Predicate |
Object |
assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_a2a99738c564d0d4da77d442ec8f7500 http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_37142d3fe55b2069b230f41b616b26a3 http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_a874da8c7d5cd8fe1d4a8d9143a067c3 |
classificationCPCAdditional |
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classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10G45-70 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10G45-04 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10G45-68 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L1-04 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L1-16 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B01J21-00 |
classificationIPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B01J23-883 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B01J23-888 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B01J23-85 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B01J29-16 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B01J29-14 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B01J21-12 |
classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C10L1-04 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C10G45-70 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C10G45-68 |
filingDate |
2011-08-12-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
grantDate |
2015-10-27-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_502af518361959e889a50bddf4d71451 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_54ee10f93f7f4f6ae7fc73a58c822693 |
publicationDate |
2015-10-27-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber |
US-9169451-B2 |
titleOfInvention |
Jet fuels having superior thermal stability |
abstract |
Disclosed herein are jet fuel compositions containing (a) a total aromatics content of from 2 vol. % to no more than about 25 vol. %; (b) a net heat of combustion of at least about 125,000 Btu/gal; (c) a concentration of less than about 5 vol. % of hydrocarbons having a boiling point greater than or equal to about 550° F., as determined by ASTM D 2887; and (d) a Jet Fuel Thermal Oxidation Test (JFTOT) thermal stability characterized by a filter pressure drop of no more than 25 mm Hg, a breakpoint temperature greater than or equal to about 300° C., and an overall tube deposit rating less than 3, as determined by ASTM D 3241. Methods for their preparation are also disclosed. |
isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10676684-B2 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2016319208-A1 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-10767131-B2 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2015259619-A1 http://rdf.ncbi.nlm.nih.gov/pubchem/patent/US-2019106644-A1 |
priorityDate |
2010-08-16-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
type |
http://data.epo.org/linked-data/def/patent/Publication |