| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_62f941494409aea84f621977c5f0ab81 |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02E20-34
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23C2900-03006 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23D14-66
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23C9-006
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23R3-42
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23R3-54
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23D17-002
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23C5-24
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23D14-22 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F23C9-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F23M3-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F23R3-54
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F23R3-42
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F23L1-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F23C5-24 |
| filingDate |
2005-06-09-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_b0445232d553d566c19e5ce812cf07e6
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_bb623fbd897422815bb18b508c8c09bf
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_37c3d788b7b8fc72f6bfc0d926a4a58d
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_024c7e546d34c429628f6936362f5a24
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_c6a4b19497220780ef0b56dd2abe4220
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_98cba5bcd63c57185733f758e67dd030 |
| publicationDate |
2006-08-17-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
CA-2574091-A1 |
| titleOfInvention |
Stagnation point reverse flow combustor for a combustion system |
| abstract |
A combustor assembly includes a combustor vessel having a wall, a proximate end defining an opening and a closed distal end opposite said proximate end. A manifold is carried by the proximate end. The manifold defines a combustion products exit. The combustion products exit being axially aligned with a portion of the closed distal end. A plurality of combustible reactant ports is carried by the manifold for directing combustible reactants into the combustion vessel from the region of the proximate end towards the closed distal end. |
| priorityDate |
2004-06-10-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |