http://rdf.ncbi.nlm.nih.gov/pubchem/patent/ES-2612571-T3
Outgoing Links
Predicate | Object |
---|---|
assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_70ec63d39d6704bacc5c7068c93ded43 |
classificationCPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L1-1616 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L1-1608 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L1-223 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L2270-04 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L2300-40 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L2200-0259 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L2270-023 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L2200-0423 |
classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10G59-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L10-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L1-19 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L1-185 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L1-04 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L1-10 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L1-16 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L1-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L1-223 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L1-1608 |
classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C10L1-10 |
filingDate | 2014-07-25-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
grantDate | 2017-05-17-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_ec534bba309f8e0547f255e947a7a5e5 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_117eafdd20545e47dc77e1e16c43572a http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_17c52a14651f6d5daf013482a6b1b24a http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_2271133f9efb4ec7d40d7e31b74cc2c2 |
publicationDate | 2017-05-17-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber | ES-2612571-T3 |
titleOfInvention | High octane unleaded aviation gasoline |
abstract | An unleaded aviation fuel composition having a MON of at least 99.6, sulfur content of less than 0.05% by weight, CHN content of at least 97.2% by weight, less than 2.8 % by weight of oxygen content, a T10 of a maximum of 75 ° C, a T40 of at least 75 ° C, a T50 of a maximum of 105 ° C, a T90 of a maximum of 135 ° C, a final boiling point of less than 190 ° C, an adjusted heat of combustion of at least 43.5 MJ / kg, a vapor pressure in the range of 38 to 49 kPa, comprising: from 20% by volume to 35 volume% toluene having a MON of at least 107; from 2% by volume to 10% by volume of aniline; from above 30% by volume to 55% by volume of at least one alkylate or alkylate mixture having an initial boiling point range of 32 ° C to 60 ° C and a final boiling point range of 105 ° C to 140 ° C, which has a T40 of less than 99 ° C, a T50 of less than 100 ° C, a T90 of less than 110 ° C, the alkylate or alkylate mixture comprising isoparaffins of 4 to 9 carbon atoms, 3-20% by volume of C5 isoparaffins, 3-15% by volume of C7 isoparaffins and 60-90% by volume of C8 isoparaffins, based on the alkylate or alkylate mixture, and less than 1% by volume of C10 +, based on the alkylate or mixture of alkylate; from 7% by volume to 14% by volume of a branched alkyl acetate having a branched chain alkyl group having 4 to 8 carbon atoms; and from 8% by volume to 26% by volume of isopentane in an amount sufficient to achieve a vapor pressure in the range of 38 to 49 kPa; where the fuel composition contains less than 1% by volume of C8 aromatics; and where the adjusted heat of combustion is calculated as follows: HOC *> = (HOCv / density) + (% increase in span /% increase in load + 1) where HOC * is the adjusted heat of combustion (MJ / kg) , HOCv is the volumetric energy density (MJ / l) obtained from the measurement of the actual heat of combustion, the density is the density of the fuel (g / l),% of the interval increase is the percentage increase in the range of aircraft compared to 100 LL (HOCLL) calculated using HOCv and HOCLL for a fixed fuel volume and% load increase is the corresponding percentage increase in load capacity due to fuel mass. |
priorityDate | 2013-10-31-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 65.