Gas turbine stationary shroud seals

Claim 1

A seal structure for controlling leakage of hot motive fluid between adjacent stationary shroud segments in a gas turbine comprising: A turbine casing having at least one blade ring disposed within said casing, said blade ring defining radially inwardly projecting members, said members having axially opening opposed grooves, an annular array of stationary blades supported on their radially outer ends by a plurality of arcuately formed outer shroud segments and supported on their inner ends by a plurality of arcuately formed inner shroud segments; said outer shroud segments having axially opposed ends generally snugly received within said opposed grooves for supporting said blades and disposed therein so as to have a circumferential gap between adjacent shroud segments providing spatially separated facing end portions; each of said portions defining a generally circumferentially projecting shoulder extending generally through the axial extent of said outer shroud segments; a seal member disposed across said gap throughout the axial extent thereof to prevent leakage of fluid therepast and being in generally sealing engagement with said adjacent facing shoulder portions with the axial ends of said seal member received snugly within said opposed grooves of said blade ring for restraint against both radial and axial displacement.