METHOD OF OPERATING A GAS TURBINE AND GAS TURBINE
First Claim
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1. A method of operating a gas turbine, comprising at least the steps of:
- providing a gas turbine having a low pressure compression stage, a high pressure compression stage, a combustion chamber, and an expansion stage;
taking in an air inlet stream with the gas turbine from an air source which is at an ambient temperature;
compressing the air inlet stream in the low pressure compression stage to provide a low pressure compressed air stream;
passing the low pressure compressed air stream to the high pressure compression stage via an intercooling stage;
cooling the low pressure compressed air stream against ambient in an intercooling ambient cooler in the intercooling stage thereby providing an ambient-cooled compressed air stream;
chilling the ambient-cooled compressed air stream in the intercooling stage to an intercooling temperature that is lower than the ambient temperature;
compressing the chilled low pressure compressed air stream coming from the intercooling stage in the high pressure compression stage to provide a high pressure air stream;
passing the high pressure air stream to the combustion chamber and producing a combusted stream by allowing the high pressure air stream to oxidize a fuel stream;
expanding the combusted stream in the expansion stage; and
driving the low pressure compression stage and the high pressure compression stage with mechanical power from the expansion stage.
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Abstract
A gas turbine system comprises a gas turbine having a low pressure compression stage and a high pressure compression stage, a combustion chamber, and an expansion stage connected to the combustion chamber. The low pressure compression stage and the high pressure compression stage are connected with each other via an intercooling stage, wherein the low pressure compressed air stream from the low pressure compression stage is chilled to an intercooling temperature that is lower than the ambient temperature of the air source from which the air stream was supplied to the low pressure compression stage of the gas turbine.
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Citations
13 Claims
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1. A method of operating a gas turbine, comprising at least the steps of:
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providing a gas turbine having a low pressure compression stage, a high pressure compression stage, a combustion chamber, and an expansion stage; taking in an air inlet stream with the gas turbine from an air source which is at an ambient temperature; compressing the air inlet stream in the low pressure compression stage to provide a low pressure compressed air stream; passing the low pressure compressed air stream to the high pressure compression stage via an intercooling stage; cooling the low pressure compressed air stream against ambient in an intercooling ambient cooler in the intercooling stage thereby providing an ambient-cooled compressed air stream; chilling the ambient-cooled compressed air stream in the intercooling stage to an intercooling temperature that is lower than the ambient temperature; compressing the chilled low pressure compressed air stream coming from the intercooling stage in the high pressure compression stage to provide a high pressure air stream; passing the high pressure air stream to the combustion chamber and producing a combusted stream by allowing the high pressure air stream to oxidize a fuel stream; expanding the combusted stream in the expansion stage; and driving the low pressure compression stage and the high pressure compression stage with mechanical power from the expansion stage. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11)
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12. A gas turbine system comprising:
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a as turbine comprising a low pressure compressor, a high pressure compressor, a combustion chamber, and an expansion stage using an expansion turbine; a first air inlet into the gas turbine for taking in an air inlet stream from an air source at an ambient temperature; a low pressure compressed air stream outlet from the gas turbine whereby the low pressure compression stage connects the first air inlet and the low pressure compressed air stream outlet; an intercooling stage for producing an intercooled air stream from the low pressure compressed air stream, which intercooling stage is arranged to receive the low pressure compressed air stream passing through the low pressure compressed air stream outlet, the intercooling stage comprising an ambient cooler for cooling the low pressure compressed air stream against ambient thereby providing an ambient-cooled compressed air stream, followed by a heat exchanger arranged to chill the ambient-cooled compressed air stream to a temperature that is lower than the ambient temperature to produce the intercooled air stream; a second air inlet into the gas turbine for taking in the intercooled air stream from the intercooling stage, whereby the combustion chamber is connected to the second air inlet via the high pressure compressor and to the expansion turbine; a fuel stream inlet into the as turbine for allowing a fuel stream into the combustion chamber; and first and second mechanical drive shafts connecting the expansion stage with the low pressure compressor and with the high pressure compressor. - View Dependent Claims (13)
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Specification