Gas turbine cooling

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

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Details

415115, 416 96R, 416241B, F02C 300

Patent

active

052791114

ABSTRACT:
A gas turbine having internally cooled thermal barrier coated turbine blades is disclosed. The turbine blades are made from an alloy substrate exhibiting a low coefficient of thermal expansion, an intermediate bond coating and an exterior ceramic coating. Cooling fluid is supplied from the shaft of the compressor where it flows into and out of the turbine blade. Thermal barrier coated turbine blades result in more efficient gas turbine designs.

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