Thermally compliant turbine shroud assembly

Details Thermally compliant turbine shroud assembly Thermally compliant turbine shroud assembly

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/32 (2006.01) F01D 9/02 (2006.01)

Patent

CA 2554121

A shroud assembly (33) is provided for a gas turbine engine having a temperature at a hot operating condition substantially greater than at a cold assembly condition thereof. The shroud assembly (33) includes at least one arcuate shroud segment (32) adapted to surround a row of rotating turbine blades. The shroud segment (32) has an arcuate, axially extending mounting flange (52, 54). A shroud hanger (34) includes an arcuate, axially-extending hook (42, 44). A dimension of one of the shroud segments (32) and the shroud hanger (34) are selected to produce a preselected dimensional relationship therebetween at the hot operating condition.

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