Apparatus and method for cooling a turbine

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

Reexamination Certificate

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C415S116000

Reexamination Certificate

active

08061971

ABSTRACT:
A cooling system for a turbine includes a blower configured to generate a cooling gas flow to be passed through a rotor cavity of the turbine; piping configured to deliver the cooling gas flow to the turbine; and at least one valve configured to control the cooling gas flow. The piping is operatively connected to the rotor of the turbine. A method of cooling a turbine includes generating a cooling gas flow with a blower to be passed through a rotor cavity of the turbine; and delivering the cooling gas flow to the turbine.

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