Cooling scheme for combustor vane interface

Details Cooling scheme for combustor vane interface Cooling scheme for combustor vane interface

F - Mech Eng,Light,Heat,Weapons

02

C

60/185

F02C 7/06 (2006.01) F01D 9/02 (2006.01) F23R 3/06 (2006.01)

Patent

CA 1245869

Abstract Cooling Scheme for Combustor Vane Interface The turbine vanes of a gas turbine engine immedi- ately downstream of the combustor is maintained at a cool temperature by judiciously directing cooling air at the stagnation point ahead of the vane's leading edge at the juncture of the vane's airfoil section and platform.

486033

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