Cooled vane structure for a combustion turbine engine

Details Cooled vane structure for a combustion turbine engine Cooled vane structure for a combustion turbine engine

F - Mech Eng,Light,Heat,Weapons

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F01D 5/08 (2006.01) F01D 5/18 (2006.01) F01D 9/02 (2006.01) F02C 7/12 (2006.01)

Patent

CA 1125660

8 48,590 ABSTRACT OF THE DISCLOSURE A cooled vane for a combustion turbine is shown having a generally hollow airfoil for receiving cooling air and with the sidewalls of the airfoil tapered in thickness from thick-to-thin in the radial direction from the vane support into the generally free end.

353911

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