Method of using external fluid for cooling high temperature components of gas turbine
A gas turbine and turbine technology, applied in the field of turbines, can solve problems such as reduced efficiency, reduced power potential, and reduced flame temperature
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[0039] The present invention provides cooling of stationary and / or rotating hot gas path components of the gas turbine using fluid external to the gas turbine in a closed loop cooling configuration. The external fluid can be nitrogen, carbon dioxide, steam or air. Preferably, the external fluid is nitrogen, which is obtained from an air separation unit (ASU) column and then introduced into the closed loop to cool the hot gas path components of the gas turbine.
[0040] After cooling the turbine components, the heat removed with the external fluid flow is dumped into the compressor discharge casing (CDC), or into one of the stages of the multi-stage turbine. Preferably, the heated external fluid is poured into the combustor / CDC where heat can be used at the optimum point of the turbo Brayton cycle. Alternatively, heated external fluid may be poured into an appropriate downstream turbine stage when the pressure of the heated fluid is insufficient for the fluid to make it to the...
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