# US 10,767,569 B2 · Method for controlling the operation of a gas turbine with an averaged turbine outlet temperature > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 10,767,569 B2 - Document ID: US10767569B2 - Status: Granted - Kind: B2 - Application number: 15/351,102 - Filed: 2016-11-14 - Published: 2017-05-18 - Granted: 2020-09-08 - Earliest claimed: 2015-11-13 - Assignees: Ansaldo Energia Switzerland AG - Applicants: Ansaldo Energia Switzerland AG - Inventors: Martin Gassner; Andreas Jan Schesny; Sebastian Lipari; Stefano Bernero; Manuel Ramirez-Espana-Mejia; Mengbin Zhang - Web page: https://patentgrep.com/patent/US10767569B2 ## CPC - F02C 9/28: Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed (F02C9/30 - F02C9/38, F02C9/44 take precedence) - F01D 17/085: {to temperature} - F01D 21/12: responsive to temperature - F02C 3/04: having a turbine driving a compressor (power transmission arrangements F02C7/36; control of working fluid flow F02C9/16) - F05D 2220/32: in gas turbines - F05D 2250/52: Outlet - F05D 2270/303: Temperature - F05D 2270/80: Devices generating input signals, e.g. transducers, sensors, cameras or strain gauges - F05D 2270/803: Sampling thereof - F02C: GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS (construction of turbines F01D; jet-propulsion plants F02K; construction of compressors or fans F04; generating combustion products of high pressure or high velocity F23R; using gas turbines in compression refrigeration plants F25B11/00) - F01D: NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES (machines or engines for liquids F03; non-positive displacement pumps F04D) - F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS ## Abstract A method is disclosed for operating a gas turbine having a compressor, a combustor, a turbine downstream of the combustor, and a total number of turbine outlet temperature measurements. The method includes locally measuring the turbine outlet temperature of the turbine with the turbine outlet temperature measurements of the respective turbine, and averaging measured temperatures of the selected turbine outlet temperature measurements to obtain an average turbine outlet temperature. The gas turbine operation is controlled depending on the determined average turbine outlet temperature. ## Claims ### Claim 1 A method for operating a gas turbine having a compressor, a combustor, a turbine downstream of the combustor, and sensors distributed at a total number of measurement points about the turbine, the method comprising: determining with the sensors a turbine outlet temperature measurement at each of the total number of measurement points to yield a total number of turbine outlet temperature measurements; obtaining a reference average turbine outlet temperature based on all the turbine outlet temperature measurements determined at each of the total number of measurement points; selecting a number of the turbine outlet temperature measurements, which is smaller than the total number of the turbine outlet temperature measurements, as selected turbine outlet temperature measurements, wherein the selecting is performed by determining ones of the turbine outlet temperature measurements which satisfy a selection criteria; averaging the selected turbine outlet temperature measurements to obtain a value of an average turbine outlet temperature; controlling an operation of the gas turbine in dependence of a deviation calculated between the reference average turbine outlet temperature obtained and the value of the average turbine outlet temperature; and wherein the selection criteria includes one of: having a specified data quality, having a measurement value within a specified number of highest measurement values considering all the turbine outlet temperature measurements determined at each of the total number of measurement points, and having a measurement value within a specified temperature deviation from a previously obtained value of the average turbine outlet temperature. ### Claim 2 (depends on 1) The method as claimed in claim 1, wherein burners of the combustor upstream of the turbine are in operation when the method is performed. ### Claim 3 (depends on 1) The method as claimed in claim 1, wherein the selection criteria is the having the specified data quality. ### Claim 4 (depends on 1) The method as claimed in claim 1, wherein the selection criteria is the having the measurement value within the specified number of highest measurement values considering all the turbine outlet temperature measurements determined at each of the total number of measurement points. ### Claim 5 (depends on 1) The method as claimed in claim 1, wherein the selection criteria is the having the measurement value within the specified temperature deviation from the previously obtained value of the average turbine outlet temperature. ### Claim 6 (depends on 1) The method as claimed in claim 1, wherein a controller of the gas turbine has a clock defining controller cycles, wherein the selection criteria is the having the measurement value within the specified temperature deviation from the previously obtained value of the average turbine outlet temperature, and wherein the previously obtained value of the average turbine outlet temperature is determined at a preceding one of the controller cycles. ### Claim 7 (depends on 1) The method as claimed in claim 1, wherein the averaging is carried out over a number of cycles of a controller of the gas turbine engine, the averaging comprising: assigning a number of the selected turbine outlet temperature measurements to a summing list; and dividing a sum of the selected turbine outlet temperature measurements assigned to the summing list by the number of the selected turbine outlet temperature measurements assigned to the summing list to obtain the value of the average turbine outlet temperature. ### Claim 8 (depends on 1) The method as claimed in claim 1, wherein the averaging is carried out over a number of cycles of a controller of the gas turbine engine, the averaging comprising: assigning the selected turbine outlet temperature measurements to a summing list; determining ones of the selected turbine outlet temperature measurements assigned to the summing list that are within a specified number of highest measurement values on the summing list; determining a sum of the ones of the selected turbine outlet temperature measurements assigned to the summing list that are within the specified number of the highest measurement values on the summing list; and dividing the sum by the specified number to obtain the value of the average turbine outlet temperature. ### Claim 9 (depends on 1) The method as claimed in claim 1, wherein the average turbine outlet temperature is controlled to a set point temperature or the average turbine outlet temperature is used to control a temperature of the combustor to a set point temperature with a closed loop control using fuel flow to the combustor as a correcting variable. ### Claim 10 (depends on 1) The method as claimed in claim 1, wherein the gas turbine operates above a relative load limit. ### Claim 11 (depends on 1) The method as claimed in claim 1, wherein controlling the operation of the gas turbine comprising: triggering a protective action upon the deviation calculated between the reference average turbine outlet temperature obtained and the value of the average turbine outlet temperature exceeding an allowable deviation. ### Claim 12 (depends on 11) The method as claimed in claim 11, wherein the protective action is one of a deloading, a load shedding, and a trip of the gas turbine. ### Claim 13 (depends on 1) The method as claimed in claim 1, wherein the gas turbine is configured as a sequential combustion gas turbine, wherein the combustor is a first combustor and the turbine is a first turbine downstream of the first combustor, and the gas turbine also has a second combustor downstream of said first turbine, and a second turbine downstream of said second combustor. ### Claim 14 (depends on 1) The method as claimed in claim 1, wherein the turbine is a second turbine and the combustor is a second combustor, wherein the gas turbine is configured as a sequential combustion gas turbine having a first combustor, a first turbine downstream of the first combustor, the second combustor downstream of said first turbine, and the second turbine downstream of said second combustor. ### Claim 15 (depends on 1) The method of claim 1, wherein the selection criteria is the having the specified data quality and the specified data quality is based on one of a relative load and an inlet guide vane position. ### Claim 16 (depends on 1) The method of claim 1, wherein the selection criteria is the having the specified data quality and the specified data quality is based on time since a start up of the gas turbine. ### Claim 17 A gas turbine comprising: a compressor; a combustor; a turbine downstream of the combustor, sensors distributed at a total number of measurement points about the turbine; and a controller, wherein the controller is configured to carry out a method which includes: determining with the sensors a turbine outlet temperature measurement at each of the total number of measurement points to yield a total number of turbine outlet temperature measurements; obtaining a reference average turbine outlet temperature based on all the turbine outlet temperature measurements determined at each of the total number of measurement points; selecting a number of the turbine outlet temperature measurements, which is smaller than the total number of the turbine outlet temperature measurements, as selected turbine outlet temperature measurements, wherein the selecting is performed by determining ones of the turbine outlet temperature measurements which satisfy a selection criteria; averaging the selected turbine outlet temperature measurements to obtain a value of an average turbine outlet temperature; controlling an operation of the gas turbine in dependence of a deviation calculated between the reference average turbine outlet temperature obtained and the value of the average turbine outlet temperature; and wherein the selection criteria includes one of: having a specified data quality, having a measurement value within a specified number of highest measurement values considering all the turbine outlet temperature measurements determined at each of the total number of measurement points, and having a measurement value within a specified temperature deviation from a previously obtained value of the average turbine outlet temperature. ### Claim 18 (depends on 17) The gas turbine of claim 17, wherein the combustor is a first combustor and the turbine is a first turbine and wherein the gas turbine also comprises: a second combustor downstream of the first turbine and a second turbine downstream of the second combustor. ### Claim 19 (depends on 17) The gas turbine of claim 17, wherein the combustor is a second combustor and the turbine is a second turbine and wherein the gas turbine also comprises: a first combustor upstream of a first turbine, the second combustor being downstream of the first turbine. ### Claim 20 (depends on 17) The gas turbine of claim 17, wherein the sensors include thermocouples.