System and method for controlling operation of a gas turbine based power plant
First Claim
1. A system for controlling a gas turbine, comprising:
- a plurality of sensors, each sensor being configured to sense and communicate a signal indicative of an operating parameter of the gas turbine;
a control system including a computing device in electronic communication with each sensor of the plurality sensors, wherein the control system is configured to;
receive the signals from the sensors, at least one of the signals being indicative of a fuel parameter;
compute cumulative wear for one or more hardware components of the gas turbine based at least in part on the fuel parameter and a combustor type of the gas turbine via the computing device;
receive input instructions selecting a desired operating mode for the gas turbine;
compute a hardware consumption rate based at least in part on the cumulative wear and the desired operating mode via the computing device;
display the hardware consumption rate to an operator via a display device that is in electronic communication with the control system; and
adjust the desired operating mode of the gas turbine based at least in part on the hardware consumption rate and a cost of fuel.
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Accused Products
Abstract
A system for controlling a gas turbine power plant includes a plurality of sensors configured to transmit signals indicative of one or more operating parameters of the gas turbine, and a control system in electronic communication with each sensor. The control system is configured to compute cumulative wear for one or more hardware components of the gas turbine based at least in part on the signals. Instructions are inputted into the control system which indicates a desired operational mode for the gas turbine. The control system may then compute a hardware consumption rate based at least in part on the cumulative wear. The hardware consumption rate may then be displayed to an operator via a display device. The operator may use the hardware consumption rate to determine potential economic impact of operating the gas turbine at the desired operational mode.
17 Citations
20 Claims
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1. A system for controlling a gas turbine, comprising:
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a plurality of sensors, each sensor being configured to sense and communicate a signal indicative of an operating parameter of the gas turbine; a control system including a computing device in electronic communication with each sensor of the plurality sensors, wherein the control system is configured to; receive the signals from the sensors, at least one of the signals being indicative of a fuel parameter; compute cumulative wear for one or more hardware components of the gas turbine based at least in part on the fuel parameter and a combustor type of the gas turbine via the computing device; receive input instructions selecting a desired operating mode for the gas turbine; compute a hardware consumption rate based at least in part on the cumulative wear and the desired operating mode via the computing device; display the hardware consumption rate to an operator via a display device that is in electronic communication with the control system; and adjust the desired operating mode of the gas turbine based at least in part on the hardware consumption rate and a cost of fuel. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10)
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11. A method for controlling a gas turbine, comprising:
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computing cumulative wear for a hardware component of the gas turbine based at least in part on a fuel parameter and a combustor type of the gas turbine via a computing device of a control system; inputting into the control system a desired operating mode for the gas turbine; computing via the computing device a hardware consumption rate based at least in part on the cumulative wear and the desired operating mode; providing the hardware consumption rate to an operator via a display device; and adjusting the desired operating mode of the gas turbine based at least in part on the hardware consumption rate and a cost of fuel. - View Dependent Claims (12, 13, 14, 15, 16, 17, 18, 19)
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20. A system for controlling a gas turbine, comprising:
a sensor configured to sense and communicate a signal indicative of a fuel parameter of the gas turbine;
a control system including a computing device in electronic communication with the sensor, wherein the control system is configured to;receive the signal indicative of the fuel parameter from the sensor; compute cumulative wear for one or more hardware components of the gas turbine based on the fuel parameter via the computing device; receive input instructions selecting a desired operating mode for the gas turbine; compute a hardware consumption rate based at least in part on the cumulative wear and the desired operating mode via the computing device; and adjust the desired operating mode of the gas turbine based at least in part on the hardware consumption rate and a cost of fuel.
Specification