Systems and methods for fuel-based thermal management
US-10815906-B2 · Oct 27, 2020 · US
US11333073B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11333073-B2 |
| Application number | US-201916686551-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 18, 2019 |
| Priority date | Nov 20, 2018 |
| Publication date | May 17, 2022 |
| Grant date | May 17, 2022 |
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To prevent or reduce an oversensitive change in the degree of opening of a bleed valve regulating the flow volume of a cooling air used to heat a fuel. A gas turbine includes: a compressor compressing an air; a combustor burning a fuel mixed with the air compressed by the compressor; a turbine configured to be driven by a combustion gas generated by the combustor; a heat exchanger causing the fuel to be supplied to the combustor to be heated through a cooling air bled from the compressor to be supplied to the turbine; a bleed valve regulating the flow volume of the cooling air; a first sensor measuring a fuel state value; a second sensor measuring a cooling air state value; and a control computer controlling the degree of opening of the bleed valve. The control computer stores therein data on reference values and dead bands including the corresponding reference value set for each of the fuel state value and the cooling air state value, and, when a measured value of at least one of the fuel state value and the cooling air state value has changed so much away from the corresponding reference value as to fall outside the corresponding dead band, controls the bleed valve such that the changed measured value is brought close to the corresponding reference value.
Opening claim text (preview).
What is claimed is: 1. A gas turbine comprising: a compressor configured to compress an air; a combustor configured to burn a fuel mixed with the air compressed by the compressor to generate a combustion gas; a turbine configured to be driven by the combustion gas generated by the combustor; a heat exchanger configured to cause the fuel to be supplied to the combustor to be heated through a cooling air bled from the compressor to be supplied to the turbine; a bleed valve configured to regulate a flow volume of the cooling air; a first sensor configured to measure a state value related to the fuel; a second sensor configured to measure a state value related to the cooling air; and a control computer configured to control a degree of opening of the bleed valve, wherein the control computer stores therein reference values and dead bands that are set for each of measured state values of the first sensor and the second sensor, and, when at least one of a measured state value measured by the first sensor and a measured state value measured by the second sensor has changed so much away from the corresponding reference value as to fall outside of the corresponding dead band, controls the bleed valve such that the changed measured state value is brought within the corresponding dead band, the state value related to the cooling air includes a cooling air temperature, and the control computer is configured to increase the degree of opening of the bleed valve to increase the cooling air flow volume in the case where the cooling air temperature has decreased to fall outside of the corresponding dead band.
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