Vane assembly for a gas turbine

Details Vane assembly for a gas turbine Vane assembly for a gas turbine

F - Mech Eng,Light,Heat,Weapons

01

D

170/66

F01D 9/00 (2006.01) F01D 9/04 (2006.01)

Patent

CA 1300030

ABSTRACT OF THE DISCLOSURE A nozzle vane assembly for a gas turbine has a number of vanes connected to a shroud. A second, concentric shroud is arranged separately and urged axially against the unrestrained ends of the vanes through a clamping device. This serves to alleviate thermal stresses and thermal fatigue in the vane assembly.

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