http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-112063117-B
Outgoing Links
| Predicate | Object |
|---|---|
| classificationCPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C08L2205-03 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C08L2205-025 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C08J2363-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C08J2483-04 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C08L63-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C08J5-24 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C08K7-06 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C08L83-05 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C08L83-04 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C08J5-24 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C08L63-00 |
| filingDate | 2020-09-23-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate | 2021-10-19-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationDate | 2021-10-19-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | CN-112063117-B |
| titleOfInvention | Ablation-resistant organic silicon modified epoxy resin-based carbon fiber composite material and preparation method thereof |
| abstract | The invention belongs to the field of polymer composite materials, and relates to an ablation-resistant organic silicon modified epoxy resin-based carbon fiber composite material and a preparation method thereof. The epoxy resin modified by the terminal methoxyl organosilicon is epoxy resin modified by the terminal methoxyl organosilicon. The ablation-resistant organosilicon modified epoxy resin-based carbon fiber composite material is a carbon fiber reinforced methoxy-terminated organosilicon modified epoxy resin composite material, and is prepared from carbon fiber cloth, methoxy-terminated organosilicon modified epoxy resin and a curing agent. The composite material provided by the invention has the properties of high temperature resistance and ablation resistance, and the carbon layer structure formed after ablation still has good mechanical properties, has a very good application prospect in the field of integration of low-cost ablation-resistant composite materials and structural ablation, and can be applied to the preparation of shell materials of aerospace aircrafts, ablation heat-proof structures of high-speed aircrafts in near space and atmosphere, spacecrafts, recoverable satellites and other aerospace equipment and the civil field. |
| priorityDate | 2020-09-23-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 47.