Abstract Gas turbine unit comprising a high pressure turbine (10) driving a high pressure compressor (11), and a low pressure turbine (13) driving a low pressure compressor (14) and a generator (12), a combustion chamber supplying gas to the compressors, and a recuperator (18) for heat exchange between exhaust gas and compressor air, the low pressure turbine having an adjustable geometry and an adjustable connection (20) being provided bypassing the recuperator, and a method in operating the gas turbine unit wherein the electric power is adjusted to a desired value by changing the geometry of the low pressure turbine and the heat power is adjusted by adjusting the bypass flow to a desired value.
Method in operating a gas turbine unit for combined production of electricity and heat comprising a combustion chamber (16), a high pressure turbine (10) driven by gas from the combustion chamber, a low pressure turbine (13) driven by the exhaust gas from the high pressure turbine, a low pressure compressor (14) driven by the low pressure turbine, a high pressure compressor (11) connected in series with the low pressure compressor and driven by the high pressure turbine for the supply of pressurized air to the combustion chamber, a generator (12) driven by the high pressure turbine for producing electricity, a recuperator (18) for heat exchange between exhaust gas and pressurized air from the compressors, an intermediate cooler (22) for producing hot water between the low pressure and the high pressure compressors, and an exhaust gas heat exchanger (19) for producing hot water, characterized in that the electric power is adjusted to the desired value by changing the geometry of the low pressure turbine in order to change the rotational speed thereof at constant temperature in the combustion chamber, and that the heat power is adjusted to the desired value by controlling a flow bypassing the recuperator.
Claim 2
Dependent Claim
196 words
Method in operating a gas turbine unit for combined production of electricity and heat comprising a combustion chamber (16), a high pressure turbine (10) driven by gas from the combustion chamber, a low pressure turbine (13) driven by the exhaust gas from the high pressure turbine, a low pressure compressor (14) driven by the low pressure turbine, a high pressure compressor (11) connected in series with the low pressure compressor and driven by the high pressure turbine for the supply of pressurized air to the combustion chamber, a generator (12) driven by the high pressure turbine for producing electricity, a recuperator (18) for heat exchange between exhaust gas and pressurized air from the compressors, an intermediate cooler (22) for producing hot water between the low pressure and the high pressure compressors, and an exhaust gas heat exchanger (19) for producing hot water, characterized in that the electric power is adjusted to the desired value by changing the geometry of the low pressure turbine in order to change the rotational speed thereof at constant temperature in the combustion chamber, and that the heat power is adjusted to the desired value by controlling a flow bypassing the recuperator.
Claim 3
Dependent Claim
16 words
Method as in claim 1 wherein water is injected into the compressor air upstream the recuperator.
Claim 4
Dependent Claim
11 words
Method as in claim 2 wherein the injection water is preheated.
Claim 5
Dependent Claim
166 words
Gas turbine unit for working the method of any of claims 1 to 3, comprising a combustion chamber (16), a high pressure turbine (10) driven by gas from the combustion chamber, a low pressure turbine (13) driven by the exhaust gas from the high pressure turbine, a low pressure compressor (14) driven by the low pressure turbine, a high pressure compressor (11) connected in series with the low pressure compressor and driven by the high pressure turbine for the supply of pressurized air to the combustion chamber, a generator (12) driven by the high pressure turbine for producing electricity, a recuperator (18) for heat exchange between exhaust gas and pressurized air from the compressors, an intermediate cooler (22) for producing hot water between the low pressure and the high pressure compressors and an exhaust gas heat exchanger (19) for producing hot water, characterized in that the low pressure turbine (13) has an adjustable geometry and that an adjustable connection (20) is provided bypassing the recuperator (18).