http://rdf.ncbi.nlm.nih.gov/pubchem/patent/KR-20190109955-A

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filingDate 2018-03-19-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_6792e5981a5550ad50f60a3304841be6
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_7d29bde2329108dccaf80b209f68b9e7
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publicationDate 2019-09-27-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber KR-20190109955-A
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; .
isCitedBy http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-114659138-B
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11525579-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/KR-102382634-B1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-114659138-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11761633-B2
priorityDate 2018-03-19-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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Total number of triples: 28.