http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2015108078-A
Outgoing Links
Predicate | Object |
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assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_cebc9740ef706cde29e885504f274ffa |
classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C08L63-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C08J5-24 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C08G59-28 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C08L77-02 |
filingDate | 2013-12-05-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_86b276e89e90efae1c115efb1be2236b http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_e8702cfb37316309b91caa2073691189 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_494188703a896e78df32ca840634bcac |
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 |
priorityDate | 2013-12-05-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 48.