| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_eb7f5415eb96e8c132733b8cff7cc2c5 |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2260-205
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T50-60 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-224
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-16
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C3-30
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C3-20 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C9-50
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C7-12
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C9-26
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C7-22 |
| filingDate |
2014-03-14-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_44b6093f032901aabd69bb47b60152fa |
| publicationDate |
2014-12-18-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
WO-2014200597-A2 |
| titleOfInvention |
Fuel conditioner, combustor and gas turbine improvements |
| abstract |
Advanced gas turbines and associated components, systems and methods are disclosed herein. A gas turbine configured in accordance with a particular embodiment includes a rotor operably coupled to a shaft and a stator positioned adjacent to the rotor, A coolant line extends at least partially through the stator to transfer heat out of an air flow within a compressor section of the gas turbine. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10830094-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/EP-3301265-A1 |
| priorityDate |
2013-03-15-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |