Invention Grant
US07901180B2 Enhanced turbine airfoil cooling 有权
增强涡轮机翼型冷却

Enhanced turbine airfoil cooling
Abstract:
The ends of cooling air passages in turbine blades and/or vanes of a gas turbine engine are provided with turbulation promoters to enhance the cooling of such structures as inner and outer shrouds and the like to accommodate thermal loads thereon.
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