Cascade 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 2596764

A turbine blade (10) includes an airfoil tip (30) with first and second ribs (36,38) extending along the opposite pressure and suction sides (20,22). The ribs (36,38) extend outwardly from a tip floor (40) and are joined together at opposite leading and trailing edges (24,26). A cascade tip baffle (42) transversely bridges the two ribs (36,38) above the tip floor (40) forward of the maximum width of the tip (30) to partition the tip (30) chordally into corresponding tip pockets (44) on opposite sides of the baffle (42).

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