http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-108383391-B
Outgoing Links
| Predicate | Object |
|---|---|
| classificationCPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B2235-6023 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B41-009 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B35-14 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B35-622 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B38-0605 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B35-803 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B28B1-26 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B41-89 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C04B41-52 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C03C14-00 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C03C14-00 |
| filingDate | 2016-09-14-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate | 2021-04-30-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationDate | 2021-04-30-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | CN-108383391-B |
| titleOfInvention | Surface-toughened alumina fiber rigid heat-insulating tile multilayer composite material, coating composition, preparation method and application thereof |
| abstract | The invention relates to a surface-toughened alumina fiber rigid heat-insulating tile multilayer composite material, a coating composition, a preparation method and application thereof. The composite material comprises a porous alumina fiber matrix, a surface toughened alumina compact ceramic layer, a high-emissivity oxide thermal barrier coating and a low-chemical-catalytic-coefficient glass coating. The coating composition includes a surface toughened alumina dense ceramic layer composition, a high emissivity oxide thermal barrier coating composition, and a low chemical catalytic coefficient glass coating composition. The preparation method of the composite material comprises the steps of sequentially preparing the substrate, the compact ceramic layer, the thermal barrier coating and the glass coating. The invention also provides the use of the composite material in a thermal protection material for the outer surface of an aircraft. The invention adopts a novel process technology and utilizes a unique substrate and a coating composition to prepare the composite material which can be repeatedly used for a long time in an environment of 1600 ℃ and has excellent temperature resistance. |
| priorityDate | 2016-09-14-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 42.