| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_cf82ac8ce63edd1612057a79e0de2f42 |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2240-302
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2220-76 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C3-085
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K7-10
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D1-34
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F04D21-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C6-02 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C3-08
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F04D21-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C6-02
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F01D1-34
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K7-10 |
| filingDate |
2003-09-25-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_a837484567e9d7787137933b7f32097b
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_ca90d38f1ef0cccb2a9a4f93fc6ae098
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_a68a02915ce6e5b7db97a3db6e4b417c |
| publicationDate |
2004-04-08-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
WO-2004029432-A2 |
| titleOfInvention |
Gas turbine power plant with supersonic gas compressor |
| abstract |
A gas turbine engine. The engine is based on the use of a gas turbine driven rotor having a compression ramp traveling at a local supersonic inlet velocity (based on the combination of inlet gas velocity and tangential speed of the ramp) which compresses inlet gas against a stationary sidewall. The supersonic compressor efficiently achieves high compression ratios while utilizing a compact, stabilized gasdynamic flow path. Operated at supersonic speeds, the inlet stabilizes an oblique/normal shock system in the gasdyanamic flow path formed between the rim of the rotor, the strakes, and a stationary external housing. Part load efficiency is enhanced by use of a lean pre-mix system, a pre-swirl compressor, and a bypass stream to bleed a portion of the gas after passing through the pre-swirl compressor to the combustion gas outlet. Use of a stationary low NOx combustor provides excellent emissions results. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-102410249-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2009501550-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-108104977-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-7670109-B2 |
| priorityDate |
2002-09-26-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |