COOLING CHANNEL FOR AIRFOIL WITH TAPERED POCKET
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United States of America Patent
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Issued Date -
May 26, 2016
app pub date -
Nov 24, 2015
filing date -
Nov 26, 2014
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Abstract
The present invention includes systems and methods for providing cooling channels located within walls of a turbine airfoil. These cooling channels include micro-circuits that taper in various directions along the length and width of the airfoil. In addition, these cooling channels have a variety of shapes and areas to facilitate convective heat transfer between the surrounding air and the airfoil.
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