Aviation fuel containing dissolved polymer and having reduced te

Fuel and related compositions – Liquid fuels – Aluminum or heavy metal – other than lead – containing

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44 70, 44 71, 44 77, 44 80, C10L 116

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active

039960234

ABSTRACT:
A polymer is dissolved in a liquid hydrocarbon fuel which has a flash point of at least 90.degree. F and is of a type suitable for gas turbine aircraft engines in order to reduce the tendency of the fuel to particulate dissemination when the fuel is subjected to shock. The polymer has a viscosity average molecular weight greater than 10.sup.6 or an intrinsic viscosity greater than 2.5 dls./gm. and the amount of polymer is sufficient that there is molecular overlap of polymer molecules in the liquid.

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patent: 3473901 (1969-08-01), DEBennevill et al.
Kirk-Othmer, Encyclopedia of Chemical Technology, 2nd Ed., vol. 15, 1968, p. 87.
Tanford, Physical Chemistry of Macromolecules, Wiley 1961, pp. 165-168, 174-178, 198-200, 402-406.
Miller, The Structure of Polymers, Reinhold 1966, pp. 190-193, 213, 214.
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Cohen et al., Journal of Polymer Science, vol. 49, 1961, pp. 377-383.
Flory, Principles of Polymer Chemistry, Cornell U. 1953, pp. 610-611.
Def. Pub. T-858,018, Jacobson, N., Multifunctional Polymeric Additive for Mineral Oils, Jan. 21, 1969, Application Ser. No. 664,925

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