http://rdf.ncbi.nlm.nih.gov/pubchem/patent/KR-102083915-B1
Outgoing Links
| Predicate | Object |
|---|---|
| classificationCPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2240-35 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23R3-286 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-22 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23R3-16 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F23R3-28 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C7-22 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F23R3-16 |
| filingDate | 2018-03-19-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate | 2020-03-03-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationDate | 2020-03-03-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | KR-102083915-B1 |
| titleOfInvention | Nozzle for combustor, combustor, and gas turbine including the same |
| abstract | The present invention provides a nozzle, a combustor, and a gas turbine capable of performing stratified multistage combustion. Combustor nozzle according to an aspect of the present invention, the inner nozzle portion for providing a fuel passage, the first injection is formed to surround the nozzle portion to form a first premix passage and injecting fuel to the first premix passage An outer tube having a hole formed therein and having a first inlet through which air is introduced, and installed to surround the outer tube to form a second premixed passage, and a nozzle shroud having a second inlet through which air is introduced; . |
| priorityDate | 2018-03-19-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 18.