Combustion gas turbine engine integrated modular temperature cooling and heating process
AssigneeHrt Power, L.L.C.
InventorsLloyd B. Tisdale, Robert L. Hauck, Paul T. Tisdale, Jr.
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AssigneeHrt Power, L.L.C.
InventorsLloyd B. Tisdale, Robert L. Hauck, Paul T. Tisdale, Jr.
Estimating the term…
The present invention comprises a modular unit in which all of the components necessary for conditioning the intake air for a combustion gas turbine are contained. The compressors, evaporators condensers and related pumps and control equipment are contained within a weather proof enclosure having sound insulation installed in the walls. The intake air conditioning system includes three loops, a compressed refrigerant loop, a chilled water loop and a condenser cooling water loop with an optional heating loop. The modular unit provides a three loop cooling system for easy connection to both a combustion gas turbine air inlet and to a cooling water tower. The loops comprise a refrigerant loop, a cooling water loop and a chilled water loop and in one embodiment a heating loop to heat the air going to the turbine.
A process for conditioning the inlet air to a combustion gas turbine comprising the steps of:
Dependencies are inferred from the claim text.