Reciprocal cooled turbine nozzle

Details Reciprocal cooled turbine nozzle Reciprocal cooled turbine nozzle

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 9/02 (2006.01) F01D 5/18 (2006.01) F01D 25/12 (2006.01)

Patent

CA 2633787

A turbine nozzle (20) includes first and second vanes (36,38) joined to outer and inner bands (40,42). The vanes (36,38) include outboard sides (50,52) defining outboard flow passages (60) containing axial splitlines (44), and opposite inboard sides (52,50) defining an inboard flow passage (58) without axial splitline. The two vanes (36,38) include different cooling circuits (62,64) for differently cooling the inboard and outboard vane sides (50,52).

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