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Annular one-piece corrugated liner for combustor of a gas turbine engine

  • US 20030192320A1
  • Filed: 04/10/2002
  • Published: 10/16/2003
  • Est. Priority Date: 04/10/2002
  • Status: Active Grant
First Claim
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1. An annular one-piece liner for a combustor of a gas turbine engine, comprising:

  • (a) a first end adjacent to an upstream end of said combustor;

    (b) a second end adjacent to a downstream end of said combustor; and

    , (c) a plurality of corrugations between said first and second ends, each corrugation having an amplitude and a wavelength between an adjacent corrugation;

    wherein the amplitude of said corrugations is variable from said first end to said second end.

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