http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-107630768-B
Outgoing Links
| Predicate | Object |
|---|---|
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-36 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C23C4-134 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C23C4-11 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C23C4-073 |
| filingDate | 2017-08-16-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate | 2019-09-17-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationDate | 2019-09-17-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | CN-107630768-B |
| titleOfInvention | A kind of missile propulsive plant band thermal barrier coating grate structure |
| abstract | The present invention provides a kind of missile propulsive plant band thermal barrier coating grate structure, including the double-deck engraved structure metallic matrix, is sprayed at the thermal barrier coating of the metal base surface, the thermal barrier coating includes metal adhesion layer and insulating ceramic layer；The material of the metallic matrix uses high strength steel；Metal adhesion layer uses MCrAlY system alloy, and thermal insulation ceramics layer material uses nanometer ZrO 2 Aggregate powder of AI/Yt. |
| priorityDate | 2017-08-16-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 16.