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Thermally stable jet prepared from highly paraffinic distillate fuel component and conventional distillate fuel component

  • US 20030116469A1
  • Filed: 10/19/2001
  • Published: 06/26/2003
  • Est. Priority Date: 10/19/2001
  • Status: Active Grant
First Claim
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1. A distillate fuel blend useful as a fuel or as a blending component of a fuel suitable for use in a turbine engine, said distillate fuel blend comprising:

  • (a) at least one highly paraffinic distillate fuel component having a paraffin content of not less than 70 percent by weight and a branching index within the range of from about 0.5 to about 3; and

    (b) at least one petroleum-derived distillate fuel component, wherein the distillate fuel blend has an ASTM D3241 breakpoint equal to or greater than 260°

    C.

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