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    • 30. 发明申请
    • AVIATION GASOLINE COMPOSITION, ITS PREPARATION AND USE
    • 航空汽油组合物,其制备和使用
    • WO2015197855A1
    • 2015-12-30
    • PCT/EP2015/064602
    • 2015-06-26
    • BP OIL INTERNATIONAL LIMITEDHJELMCO ABHJELMBERG, Lars
    • HJELMBERG, Lars
    • C10L1/06
    • C10L1/04C10L1/023C10L1/06C10L1/18C10L1/1852C10L1/305C10L10/10C10L2200/0407C10L2200/0423C10L2270/023C10L2270/04
    • An aviation gasoline composition comprising an impure iso-octane fraction, at least one xylene and at least one C 4 or C 5 alkane, wherein the impure iso-octane fraction in said composition is a fraction comprising at least 90 mol% iso-octane and having a final boiling point of at least 180 °C and is present in the composition in an amount in the range of from 30 to 80 vol.% based on the composition, the composition is substantially free of any lead compounds, the composition has a motor octane number of at least 94 and the composition has a final boiling point of at most 170 °C. The composition of the present invention may be made by blending together an impure iso-octane fraction, xylene, at least one C 4 or C 5 alkane, optionally ethyl tertiary butyl ether, and optionally methylcyclopentadienyl manganese tricarbonyl and may be used in a spark ignition aviation engine, either alone or in combination with methanol or a methanol and water mixture.
    • 一种包含不纯的异辛烷级分,至少一种二甲苯和至少一种C 4或C 5烷烃的航空汽油组合物,其中所述组合物中不纯的异辛烷级分是包含至少90mol%异辛烷并具有 最终沸点为至少180℃,并且基于组合物以组合物的30至80体积%的量存在于组合物中,组合物基本上不含任何铅化合物,该组合物具有马达辛烷值 数量至少为94,组合物的最终沸点为至多170℃。 本发明的组合物可以通过将不纯的异辛烷馏分,二甲苯,至少一种C 4或C 5烷烃,任选的乙基叔丁基醚和任选的甲基环戊二烯基三羰基锰混合在一起来制备,并且可以用于火花点火航空发动机 单独或与甲醇或甲醇和水混合物组合。