Invention Grant
US08425183B2 Triforial tip cavity airfoil 失效
尖端腔翼型

Triforial tip cavity airfoil
Abstract:
A turbine blade includes an airfoil having first and second tip ribs extending along the opposite pressure and suction sides thereof. The tip ribs are spaced apart between the leading and trailing edges of the airfoil to include a trifurcate tip baffle defining a triforial tip cavity.
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