Invention Grant
US08727726B2 Turbine endwall cooling arrangement 有权
涡轮端壁冷却装置

Turbine endwall cooling arrangement
Abstract:
An airfoil is provided and includes an airfoil body having a pressure surface extendable between radial ends and a fluid path in an airfoil interior defined therein. The pressure surface is formed to further define a passage by which coolant is deliverable from the fluid path in the airfoil interior, in a perimetric direction from the pressure surface for the purpose of cooling a portion on the surface of the radial end.
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