Turbine shroud segment seal

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

Patent

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Details

F01D 11/10 (2006.01) F01D 11/12 (2006.01)

Patent

CA 2523192

A ring seal for sealing an annular gap defined between opposed surfaces of concentric inner and outer annular engine parts in a gas turbine engine. The ring seal being wholly disposed within the annular gap and having a wave pattern with alternating peaks. The ring seal radially inwardly loads the inner engine part and provides a fluid seal between the inner and outer engine parts.

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