| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_71a0056120827ca683cab863b7f0340c
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_c72d118f5664072de841f9c5c34b9d99
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_d43b306720f2f4d63fb1fac076b3864e
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_721d6508798abc4c07bfacd59397fbfa |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F04D29-284
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F04D29-44
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F04D29-441 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F04D29-44
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F04D21-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F04D29-284
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F04D17-127
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F04D29-28 |
| classificationIPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F04D29-28 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F04D21-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F04D17-12
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F04D29-44 |
| filingDate |
2009-06-25-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate |
2015-08-04-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_148940f64e8f3acf4d4f8d99a5abbb74
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_6b1d0122a745eedd1af4c43b959ff076
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_9c17f63496734e5cb5ebe9fd90f44cf4 |
| publicationDate |
2015-08-04-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
US-9097258-B2 |
| titleOfInvention |
Supersonic compressor comprising radial flow path |
| abstract |
The present invention provides novel supersonic compressors comprising novel supersonic compressor rotors. The supersonic compressor rotors are designed to operate at very high rotational speed wherein the velocity of the gas entering the supersonic compressor rotor is greater than the local speed of sound in the gas, hence the descriptor “supersonic”. The new supersonic compressors comprise at least one supersonic compressor rotor defining an inner cylindrical cavity and an outer rotor rim and at least one radial flow channel allowing fluid communication between the inner cylindrical cavity and the outer rotor rim, said radial flow channel comprising a supersonic compression ramp. The novel supersonic compressor rotors are expected to enhance the performance of supersonic compressors comprising them, and to provide for greater design versatility in systems comprising such novel supersonic compressors. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11346366-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2014234094-A1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11396887-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9982539-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-9909597-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10378551-B2 |
| priorityDate |
2009-06-25-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |