Shroud support rail and method for assembling in turbine engine

Details Shroud support rail and method for assembling in turbine engine Shroud support rail and method for assembling in turbine engine

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/00 (2006.01) F01D 11/00 (2006.01) F01D 11/08 (2006.01) F01D 25/24 (2006.01)

Patent

CA 2072421

13dv-10447 ABSTRACT OF THE DISCLOSURE A shroud support for use in a gas turbine engine having a foot section which is equipped with two continuous rails which extend in a circumferential manner forming a gap between them. The rails contact a foot section of a shroud and prevent cooling air from leaking from a plenum formed by the shroud support to a position to the aft of the foot sections of the shroud and shroud support.

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