Gas turbine vane body with instrumentation
US-2024287912-A1 · Aug 29, 2024 · US
US2020200035A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2020200035-A1 |
| Application number | US-201816229812-A |
| Country | US |
| Kind code | A1 |
| Filing date | Dec 21, 2018 |
| Priority date | Dec 21, 2018 |
| Publication date | Jun 25, 2020 |
| Grant date | — |
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A method for determining a performance characteristic for a target startup sequence of a gas turbine, wherein the gas turbine includes a compressor, a combustor, and, drivingly coupled to the compressor, a turbine. The method includes the steps of: measuring one or more operating parameters during a target operating period of the gas turbine, the target operating period being selected so that the target operating period includes the target startup sequence; creating a time series plot from data points derived from the one or more operating parameters measured during the target operating period; comparing the time series plot against a reference time series plot and, based on the comparison, determining a degree of similarity therebetween; and determining a value for the performance characteristic based on the degree of similarity.
Opening claim text (preview).
That which is claimed: 1 . A method for determining a performance characteristic for a target startup sequence of a gas turbine, wherein the gas turbine comprises a compressor, a combustor, and, drivingly coupled to the compressor, a turbine, the method comprising the steps of: measuring one or more operating parameters during a target operating period of the gas turbine, the target operating period being selected so that the target operating period includes the target startup sequence; creating a time series plot from data points derived from the one or more operating parameters measured during the target operating period; comparing the time series plot against a reference time series plot and, based on the comparison, determining a degree of similarity therebetween; and determining a value for the performance characteristic based on the degree of similarity. 2 . The method according to claim 1 , wherein the comparing the time series plot against the reference time series plot comprises a dynamic time warping (“DTW”) method; and wherein the one or more operating parameters include at least one of a rotor speed and a power output of the gas turbine. 3 . The method according to claim 2 , wherein the DTW method is defined as an algorithm for determining a degree of similarity between two given time series plots by non-linearly warping in a time dimension to find an optimal match between the two given time series plots. 4 . The method according to claim 2 , wherein the reference time series plot comprises data points derived from the one or more operating parameters measured during a previous startup sequence of the gas turbine, the previous startup sequence comprising a desirable startup outcome. 5 . The method according to claim 4 , wherein the one or more operating parameters include both the rotor speed and the power output of the gas turbine. 6 . The method according to claim 5 , wherein the data points used to create the time series plot each comprises a value of the rotor speed added to a corresponding value of the power output. 7 . The method according to claim 5 , wherein the value of the performance characteristic comprises a classification of the target startup sequence as being either a successful startup or an unsuccessful startup. 8 . The method according to claim 5 , wherein the gas turbine comprises a plurality of startup sequence types, the plurality of startup sequence types comprising at least a first startup sequence type and a second startup sequence type; and wherein the value of the performance characteristic comprises a classification of the target startup sequence as being either the first startup sequence type or second startup sequence type. 9 . The method according to claim 8 , wherein the reference time series plot comprises a first reference time series plot and a second reference time series plot; and wherein: the first reference time series plot corresponds to the first startup sequence type, and the first reference time series plot comprises data points derived from the one or more operating parameters measured during a previous startup sequence of the first startup sequence type; and the second reference time series plot corresponds to the second startup sequence type, and the second reference time series plot comprises data points derived from the one or more operating parameters measured during a previous startup sequence of the second startup sequence type. 10 . The method according to claim 9 , wherein the step of comparing the target time series plot against the reference time series plot comprises: comparing the target time series plot against the first reference time series plot and, based on the comparison, deriving a first degree of similarity; comparing the target time series plot against the second reference time series plot and, based on the comparison, deriving a second degree of similarity; further comprising the step of determining whether the target time series plot has a greater degree of similarity to the first reference time series plot or the second reference time series plot based on the first degree of similarity and the second degree of similarity; wherein the classification of the target startup sequence is equal to: the first startup sequence type if the target time series plot is determined to have the greater degree of similarity with the first reference time series plot; or the second startup sequence type if the target time series plot is determined to have the greater degree of similarity with the second reference time series plot. 11 . The method according to claim 4 , wherein the target startup sequence is defined between a beginning of the target startup sequence (“beginning-of-start”) and an end of the target startup sequence (“end-of-start”), wherein the end-of-start is defined as a startup completion time of the target startup sequence; and wherein the value for the performance characteristic comprises the startup completion time of the target startup sequence. 12 . The method according to claim 11 , wherein: the step of creating the time series plot from the data points derived from the one or more operating parameters measured during the target operating period comprises: creating candidate time series plots from the data points derived from the one or more operating parameters measured during the target operating period, wherein the candidate time series plots are created so that each comprises a unique startup completion time; the step of comparing the time series plot against the reference time series plot and, based on the comparison, determining the degree of similarity therebetween comprises: comparing each of the candidate time series plots against the reference time series plot and, based on the comparison, deriving the degree of similarity between each of the candidate time series plots and the reference time series plot. 13 . The method according to claim 12 , wherein: the step of determining the value for the performance characteristic based on the degree of similarity comprises: determining which of the candidate time series plots produced a highest value of the degree of similarity with the reference time series plot; determining the candidate startup completion time that corresponds to the candidate time series plot that produced the highest value of the degree of similarity; and deeming a time of the candidate startup completion time that corresponds to the candidate time series plot that produced the highest value of the degree of similarity as the startup completion time for the target startup sequence. 14 . The method according to claim 13 , further comprising the step of wherein the candidate end-of-starts of the plurality of the time series plots are varied over a range contained within the operating period. 15 . A system comprising: a gas turbine comprising a compressor, a combustor, and, drivingly coupled to the compressor, a turbine; a first sensor for measuring a turbine speed of the gas turbine; a second sensor for measuring a power output of the gas turbine; a controller operably connected to the gas turbine, the first sensor, and the second sensor, the controller comprising: a hardware processor; a machine-readable storage medium on which is stored instructions that cause the hardware processor to execute a process for determining a performance characteristic for a target startup sequence of the gas turbine; wherein the process comprises the following steps: measuring the turbine speed and the power output of the gas turbine during a tar
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