F - Mech Eng,Light,Heat,Weapons – 01 – D
Patent
F - Mech Eng,Light,Heat,Weapons
01
D
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).
Keith Brian David
Klasing Kevin Samuel
Lee Ching-Pang
Vitt Paul Hadley
Company General Electric
Craig Wilson And Company
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