Damper seal system and method

摘要

A damper and seal system for a stage of a turbine that includes inner shrouds (12) disposed circumferentially of a hot gas path through the turbine stage and shroud body(s) (10) for supporting the inner shroud(s). A damper block (16) engages a backside surface (22) of the inner shroud (12) and a damping mechanism (30) is carried by the shroud body (10) and connected to the damper block (16) for applying a load to the damper block and inner shroud through the engagement of the block with the backside surface (22) of the inner shroud (12), thereby damping vibratory movement of the inner shroud. The seal system includes at least one primary, integral seal (18, 72, 76) and at least one secondary, non-integral seal (74) to limit axial and radial hot gas leakage through the stage.