System for cooling gas turbine blades

Power plants – Combustion products used as motive fluid – Combustion products generator

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Details

415114, 415115, 415116, 415117, F02C 712, F01D 906

Patent

active

059836237

ABSTRACT:
A cooling passage in a turbine blade of gas turbine can be prevented from being blocked by a scale when the turbine blade is cooled by steam. A system for cooling a blade of a gas turbine having a compressor, a combustor and a turbine section comprises a cooling steam supply tube and a steam discharge tube providing communication with a cooling passage in a guide blade of the turbine section, and a cyclone separator provided in the middle of the steam supply tube in proximity to the guide blade.

REFERENCES:
patent: 3066912 (1962-12-01), Scheper, Jr.
patent: 5120192 (1992-06-01), Ohtomo et al.
patent: 5558496 (1996-09-01), Woodmansee et al.
patent: 5634766 (1997-06-01), Cunha et al.
patent: 5813827 (1998-09-01), Nordlund et al.

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