| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_733701ffd25619969a95ea5e4639061c
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_dcd7be4ad60873d6c8f19f119527ef17 |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02B90-10
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H01M2008-1293
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H01M2250-402
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H01M2250-407
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02E60-50
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H01M2250-20
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T90-40 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B60L58-30
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C6-10
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B60L58-34
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C1-05
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H01M8-04111
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C3-36 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C6-04
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B60W20-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B60W10-02 |
| filingDate |
2010-03-30-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_b76a71ade81dd060dc85545ecdb262e6 |
| publicationDate |
2012-04-05-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
US-2012083387-A1 |
| titleOfInvention |
Reheated gas turbine system, in particular such a system having a fuel cell |
| abstract |
The present invention relates to (with reference to FIG. 2 ) a gas turbine system comprising: a gas compressor ( 210 ); an upstream heat source, e.g. a fuel cell ( 212 ), which receives gas compressed by the compressor ( 210 ) and heats the gas passing therethrough (and when a fuel cell generates electrical power); an intermediate turbine ( 220 ) which receives the gas previously heated in the upstream heat source and which is connected to and drives the compressor ( 210 ); and an output turbine ( 240 ) which receives gas output by the intermediate turbine ( 220 ). Expanded gas leaving the intermediate turbine passes to the output turbine through either or both of a downstream combustion chamber and/or a downstream fuel cell, whereby the expanded gas is reheated prior to expansion in the output turbine ( 240 ). Preferably the system is configured such that the temperature of the gas received by the output turbine ( 240 ) is higher than the temperature of the gas received by the intermediate turbine ( 220 ). |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2015051818-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2014349808-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10107190-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-112796886-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-109592028-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11011761-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10914233-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2015053491-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/WO-2023143868-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-103206307-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2023212977-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-108069039-A |
| priorityDate |
2009-03-30-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |