Gas turbine system and method using temperature control of the exhaust gas entering the heat recovery cycle by mixing with ambient air
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United States of America Patent
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May 27, 1997
Issued Date -
N/A
app pub date -
Jun 20, 1994
filing date -
Jun 14, 1994
priority date (Note) -
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Abstract
A gas turbine system with a heat recovery cycle includes a gas turbine unit that produces hot exhaust gases which are applied to a heat recovery heat exchanger containing a working fluid responsive to applied hot gases for producing vaporized working fluid and cooled gases which are vented. A turbine connected to a generator and responsive to the vaporized working fluid generates power and produces expanded working fluid. A condenser condenses the expanded vaporized working fluid to condensate which is returned to the heat recovery heat exchanger. A control device (94) controls the temperature of the applied hot gases, based on a sensed temperature (89) and include mixer apparatus (87) for mixing ambient air with the hot exhaust gases and producing a mixture of hot exhaust gases and ambient air before the mixture is applied to the heat recovery heat exchanger.
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