| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_d622a0608e3aeef107d6d1c53e172695 |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23N2221-10
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02E20-16
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23N2223-36
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C9-48
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C9-50
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T50-60
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23N2241-20 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23C9-08
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C1-005
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-22
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C9-26
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23N5-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C9-28
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23N5-006
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C1-08
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C3-34
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23N5-18
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23N1-002
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23N1-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23N5-003
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C6-18 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C9-26
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C9-50
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F23N5-18
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F23C9-08 |
| filingDate |
2013-10-31-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_9ed2afacef286bacc7f71f74a0527259 |
| publicationDate |
2015-05-21-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
AU-2013374290-A1 |
| titleOfInvention |
Gas turbine combustor control system |
| abstract |
A gas turbine system includes a controller (118) configured to receive fuel composition information related to a fuel (70) used for combustion in a turbine combustor (160); receive oxidant composition information related to an oxidant (68) used for combustion in the turbine combustor (160); receive oxidant flow information related to a flow of the oxidant to the turbine combustor (160); determine a stoichiometric fuel-to-oxidant ratio based at least on the fuel composition information and the oxidant composition information; and generate a control signal for input to a fuel flow control system configured to control a flow of the fuel to the turbine combustor (160) based on the oxidant flow information, a target equivalence ratio, and the stoichiometric fuel-to-oxidant ratio to enable combustion at the target equivalence ratio in the presence of an exhaust diluent within the turbine combustor. |
| priorityDate |
2012-11-02-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |