Stationary blade shroud of a gas turbine

Details Stationary blade shroud of a gas turbine Stationary blade shroud of a gas turbine

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 25/24 (2006.01) F01D 9/02 (2006.01) F01D 11/00 (2006.01)

Patent

CA 2366758

A base plate and honeycomb member disposed at the inner circumference side of an inside shroud are fixed to the inside shroud, at a phase deviation in the peripheral direction, with respect to the inside shroud, so as to plug the missing range of seal member, out of gaps between adjacent inside shrouds, and therefore leak of purge air from the missing range of seal member is prevented without adding new constituent members.

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