http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2015108078-A

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filingDate 2013-12-05-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_86b276e89e90efae1c115efb1be2236b
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publicationDate 2015-06-11-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber JP-2015108078-A
titleOfInvention Epoxy resin composition, prepreg and fiber reinforced composite material
abstract A fiber reinforced composite material having a high fracture toughness value (so-called GIC) in mode I (interlaminar peeling deformation) and excellent in compressive strength after impact and interlaminar shear strength, which is optimal as a prepreg for structural materials for aircraft. Offer. An epoxy resin composition for prepreg comprising the following components (A), (B) and (C), a prepreg and a fiber reinforced composite material using the same. Component (A): epoxy resin represented by the following general formula (R1 to R5 are each independently H, halogen atom or C1-8 alkyl group) Component (B): 4,4′-diaminodiphenylsulfone component (C) : Nylon 12 fine particles [Selection figure] None
isCitedBy http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2020235484-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2019156981-A
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