Systems and methods for generating variable ramp rates for turbomachinery

US2016195026A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2016195026-A1
Application numberUS-201514590513-A
CountryUS
Kind codeA1
Filing dateJan 6, 2015
Priority dateJan 6, 2015
Publication dateJul 7, 2016
Grant date

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Abstract

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A system includes a controller configured to receive one or more inputs associated with an operation of a turbine system, derive a set of ramp rates for the turbine system based at least in part on the one or more inputs, and to select a ramp rate from the set of ramp rates. The ramp rate includes a variable ramp rate. The controller is further configured to generate an output signal based on the selected ramp rate.

First claim

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1 . A system, comprising: a controller configured to: receive one or more inputs associated with an operation of a turbine system; derive a set of ramp rates for the a turbine system based at least in part on the one or more inputs; select a ramp rate from the set of ramp rates, wherein the ramp rate comprises a variable ramp rate; and generate an output signal based on the selected ramp rate. 2 . The system of claim 1 , wherein the controller is configured to receive a user input, a maximum possible ramp rate input, a physics-based model input of the operating parameters of the turbine system, an event detection input, a measured operational parameter input, a scheduling parameter input, or any combination thereof, as the one or more inputs. 3 . The system of claim 1 , wherein the controller is configured to: receive a first physics-based model input of an operating parameter of the turbine system and a second physics-based model input of operating parameters of an industrial system comprising the turbine system; and derive the set of ramp rates for the turbine system by generating a model based control (MBC) model of each a plurality of tolerable ramp rates for the turbine system. 4 . The system of claim 1 , wherein the controller is configured to derive the set of ramp rates for the turbine system based on a ramp rate tolerability of each component of the turbine system. 5 . The system of claim 1 , wherein the controller is configured to select varying ramp rates from the set of ramp rates over an operational period of the turbine system. 6 . The system of claim 5 , wherein the controller is configured to select the varying ramp rates from the set of ramp rates over a loading or over a ramping period of the turbine system. 7 . The system of claim 1 , wherein the controller is configured to derive a set of respective maximum ramp rates for each component of the turbine system as the set of ramp rates. 8 . The system of claim 7 , wherein the controller is configured to select a lowest ramp rate from the set of respective maximum ramp rates for each component of the turbine system as the selected ramp rate. 9 . The system of claim 1 , wherein the turbine system comprises a gas turbine, a steam turbine, a generator, a compressor, or any combination thereof. 10 . The system of claim 1 , wherein the controller is configured to be programmably retrofitted with instructions to: derive the set of ramp rates for the turbine system based on the one or more inputs; and select the ramp rate from the set of ramp rates. 11 . A non-transitory computer-readable medium having computer executable code stored thereon, the code comprising instructions to: cause a controller to receive one or more inputs associated with an operation of a turbine system; cause the controller to derive a set of ramp rates for the turbine system based at least in part on the one or more inputs; cause the controller to select a ramp rate from the set of ramp rates, wherein the ramp rate comprises a variable ramp rate; and cause the controller to generate an output signal based on the selected ramp rate. 12 . The non-transitory computer-readable medium of claim 11 , wherein the code comprises instructions to cause the controller to receive a user input, a maximum possible ramp rate input, a physics-based model input of the operating parameters of the turbine system, an event detection input, a measured operational parameter input, a scheduling parameter input, or any combination thereof, as the one or more inputs. 13 . The non-transitory computer-readable medium of claim 11 , wherein the code comprises instructions to: cause the controller to receive a physics-based model input of an operating parameter of the turbine system and a physics-based model input of operating parameters of an industrial system comprising the turbine system; and cause the controller to derive the set of ramp rates for the turbine system by generating a model based control (MBC) model of each a plurality of tolerable ramp rates for the turbine system. 14 . The non-transitory computer-readable medium of claim 11 , wherein the code comprises instructions to cause the controller to derive the set of ramp rates for the turbine system based on a ramp rate tolerable by each component of the turbine system. 15 . The non-transitory computer-readable medium of claim 11 , wherein the code comprises instructions to cause the controller to select varying ramp rates from the set of ramp rates over an operational period of the turbine system. 16 . The non-transitory computer-readable medium of claim 15 , wherein the code comprises instructions to cause the controller to select the varying ramp rates from the set of ramp rates over a loading or a ramping period of the turbine system. 17 . The non-transitory computer-readable medium of claim 11 , wherein the code comprises instructions to cause the controller to derive a set of respective maximum ramp rates for each component of the turbine system as the set of ramp rates. 18 . The non-transitory computer-readable medium of claim 17 , wherein the code comprises instructions to cause the controller to elect a lowest ramp rate from the set of respective maximum ramp rates for each component of the turbine system as the selected ramp rate. 19 . A system, comprising: a gas turbine system; and a controller communicatively coupled to the gas turbine system, comprising: a selector device configured to: receive a plurality of inputs associated with an operation of the gas turbine system, wherein the plurality of inputs comprises a first set of model based operational parameters of the gas turbine system and a second set of sensed operational parameters of the gas turbine system; derive a plurality of ramp rates for the gas turbine system based on the plurality of inputs, wherein the plurality of ramp rates comprises a respective maximum tolerable ramp rate for each component of the gas turbine system; and select one or more ramp rates of the plurality of ramp rates; and a ramp controller device configured to receive the selected one or more ramp rates and to generate an output signal based on the selected one or more ramp rates. 20 . The system of claim 19 , wherein the ramp controller device is configured generate a fuel flow command as the output signal, and wherein the fuel flow command is configured to activate an actuator to control a loading of the gas turbine system.

Assignees

Inventors

Classifications

  • F02C9/28Primary

    Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed (F02C9/30 - F02C9/38, F02C9/44 take precedence) · CPC title

  • having a turbine driving a compressor (power transmission arrangements F02C7/36; control of working fluid flow F02C9/16) · CPC title

  • Rate of change of parameters · CPC title

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What does patent US2016195026A1 cover?
A system includes a controller configured to receive one or more inputs associated with an operation of a turbine system, derive a set of ramp rates for the turbine system based at least in part on the one or more inputs, and to select a ramp rate from the set of ramp rates. The ramp rate includes a variable ramp rate. The controller is further configured to generate an output signal based on t…
Who is the assignee on this patent?
Gen Electric
What technology area does this patent fall under?
Primary CPC classification F02C9/28. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Thu Jul 07 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).