http://rdf.ncbi.nlm.nih.gov/pubchem/patent/KR-20190101554-A

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filingDate 2018-02-23-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_1ff074967b42388e06143a260bd61d85
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_7d29bde2329108dccaf80b209f68b9e7
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publicationDate 2019-09-02-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber KR-20190101554-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 uniformly premixing fuel and air. The nozzle for the combustor according to an aspect of the present invention is formed to partially surround the inner tube and the inner tube providing the first premix passage through which the premixed air moves and to form an outer fuel passage through which the fuel moves. An integrated swirler including a plurality of vanes connected to the outer tube and having a discharge hole for discharging fuel, and a fuel injector having an inner fuel passage inserted into the inner tube and having fuel moved therein; The fuel injector may include a peg connected to the inner fuel passage and formed with a injection hole for injecting fuel into the first premix passage.
priorityDate 2018-02-23-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

Incoming Links

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Total number of triples: 28.