Triforial tip cavity airfoil

Details Triforial tip cavity airfoil Triforial tip cavity airfoil

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/20 (2006.01)

Patent

CA 2610090

A turbine blade (10) includes an airfoil (12) having first and second tip ribs (36,38) extending along the opposite pressure and suction sides (20,22) thereof. The tip ribs (36,38) are spaced apart between the leading and trailing edges (24,26) of the airfoil (12) to include a trifurcate tip baffle (42,44,46) defining a triforial tip cavity (48,50,52).

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