Thermally compliant turbine shroud mounting

Details Thermally compliant turbine shroud mounting Thermally compliant turbine shroud mounting

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/30 (2006.01) F01D 9/02 (2006.01)

Patent

CA 2554341

A shroud segment (112) is adapted to surround a row of rotating turbine blades in a gas turbine engine. The shroud segment (110) includes: an arcuate, axially extending first mounting flange (130) having a first radius of curvature, and an arcuate, axially extending first overhang (134) having a second radius of curvature. The first overhang (134) is disposed parallel to and radially inboard of the first mounting flange (130) so that a first groove (138) is defined between the first mounting flange (130) and the first overhang (134). The first and second radii of curvature are substantially different from each other. The shroud segment (112) may attached to a supporting structure or shroud hanger (114) to form a shroud assembly (110).

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