Methods and apparatus for operating gas turbine engines

Power plants – Combustion products used as motive fluid – Process

Reexamination Certificate

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C060S728000

Reexamination Certificate

active

07007484

ABSTRACT:
A method for operating a gas turbine engine including a compressor, combustor, and turbine is provided that includes channeling compressed airflow from the compressor to a heat exchanger having a working fluid circulating within, channeling the working fluid from the heat exchanger to a chiller, extracting energy from the working fluid to power the chiller, and directing airflow entering the gas turbine engine through the inlet chiller such that the temperature of the airflow is reduced prior to the airflow entering the compressor.

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