http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9347376-B2
Outgoing Links
Predicate | Object |
---|---|
assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_c72d118f5664072de841f9c5c34b9d99 |
classificationCPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2250-13 |
classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-224 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C3-22 |
classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C7-224 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C3-22 |
filingDate | 2013-04-24-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
grantDate | 2016-05-24-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_1e47d973335a4650b7ff2b9081f8ba31 |
publicationDate | 2016-05-24-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber | US-9347376-B2 |
titleOfInvention | Liquified fuel backup fuel supply for a gas turbine |
abstract | A system for supplying a gaseous fuel to a gas turbine includes a liquefied fuel source for supplying a liquefied fuel to a liquid fuel pump that is disposed downstream from the liquefied fuel source. The liquid fuel pump is sufficient to raise the pressure of the liquefied fuel to a substantially supercritical pressure. A supercritical liquefied fuel vaporizer is disposed downstream from the liquid fuel pump. A heat recovery system is in thermal communication with the liquefied fuel. The heat recovery system is positioned between the liquid fuel source and the supercritical liquefied fuel vaporizer. |
isCitedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11371711-B2 |
priorityDate | 2013-04-24-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 38.