Turbine nozzle for a gas turbine engine

Details Turbine nozzle for a gas turbine engine Turbine nozzle for a gas turbine engine

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 9/02 (2006.01)

Patent

CA 2680410

A turbine nozzle includes: a hollow, airfoil-shaped turbine vane (14); and an arcuate first band (16, 18) disposed at a first end of the turbine vane (14), the first band (16, 18) having a flowpath face adjacent the turbine vane (14), and an opposed back face (56). The back face (56) includes at least one open pocket (58), the at least one pocket (58) defined in part by a bottom wall (66) recessed from the back face (56), opposed ends of the bottom wall (66) merging with the back face (56). The bottom wall (66) is substantially free of interior corners.

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