http://rdf.ncbi.nlm.nih.gov/pubchem/patent/KR-101957595-B1

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assignee http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_60f0f9fcc232efca2e6c8691ab540880
classificationCPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-14
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classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C7-14
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C7-16
filingDate 2017-10-11-04:00^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 2019-03-12-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_c9f671f3cde0f8af8609ce9b7d33ee2a
publicationDate 2019-03-12-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber KR-101957595-B1
titleOfInvention Fuel supplying system combustor and gas turbine having it
abstract The present invention relates to a fuel supply system for supplying fuel to a combustor and a gas turbine including the fuel supply system. The fuel supply system includes a fuel gas compressor and a cooling section. The cooling section uses the nanofluid as a refrigerant to prevent the fuel gas compressor from overheating even when the gas turbine is in a standby state. Therefore, it is possible to start operation immediately when the gas turbine in the standby state is operated.
priorityDate 2017-10-11-04:00^^<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: 34.