Systems and methods for control of operating life of a gas turbine
First Claim
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1. A system, comprising:
- a gas turbine system comprising a compressor, combustor, and a turbine;
a controller communicatively coupled to the gas turbine system and configured to control operations of the gas turbine system; and
a life consumption model configured, during the gas turbine system operating under a load operating condition, to determine an operating life of the gas turbine system based on both a health status of one or more components of the gas turbine system and operating conditions of the gas turbine system, wherein the controller, during the gas turbine system operating under the load operating condition, is configured to utilize at least the life consumption model to derive and output a control action for the gas turbine system, and the operating conditions comprise actual operating conditions or statistically derived estimates of most likely operating conditions during the load operating condition;
wherein the life consumption model is configured, during the gas turbine system operating under the load operating condition, to calculate an actual life consumption rate for the gas turbine system based on both the health status of the one or more components of the gas turbine system and the operating conditions of the gas turbine system.
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Abstract
A system includes a gas turbine system including a compressor, a combustor, and a turbine. The system also includes a controller communicatively coupled to the gas turbine system and configured to control operations of the gas turbine system. The system further includes a life consumption model configured to determine an operating life of the gas turbine system based on both a health status of one or more components of the gas turbine system and operating conditions of the gas turbine system. The controller is configured to utilize at least the life consumption model to derive a control action for the gas turbine system.
18 Citations
15 Claims
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1. A system, comprising:
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a gas turbine system comprising a compressor, combustor, and a turbine; a controller communicatively coupled to the gas turbine system and configured to control operations of the gas turbine system; and a life consumption model configured, during the gas turbine system operating under a load operating condition, to determine an operating life of the gas turbine system based on both a health status of one or more components of the gas turbine system and operating conditions of the gas turbine system, wherein the controller, during the gas turbine system operating under the load operating condition, is configured to utilize at least the life consumption model to derive and output a control action for the gas turbine system, and the operating conditions comprise actual operating conditions or statistically derived estimates of most likely operating conditions during the load operating condition; wherein the life consumption model is configured, during the gas turbine system operating under the load operating condition, to calculate an actual life consumption rate for the gas turbine system based on both the health status of the one or more components of the gas turbine system and the operating conditions of the gas turbine system. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8)
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9. A method, comprising:
during a gas turbine system operating under a load operating condition; receiving at least one turbine operating condition of the gas turbine system, wherein the at least one turbine operating condition comprises an actual operating condition or a statistically derived estimate of a most likely operating condition during the load operating condition; receiving a health status of at least one component of the gas turbine system; modeling an operating life of the gas turbine system based on the at least one turbine operating condition and the health status of the at least one component; calculating an actual life consumption rate for the gas turbine system based on the at least one turbine operating condition and the health status of the at least one component; and outputting a control action based on at least the operating life of the gas turbine system for controlling the gas turbine system. - View Dependent Claims (10, 11, 12, 13)
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14. A non-transitory computer-readable medium having computer executable code stored thereon, the code comprising instructions for:
during a gas turbine system operating under a load operating condition; receiving at least one turbine operating condition of the gas turbine system, wherein the at least one turbine operating condition comprises an actual operating condition or a statistically derived estimate of a most likely operating condition during the load operating condition; receiving a health status of at least one component of the gas turbine system; modeling an operating life of the gas turbine system based on the at least one turbine operating condition and the health status of the at least one component; calculating an actual life consumption rate for the gas turbine system based on the at least one turbine operating condition and the health status of the at least one component; and outputting a control action based on at least the operating life of the gas turbine system for controlling the gas turbine system. - View Dependent Claims (15)
Specification