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F - Mech Eng,Light,Heat,Weapons

01

D

170/60

F01D 25/28 (2006.01) F01D 11/08 (2006.01) F01D 25/24 (2006.01) F16J 15/32 (2006.01) F16M 1/04 (2006.01)

Patent

CA 1117429

ABSTRACT OF DISCLOSURE A turbine suitable for a gas turbine engine is provided with a stage of rotary aerofoil blades which is surrounded by a shroud ring made of silicon nitride. In order to minimise load transfer between the shroud ring and the turbine casing the shroud ring is radially supported by and radially spaced apart from the turbine casing by an annular brush seal.

352259

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