GAS TURBINE LOWER HEATING VALUE METHODS AND SYSTEMS
First Claim
1. A control system for a gas turbine system, comprising:
- a controller comprising a processor, wherein the processor is configured to;
receive a plurality of signals comprising a temperature signal, a pressure signal, a speed signal, a mass flow signal, or a combination thereof, from sensors disposed in the gas turbine system;
apply the plurality of signals as input to a heating value model;
execute the heating value model to derive a heating value for a fuel combusted by the gas turbine system;
control operations of the gas turbine system based on the heating value for the fuel.
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Accused Products
Abstract
A control system for a gas turbine includes a controller. The controller includes a processor configured to receive a plurality of signals comprising a temperature signal, a pressure signal, a speed signal, a mass flow signal, or a combination thereof, from sensors disposed in the gas turbine system. The processor is further configured to apply the plurality of signals as input to a heating value model. The processor is also configured to execute the heating value model to derive a heating value for a fuel combusted by the gas turbine system. The processor is additionally configured to control operations of the gas turbine system based on the heating value for the fuel.
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Citations
20 Claims
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1. A control system for a gas turbine system, comprising:
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a controller comprising a processor, wherein the processor is configured to; receive a plurality of signals comprising a temperature signal, a pressure signal, a speed signal, a mass flow signal, or a combination thereof, from sensors disposed in the gas turbine system; apply the plurality of signals as input to a heating value model; execute the heating value model to derive a heating value for a fuel combusted by the gas turbine system; control operations of the gas turbine system based on the heating value for the fuel. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8)
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9. A non-transitory computer-readable medium having computer executable code stored thereon, the code comprising instructions to:
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receive a plurality of signals comprising a temperature signal, a pressure signal, a speed signal, a mass flow signal, or a combination thereof, from sensors disposed in the gas turbine system; apply the plurality of signals as input to a heating value model; execute the heating value model to derive a heating value for a fuel combusted by the gas turbine system; control operations of the gas turbine system based on the heating value for the fuel. - View Dependent Claims (10, 11, 12, 13, 14, 15)
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16. A method for a gas turbine system, comprising:
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receiving a plurality of signals comprising a temperature signal, a pressure signal, a speed signal, a mass flow signal, or a combination thereof, from sensors disposed in the gas turbine system; applying the plurality of signals as input to a heating value model; executing the heating value model to derive a heating value for a fuel combusted by the gas turbine system; controlling operations of the gas turbine system based on the heating value for the fuel. - View Dependent Claims (17, 18, 19, 20)
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Specification