Method and apparatus for cooling the inlet air of gas turbine an

Power plants – Combustion products used as motive fluid

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60728, F02C 100

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active

054449715

ABSTRACT:
A multi-stage method and apparatus for cooling the inlet air of internal combustion engine and gas turbine prime movers with various load applications comprising: generating and providing a multi-stage refrigerated cooling system associated with the air inlet of internal combustion engine and gas turbine prime movers which provides thermodynamic efficiencies in accordance with a divided psychrometric inlet air cooling path enthalpy curve; cascading the cooled refrigerant from a first cooling stage as the liquid feed into a subsequent lower temperature cooling stage for cooling to the desired temperature; energizing power means to drive the prime mover and refrigerant cooling system; and adjusting the power means based on current energy costs to optimize net revenues to produce electricity or useful work from the prime mover application.

REFERENCES:
patent: 2513601 (1950-07-01), Traupel
patent: 3733845 (1973-05-01), Lieberman
patent: 3735601 (1973-05-01), Stannard, Jr.
patent: 3788066 (1974-01-01), Nebgen
patent: 3796045 (1974-03-01), Foster-Pegg
patent: 3852974 (1974-12-01), Brown
patent: 4676072 (1987-06-01), Higuchi

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