Patent ID: 7683224
Filing Date: 2010-03-23
Classification: C10L

Abstract:
1. A fuel composition for use in jets, gas turbines, rockets, or diesel engines comprising: (a) from about 5% to about 99% by weight of the fuel composition of formula wherein the A moiety is selected from benzene, cyclohexane, and mixtures thereof, such that the A moiety is non-terminally attached to the L moiety and further such that the A moiety is directly connected to the L moiety; R′ is selected from hydrogen and C 1 to C 3 alkyl; R″ is selected from hydrogen and C 1 to C 3 alkyl; wherein both of R′ and R″ are nonterminally attached to the L moiety; the L moiety is a linear acyclic aliphatic hydrocarbyl such that the sum of carbons in the L moiety, R′, and R″ is from 5 to 25 carbons; (b) at least about 0.01% of fuel additives; and (c) from 0% to about 90% of conventional jet, gas turbine, rocket or diesel blendstocks.