Countercooled turbine nozzle

Details Countercooled turbine nozzle Countercooled 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 2562584

A turbine nozzle (20) includes a mid vane (24) mounted between a pair of end vanes (26) in outer and inner bands (28,30). The mid vane (24) includes a first pattern of film cooling holes (56,58,60) configured to discharge more cooling air than each of the two end vanes having respective second patterns of film cooling holes (56,58).

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