the liquid no longer gathers together after the spatula is pulled through the liquid itself.

Pure resin samples for each test were made as follows: the reaction mixture was poured into a 2mm thick mold thermostated at 135 ℃ and pretreated with a mold release agent (Muench-Chemie Mikon W-31+) and the amounts of the components were mixed again in a cup with a spatula. After pouring the appropriate amount of reaction mixture for 5 minutes (i.e. completely filling the mold), the mold was opened and a 2mm thick plaque of non-reinforced resin was removed. Tensile strength and tensile modulus (according to EN 527-1) and flexural modulus (according to ASTM D790) were tested on these samples.

A unidirectional carbon composite is prepared using a wet-pressing technique. The reaction mixture was poured unidirectionally onto a carbon fiber fabric (DowAksa a42) (6 layers on a table); the carbon fiber fabric, which had been wetted with the reaction mixture, was then transferred into an open, thermostatted mold (540X290 mm X2mm thick, temperature 135 ℃) which was located in a press capable of delivering a pressure of 200 bar. After placing the fabric at the bottom of the mold, the press was slowly closed to a final thickness of 2 mm; the material was then cured in the press for five minutes. After five minutes, the press was opened and the composite part was removed. The amount of the reaction mixture was adjusted relative to the weight of the fibers such that the final indicating fiber weight fraction in the composite was about 61 weight percent. The samples were subjected to an Interlaminar Shear Strength test (according to EN ISO 14130) and a glass transition temperature (according to ASMT D5023). The results are shown in table 1 b:

some samples were subjected to hot water aging tests. The neat resin samples were subjected to hot water (80 ℃) aging. Two neat resin samples of size 60x12x2mm were used for this experiment; after a pretreatment at 110 ℃ for 24 hours and cooling to room temperature in a desiccator for 24 hours, the first sample was tested for Tg by DMA, while the other sample was soaked in hot water (80 ℃) and placed in an oven to maintain this temperature for 60 days. The weight was checked daily. At the end of 60 days, the Tg was checked.

Hot water (80 ℃) aging treatment of the carbon composite material part. Two DMA samples of carbon composite parts of size 60x12x2mm and twelve ILSS (EN 14130) samples of size 20x10x2mm were used. The 6 ILSS and 1 DMA samples were tested prior to aging and the remaining six ILSS and one DMA sample were tested after 21 days of immersion in hot water (80 ℃).

Before and after thermal cycling, composite samples were tested by DMTA analysis (according to ASTM 5023) to determine the effect of heat on Tg. The thermal cycling is performed by exposing the composite part to high temperatures (particularly 230 ℃). 20 cycles were performed and this simulated the environmental conditions of the composite part subjected to repeated heating. Composite boards of the previously described dimensions (540x290x2mm) were placed on the bottom of a preheating oven, made of steel, so that the composite surface was in full contact with the bottom of the oven. In the first experiment, the temperature of the composite material on the surface not in contact with the furnace bottom was measured by means of a thermocouple reader equipped with a thermocouple of the K type installed on the upper surface of the composite material. The temperature of the plate reached a steady (225 ± 5) ° c within 2 minutes; after 15 minutes of exposure, the oven was opened, the composite panel was removed and cooled on a wooden table. The temperature reaches (30 +/-5) DEG C within 10 minutes.

TABLE 1a