| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_f1f2f2d5c061af6c111cdf6aca4c2112 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-48
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K9-97 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-97
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-48 |
| filingDate |
2015-08-27-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_087bb1f72b9ccf04eea13fdaf610df11
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_f85eb163fe961d8a9fda684c8332bb3f |
| publicationDate |
2016-03-17-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
WO-2016039993-A1 |
| titleOfInvention |
Liquid propellant rocket engine with afterburner combustor |
| abstract |
A liquid propellant rocket engine includes a combustion chamber that has a throat. A nozzle diverges from the throat. The nozzle includes an afterburner combustor section that has a fuel injector orifice. A gas generator includes an exhaust duct and there is at least one turbine that has a turbine inlet and a turbine outlet. The turbine inlet is fluidly coupled with the exhaust duct, and a turbine outlet is fluidly coupled with the fuel injector orifice. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-114991994-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2789943-C1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-114991994-B
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-112555056-A |
| priorityDate |
2014-09-12-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |