| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_998cbe39a12d4bb364b8ad41ff5792dc
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_98a65034128826ed2fe2afe2c5acbf22
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_1ad7e00217cfc977a75e8d11bd8b5b57
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_bd66bcf8e4d10df2900953f1ae3d3349
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_0ab1efaeff6cca6e8bea029148dae6cb |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T50-60
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2270-082 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01N3-08
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D25-305 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F01D25-30
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C3-30 |
| filingDate |
2011-05-31-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_3a32d00ae1eef1983c74722e8d46f1e0
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_1daa5877f64d3fac6576143fd32fa11a
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_319c281ce562a9c5b46beacfd5cca2e0 |
| publicationDate |
2011-12-15-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
WO-2011154280-A1 |
| titleOfInvention |
Exhaust gas treatment of gas turbine engines |
| abstract |
The invention relates to gas turbine engines, especially a turbojet or turbofan for an aircraft. The gas turbine engine comprising a combustion section and an exhaust section produces an exhaust gas. The emission products can be reduced by using a gas treatment device with a reactor and an injection device. The reactor produces a nitrogeneous substance such as ammonia. This reducing agent is injected in the gas phase in the exhaust section of the gas turbine engine. By selective non catalytic reaction the Nitrogen oxides of the exhaust gas can be reduced. Furthermore the injection device is arranged such that the temperature window of this reduction process is ranging from 850°C to 1100 ° C. The reactor for producing gaseous ammonia can either be a thermal reactor or a high pressure plasma device. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-103971580-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-103971580-B |
| priorityDate |
2010-06-07-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |