Epoxy resin composition and fiber reinforced composite material
US-2017327652-A1 · Nov 16, 2017 · US
US9434811B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9434811-B2 |
| Application number | US-201013634518-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 24, 2010 |
| Priority date | Mar 23, 2010 |
| Publication date | Sep 6, 2016 |
| Grant date | Sep 6, 2016 |
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Disclosed is a carbon-fiber-reinforced composite material that is suitable for use as a construction material and exhibits high mechanical strength in harsh usage environments such as low-temperature environments and high-temperature moisture-absorbing environments. Also disclosed are an epoxy resin composition for producing the aforementioned carbon-fiber-rein-forced composite material and a prepreg obtained through the use of said epoxy resin composition. Said epoxy resin composition comprises at least the following constituents, by mass with respect to the total mass of the composition: (A) between 20% and 80% of an epoxy resin having the structure represented by formula (1); and (B) between 10% and 50% of an epoxy resin that has at least two ring structures with four or more members each and also has one amine glycidyl or ether glycidyl directly connected to a ring structure.
Opening claim text (preview).
The invention claimed is: 1. An epoxy resin composition for use in a carbon fiber reinforced composite material, comprising at least the following components [A] and [B], wherein the content of [A] is 20 to 80 mass % and the content of [B] is 25 to 50 mass % per 100 mass % as the total amount of the mixed epoxy resins, [A]: an epoxy resin with one or more amine type glycidyl groups at the meta position(s), wherein [A] is tetraglycidyl-3,4′-diaminodiphenylether or tetraglycidyl-3,3′-diaminodiphenylether, [B]: a bifunctional epoxy resin with two or more four- or larger-membered ring structures and one amine type glycidyl group directly bonded to one of the ring structures, wherein [B] contains a diphenylether, and the epoxy resin [B] is at least one selected from the group consisting of diglycidyl-p-phenoxyaniline, diglycidyl-4-(4-methylphenoxy)aniline, diglycidyl-4-(3-methlyphenoxy)aniline, diglycidyl-4-(2-methlyphenoxy)aniline, diglycidyl-4-(4-ethylphenoxy)aniline, diglycidyl-4-(3-ethylphenoxy)aniline, diglycidyl-4-(2-ethylphenoxy)aniline, diglycidyl-4-(4-propylphenoxy)aniline, diglycidyl-4-(4-tert-butylphenoxy)aniline, diglycidyl-4-(4-cyclohexylphenoxy)aniline, diglycidyl-4-(3-cyclohexylphenoxy)aniline, diglycidyl-4-(2-cyclohexylphenoxy)aniline, diglycidyl-4-(4-methoxyphenoxy)aniline, diglycidyl-4-(3-methoxyphenoxy)aniline, diglycidyl-4-(2-methoxyphenoxy)aniline, diglycidyl-4-(3-phenoxyphenoxy)aniline, diglycidyl-4-(4-phenoxyphenoxy aniline, diglycidyl-4-[4-trifluoromethyl)phenoxy]aniline, diglycidyl-4-[3-(trifluoromethyl)phenoxy]aniline, diglycidyl-4-[2-(trifluoromethyl)phenoxyl]aniline, diglycidyl-p-(2-naphthyloxyphenoxy)aniline, diglycidyl-p-(1-naphthyloxyphenoxy)aniline, diglycidyl-4-[(1,1′-biphenyl-4-yl)oxy]aniline, diglycidyl-4-(4-nitrophenoxy)aniline, diglycidyl-4-(3-nitrophenoxy)aniline diglycidyl-4-(2-nitrophenoxy)aniline, diglycidyl-4-(4-methylphenoxy)aniline diglycidyl-4-(3-methylphenoxy)aniline, diglycidyl-4-(2-methylphenoxy)aniline, diglycidyl-4-(4-ethylphenoxy)aniline, diglycidyl-4-(3-ethylphenoxy)aniline, diglycidyl-4-(4-tert-butylphenoxy)aniline, diglycidyl-4-(4-cyclohexylphenoxy)aniline, diglycidyl-p-(2-naphthyloxyphenoxy)aniline. 2. An epoxy resin composition for use in a carbon fiber reinforced composite material, according to claim 1 , which further contains the following [C], [C]: A thermoplastic resin dissolvable in the epoxy resins. 3. A prepreg comprising carbon fibers impregnated with the epoxy resin composition set forth in claim 1 . 4. A carbon fiber reinforced composite material obtained by curing the prepreg set forth in claim 3 . 5. A carbon fiber reinforced composite material comprising the cured resin product obtained by curing the epoxy resin composition set forth in claim 1 , and carbon fibers. 6. A aircraft structural member or windmill blade comprising the carbon fiber reinforced composite material according to claim 5 .
Impregnating materials with prepolymers which can be polymerised in situ, e.g. manufacture of prepregs · CPC title
Compounds containing acyclic nitrogen atoms · CPC title
Compositions of epoxy resins; Compositions of derivatives of epoxy resins · CPC title
Characterised by the use of epoxy resins; Derivatives of epoxy resins · CPC title
containing two or more polymers of the same C08L -group · CPC title
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