http://rdf.ncbi.nlm.nih.gov/pubchem/patent/KR-100554065-B1
Outgoing Links
| Predicate | Object |
|---|---|
| classificationCPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23G2209-14 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23G2202-102 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23G5-085 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23G5-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F23G5-027 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F23G5-00 |
| filingDate | 2003-01-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate | 2006-02-22-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationDate | 2006-02-22-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | KR-100554065-B1 |
| titleOfInvention | Waste treatment method using liquid propulsion engine and its device |
| abstract | The present invention relates to an apparatus and a method for treating waste by using a high temperature technology that can be obtained from a liquid propulsion engine of a rocket. The powder, liquid, and gaseous wastes are injected simultaneously with a liquid fuel and an oxidant, and then 2,500 ° C. to 3,500 ° C. After high temperature oxidation and pyrolysis, the gas discharged at high speed is re-burned at 1,000 ~ 2,500 ℃ to completely decompose and then released to the atmosphere by removing harmful gases such as NOx and acid gas (HCl, SOx). .n n n n Liquid Propulsion Engines, Waste |
| priorityDate | 2003-01-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 52.