# US 5,704,205 A · Method of setting a main controlled variable during the operation of a gas-turbine group > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 5,704,205 A - Document ID: US5704205A - Status: Granted - Kind: A - Application number: 08/609,838 - Filed: 1996-03-01 - Granted: 1998-01-06 - Earliest claimed: 1995-05-08 - Assignees: Asea Brown Boveri AG - Inventors: Stephan Hepner; Johann-Kaspar Scherrer; Bozidar Seketa - Web page: https://patentgrep.com/patent/US5704205A ## 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) - 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) ## Abstract In a method of setting a main controlled variable during the operation of a gas-turbine group, the gas-turbine group essentially comprises a compressor (40), at least one combustion chamber (43), at least one turbine (41) and a generator (46). A desired value (3) is compared with a measured value (4) and the resulting main control difference (5) is hierarchically allocated via a management unit (1) to at least one cascade (9, 18). The cascade (9, 18) is essentially composed of a main-controlled-variable controller (6, 15) and a downstream variable controller (8, 17) which acts on the respective variable actuator (14, 23). ## Claims ### Claim 1 A method of adjusting a main controlled parameter during operation of a gas-turbine group, the gas-turbine group including a compressor, at least one combustion chamber, at least one turbine and a generator, the method comprising the steps of: comparing a desired value of a main controlled parameter with a measured value of the main controlled parameter to determine a main controlled parameter difference; allocating the difference in portions by a management unit as difference signals to at least two control cascades, each cascade controlling a different operating variable and having a main-controlled-parameter controller to receive the allocated difference signal from the management unit and convert the difference signal for use by a variable controller which acts on a respective variable actuator, wherein, the two control cascades each adjust the respective variable according to the allocated difference signal to correct for a portion of the main controlled parameter difference. ### Claim 2 (depends on 1) The method as claimed in claim 1, wherein the output power of the gas turbine is the main controlled parameter. ### Claim 3 (depends on 1) The method as claimed in claim 1, wherein the rotational speed of the turbine is the main controlled parameter. ### Claim 4 (depends on 2) The method as claimed in claim 2 wherein the at least two control cascades includes a temperature cascade comprising a main-controlled-parameter controller and a temperature controller. ### Claim 5 (depends on 4) The method as claimed in claim 4, wherein a fuel mass-flow setting actuator is used as the actuator of the temperature controller. ### Claim 6 (depends on 2) The method as claimed in claim 2, wherein the at least two control cascades includes a compressor output pressure cascade comprising a main-controlled-parameter controller and a compressor output pressure controller. ### Claim 7 (depends on 6) The method as claimed in claim 6, wherein a guide-vane setting actuator in the compressor is the actuator of the compressor output pressure controller. ### Claim 8 (depends on 2) The method as claimed in claim 2, wherein, the management unit allocates to a first cascade a main controlled parameter difference portion corresponding to a capacity of the first cascade to adjust a first operating variable, and when the capacity of the first cascade is reached, the management unit allocates a remaining portion of the difference to a second cascade to adjust a second operating variable. ### Claim 9 (depends on 8) The method as claimed in claim 8, wherein said first cascade is a temperature cascade. ### Claim 10 (depends on 8) The method as claimed in claim 8, wherein the gas turbine group includes in series a first turbine having a first combustion chamber and a second turbine having a second combustion chamber, and wherein the method comprises allocating a main controlled parameter difference to a temperature cascade for adjusting the first combustion chamber. ### Claim 11 A method of adjusting one of turbine power output and turbine speed during operation of a gas-turbine group, the gas-turbine group including a compressor, at least one combustion chamber, at least one turbine and a generator, the method comprising the steps of: measuring one of a turbine power output and turbine speed to determine an output parameter value; comparing a desired output parameter value with the measured output parameter value to determine a difference value; distributing a first and second difference signal each based on a different portion of the difference value respectively to a turbine inlet temperature control cascade and a compressor output pressure control cascade, each cascade having an output parameter controller to receive the difference signal and convert the difference signal for use by a variable controller which acts on a respective variable actuator; wherein, the turbine inlet temperature control cascade receives the first difference signal and adjusts a fuel mass flow according to the first difference signal and the compressor output pressure control cascade receives the second difference signal and adjusts the compressor output pressure according to the second difference signal so that each cascade corrects for a portion of the output parameter difference.