http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-104725777-B

Outgoing Links

Predicate Object
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C08K5-18
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C08K5-17
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C01B32-15
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C08L63-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C08K3-04
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filingDate 2013-12-19-04:00^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 2017-07-21-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationDate 2017-07-21-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber CN-104725777-B
titleOfInvention A kind of preparation of the epoxy resin-base of low-density high thermal stability
abstract The present invention relates to a kind of epoxy resin-base for fibre reinforced composites, the preparation of more particularly to a kind of epoxy resin-base containing hollow nano carbon ball belongs to field of compound material.Its preparation process is:(1)The preparation of hollow nano carbon ball;(2)In hollow nano carbon ball surface grafting amino-compound;(3)The hollow nano carbon ball of surface grafting amino-compound is added in epoxy resin, stirred, then removes bubble after being mixed with curing agent, hollow nano carbon ball/epoxy resin-base is obtained.Hollow nano carbon ball/the epoxy resin-base has the advantages that low-density, high-modulus and good heat endurance, may be used as carbon fiber, glass fibre or aramid fiber strengthens the matrix of composite, is widely used in the preparation of the field such as Aeronautics and Astronautics, the energy, traffic composite material component.
priorityDate 2013-12-19-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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