Counter tip baffle airfoil

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

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Details

F01D 5/14 (2006.01) F01D 5/18 (2006.01) F01D 5/20 (2006.01)

Patent

CA 2596782

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 tip baffle (42). The baffle (42) extends chordally in counter profile with the first rib (36) to define a first pocket (44), and in counter profile with the second rib (38) to define a second pocket (46).

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