http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-107057781-B
Outgoing Links
| Predicate | Object |
|---|---|
| classificationCPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10G2300-1022 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L2270-04 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10G67-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L1-04 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C10G67-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C10L1-04 |
| filingDate | 2016-12-27-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate | 2018-09-28-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationDate | 2018-09-28-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | CN-107057781-B |
| titleOfInvention | A kind of high density, high heating value jet fuel |
| abstract | A kind of high density, high heating value jet fuel, its raw material composition includes the component that boiling range is 300 DEG C of 180 ﹣ in F T synthesis coal liquifactions, high-density propellant blend component, wherein, the component that boiling range is 300 DEG C of 180 ﹣ in F T synthesis coal liquifactions, the mass ratio of high-density propellant blend component is less than or equal to 5: 7, the high-density propellant blend component is using inferior heavy oil as raw material, it is the cycloalkane and aromatic hydrocarbons of 300 DEG C of 180 ﹣ and tail oil part by the boiling range that hydrofinishing obtains, the physicochemical property of high-density propellant blend component meets the standard of 3 jet fuels of RP, and its density is 960 ﹣ 980kg/m 3 , net heating value is 43.8 ﹣ 44.8MJ/kg.The design not only increases the density and calorific value of jet fuel, and production cost is low. |
| priorityDate | 2016-12-27-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 30.