Turbine engine shroud segment, hanger and assembly

Details Turbine engine shroud segment, hanger and assembly Turbine engine shroud segment, hanger and assembly

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/22 (2006.01) F01D 11/18 (2006.01) F01D 25/26 (2006.01) F04D 29/54 (2006.01)

Patent

CA 2502805

A turbine engine shroud segment (10) comprises a body (12) including an outer surface (16) from and along which a segment projection (26) extends away (36) from and in an axial direction (34). The segment projection (26) includes circumferentially spaced apart segment support surfaces (28,30). A shroud hanger (48) comprises a body (50) including an inner surface (52) from and along which a hanger projection (64) extends in an axial direction (34). The hanger projection (64) includes circumferentially spaced hanger bearing surfaces (66,68). In a circumferential turbine engine shroud assembly (10,48) of shroud segments (10) and hangers (48), a shroud hanger (48) is assembled between a pair of adjacent shroud segments (10) separated by an axial interface (74). The hanger projection (64) is in juxtaposition with the interface (74), and respective segment support surfaces (28,30) and hanger bearing surfaces (66,68) are in registry.

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