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Microcircuits for small engines

  • US 20070177976A1
  • Filed: 01/31/2006
  • Published: 08/02/2007
  • Est. Priority Date: 01/31/2006
  • Status: Active Grant
First Claim
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1. A method for design a turbine engine component comprising the steps of:

  • designing an airfoil portion having a root portion, a tip portion, a first wall forming a suction side wall, a second wall forming a pressure side wall, and a supply cavity; and

    said designing step comprising increasing wall thickness of said first and second walls from a point near said root portion to a point near said tip portion.

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