Renewable engine fuel and method of producing same
AssigneeSwift Fuels, LLC
InventorsJohn J. Rusek, Mary-Louise R. Rusek, Jonathon D. Ziulkowski, Justin D. Zink
Life of this patent
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Abstract
The present invention provides high-octane fuel, and a method of producing same. These fuels may be formulated to have a wide range of octane values and energy, and may effectively be used to replace 100 LL aviation fuel (known as AvGas), as well as high-octane, rocket, diesel, turbine engine fuels, as well as two-cycle, spark-ignited engine fuels.
Claims8
A 100 octane aviation fuel comprising:
- (a) 70-85 wt % of sym-trimethyl benzene (mesitylene);
- and (b) 15-30 wt % of isopentane, wherein the fuel has a motor octane number of 99.5 or greater, and a Reid vapor pressure of from 5.5 to 7.1 psi.
A 100 octane aviation fuel consisting essentially of:
- (a) 70-85 wt % of sym-trimethyl benzene (mesitylene);
- and (b) 15-30 wt % of isopentane, wherein the fuel has a motor octane number of 99.5 or greater, and a Reid vapor pressure of from 5.5 to 7.1 psi.
A 100 octane aviation fuel consisting of:
- (a) 70-85 wt % of sym-trimethyl benzene (mesitylene);
- and (b) 15-30 wt % of isopentane, wherein the fuel has a motor octane number of 99.5 or greater, and a Reid vapor pressure of from 5.5 to 7.1 psi.
A high octane aviation fuel comprising:
- (a) 60-85 wt % of sym-trimethyl benzene (mesitylene), and (b) 15-40 wt % of isopentane, wherein the fuel has a motor octane number of 99.5 or greater, and a Reid vapor pressure of from 5.5 to 7.1 psi.
A high octane fuel comprising:
- (a) 70-85 wt % of sym-trimethyl benzene (mesitylene);
- and (b) 15-30 wt % of isopentane, wherein the fuel is an aviation fuel having a motor octane number of 99.5 or greater, and a Reid vapor pressure of from 5.5 to 7.1 psi.
A 100 octane aviation fuel comprising:
- (a) 70-85 wt % of sym-trimethyl benzene (mesitylene);
- and (b) 15-30 wt % of isopentane, wherein the fuel has a motor octane number of greater than 99.5, and a Reid vapor pressure of from 5.5 to 7.1 psi.
Dependencies are inferred from the claim text.