http://rdf.ncbi.nlm.nih.gov/pubchem/patent/KR-20170018429-A

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filingDate 2015-06-12-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_66d11cdc5acb8fe8fbcf542210b75033
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publicationDate 2017-02-17-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber KR-20170018429-A
titleOfInvention Systems and methods for balancing thrust loads in a heat engine system
abstract The turbo pump system includes a pump portion including a housing having a pressure relief passage disposed therein. The pump portion is disposed between the high pressure side and the low pressure side of the working fluid circuit. The drive turbine is coupled to the pump portion and is configured to drive the pump portion to enable the pump portion to circulate the working fluid through the working fluid circuit. The pressure relief valve is fluidly coupled to the pressure relief passageway and is connected to an open position for enabling pressure relief through the pressure relief passage and to a closed position for disabling pressure relief through the relief passage And is configured to be positioned.
priorityDate 2014-06-13-04:00^^<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: 28.