Polymer solution
AssigneeImperial Chemical Industries PLC
InventorsDesmond Wilfrid John Osmond, Norman Douglas Patrick Smith, Frederick Andrew Waite
Life of this patent
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Abstract
The dissemination of gas turbine engine aviation fuels under shock conditions, particularly by forming mist particles, and the accompanying fire hazard, are reduced by dissolving in the fuel a soluble polymer of molecular weight greater than 10.sup.6 in such concentration that there is molecular overlap of the dissolved polymer in the fuel, the dissolved polymer being one containing polar groups which form bonds with each other when the fuel is subjected to shock.
Claims5
A liquid hydrocarbon jet aviation fuel of flash point at least 90.degree. F suitable for use in gas turbine engined aircraft, and having a reduced tendency to particulate dissemination on being subjected to shock, the fuel containing dissolved therein 0.01 to 1% by weight of an addition polymer of ethylenically unsaturated monomer which is soluble in said hydrocarbon fuel of molecular weight greater than 10.sup.6 (viscosity average) or of intrinsic viscosity greater than 2.5 dls./gm. in a concentration such that there is molecular overlap of the polymer molecules in the liquid but the viscosity is less than 1 poise at zero shear rate at ambient temperature, the dissolved polymer containing polar groups which form inter-molecular associative bonds arising from electrostatic attraction between polar and/or dipolar charges in the polar groups, the bonds being hydrogen or electrovalent bonds.
Dependencies are inferred from the claim text.