Mounting apparatus for low-ductility turbine shroud

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

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Details

F01D 25/26 (2006.01) F01D 11/14 (2006.01) F02C 7/20 (2006.01)

Patent

CA 2729528

A turbine shroud apparatus is provided for a gas turbine engine having a central axis. The apparatus includes: (a) an annular support member (14); (b) a turbine shroud (12) disposed in the support member (14), the shroud (12) being a continuous ring comprising a low-ductility material and having opposed flowpath and back surfaces, and opposed forward and aft ends; and (c) a spring (32) mounted between the support member (14) and the shroud (12) and arranged to resiliently urge the shroud (12) to a concentric position within the support member (14).

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