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

Data processing: vehicles – navigation – and relative location – Vehicle control – guidance – operation – or indication – With indicator or control of power plant

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701104, 701105, 60 3902, 60 3953, F02C 100

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active

057909725

ABSTRACT:
A multi-stage method and apparatus for cooling the inlet air of internal combustion engine and gas turbine prime movers associated 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 stage to stage to cool primary or secondary refrigerant from a first cooling stage as a precooling heat transfer coolant to exchange against and subcool subsequent stages of primary or secondary refrigerant 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: 4213738 (1980-07-01), Williams
patent: 4285917 (1981-08-01), Knight
patent: 4619240 (1986-10-01), Bedford et al.
patent: 4668162 (1987-05-01), Cederwall et al.
patent: 4905637 (1990-03-01), Ott
patent: 5278772 (1994-01-01), Knupp
patent: 5444971 (1995-08-01), Kolenberger

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