http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9347376-B2

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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.
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