Turbine shroud assembly and method for assembling a gas...

Rotary kinetic fluid motors or pumps – Casing and spaced housing with space vented to working fluid

Reexamination Certificate

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C415S115000, C415S182100

Reexamination Certificate

active

11250660

ABSTRACT:
A method for assembling a gas turbine engine includes coupling a rotor assembly including a plurality of rotor blades about a rotatable main shaft of the gas turbine engine. The main shaft is aligned in an axial direction of the gas turbine engine. A shroud assembly is coupled to the gas turbine engine. The shroud assembly includes a plurality of shroud segments circumferentially coupled about the rotor assembly such that a shroud spacing gap is formed in the axial direction between adjacent shroud segments. A cooling fluid source is coupled to each shroud segment such that cooling fluid is channeled through each shroud segment into a corresponding shroud spacing gap to facilitate positive purge flow through the shroud spacing gap.

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