High octane unleaded aviation gasoline
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United States of America Patent
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Sep 1, 2015
Grant Date -
Apr 30, 2015
app pub date -
Jul 25, 2014
filing date -
Oct 31, 2013
priority date (Note) -
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Abstract
High octane unleaded aviation fuel compositions having a CHN content of at least 97.2 wt %, less than 2.8 wt % of oxygen content, a T10 of at most 75° C., T40 of at least 75° C., a T50 of at most 105° C., a T90 of at most 135° C., a final boiling point of less than 210° C., an adjusted heat of combustion of at least 43.5 MJ/kg, a vapor pressure in the range of 38 to 49 kPa is provided.
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