Abradable CMC stacked laminate ring segment for a gas turbine

Rotary kinetic fluid motors or pumps – Bearing – seal – or liner between runner portion and static part

Reexamination Certificate

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Details

C415S173100, C415S173400, C415S173600, C415S174400, C415S200000

Reexamination Certificate

active

07819625

ABSTRACT:
A pattern of depressions (36) in a sealing surface (34) on a CMC wall (32) of gas turbine ring segment (30) allows minimum clearance against turbine blades tips, and thus maximizes working gas sealing. An array of depressions (36) on the surface (34) increases abradability of the surface (34) by blade tip contact during zero clearance conditions and reduces blade tip damage. The depressions (36) are unconnected, preventing bypass of the working gas around the blade tips. A desired abradable surface geometry may be formed in a stacked laminate wall construction (40-43, 52) by staggered laminate edge profiles (50, 52) or by machining of depressions (36, 54) after construction.

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