| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_ac29389b816db7ae7fa345b16ba89a60
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_2505a9a738a1e2d378eb3e2c932f4981
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_6695ba89bab286ee5b174a2fdb50faab |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10G2400-08
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10G2300-308
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10G2300-1022 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10G2-30
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L1-04
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L1-08
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10G47-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10J3-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10G45-00 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C10G45-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C10G2-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C10J3-00
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C10G47-00 |
| filingDate |
2010-08-02-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_d76df70ddcc34ce7d6fa9eaec3f3ff39
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_e0acbf61e9edcfd311ead1e3946cabd2 |
| publicationDate |
2011-02-10-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
WO-2011017720-A1 |
| titleOfInvention |
Fully synthetic jet fuel |
| abstract |
The invention provides a fully synthetic aviation fuel or aviation fuel component having : " a total naphthenic content of more than 30 mass % " a mass ratio of naphthenic to iso-paraffinic hydrocarbon species of more than 1 and less than 15 " a density (at 15°C) of greater than 0.775 g.cm-3, but less than 0.850 g.cm-3 " an aromatic hydrocarbon content of greater than 8 mass %, but less than 20 mass % " a freezing point of less than - 47°C " a lubricity BOCLE WSD value of less than 0.85mm. The invention further provides for the preparation of a fully synthetic coal-derived aviation fuel or aviation fuel component by blending a LTFT and a tar derived blend component. The invention extends to a method of producing a coal-derived, fully synthetic aviation fuel or aviation fuel component from coal gasifier tar and an LTFT derived fraction. |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-11021666-B2
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/JP-2016501279-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2733388-C2 |
| priorityDate |
2009-08-03-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |