http://rdf.ncbi.nlm.nih.gov/pubchem/patent/KR-101957595-B1
Outgoing Links
Predicate | Object |
---|---|
assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_60f0f9fcc232efca2e6c8691ab540880 |
classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-14 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-16 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C09K5-041 |
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 |
Incoming Links
Total number of triples: 34.