http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-112812861-B
Outgoing Links
Predicate | Object |
---|---|
classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L1-1608 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L1-04 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/C10L10-00 |
classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C10L1-04 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C10L10-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/C10L1-16 |
filingDate | 2021-01-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
grantDate | 2022-11-18-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationDate | 2022-11-18-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber | CN-112812861-B |
titleOfInvention | Aviation Alternative Fuel Blending Method for Improving Ignition Performance of Heavy Oil Piston Engines |
abstract | The invention relates to a method for blending aviation alternative fuels for improving the ignition performance of heavy oil piston engines, which comprises adding components (1), (2), (3) or combinations thereof to aviation fuels, wherein component (1) is selected from One or more of methylcyclopentane, methylcyclohexane and ethylcyclohexane; component (2) is selected from one or more of propylcyclopentane and propylcyclohexane ; Component (3) is selected from one or more of C7-C10 paraffins. The invention also discloses an aviation fuel additive. The invention significantly improves the ignition performance of the aviation piston engine, not only balances atomization and volatility, cetane number, ignition delay, ignition energy, calorific value, and ignition boundary, but also expands the operating range of working conditions. |
priorityDate | 2021-01-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 34.