Method and apparatus for cooling the inlet air of gas turbine and internal combustion engine prime movers
OwnerCharles R. Kohlenbergerinventor
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OwnerCharles R. Kohlenbergerinventor
Estimating the term…
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.
A method for optimizing the power output and performance of combustion prime movers, gas turbines and internal combustion engines having air inlets taking in inlet air for admixture with fuel for combustion, and associated with a prime mover load application to increase power output and reduce fuel consumption, comprising:
An apparatus for optimizing the energy power output and performance of combustion prime movers having air inlets taking in inlet air at the minimum acceptable inlet air temperature to prevent damage to the prime mover and its auxiliary components for admixing with fuel for combustion, and associated with a prime mover load application, comprising:
Dependencies are inferred from the claim text.