General Electric Company

Exxonmobil Upstream Research Company

Jonathan Carl Thatcher

Aaron Lavene Vorel

Karl Dean Minto

Justin Varkey John

Richard Alan Huntington

Bryan Edward Sweet

Brian Michael Gallagher

Ravi Praveen S Eluripati

Priscilla Childers

Bin Xu

Lalit Keshav Mestha

Steven Sebastian Burdgick

Harry Kirk Mathews, Jr

Robert Joseph Iasillo

Kevin Thomas McCarthy

Ravi Rajamani

William Forrester Seely

Timothy Andrew Healy

Krishna Kumar Venkataraman

Ilya Aleksandrovich Slobodyanskiy

Roger C Walker

James Anthony West

Daniel Francis Holzhauer

Bruce Gordon Norman

Aditya Kumar

Thomas Raymond Farrell

Christopher Eugene Long

Sal Albert Leone

John Rogers Huey

Sameer Vittal

Ruijie Shi

Anup Menon

Jesse Edwin Trout

John Carver Maters

John Harry Down

Olugbenga Moses Anubi

Robert William Grubbs

Brian Allen Rittenhouse

Tagir Nigmatulin

Joshua Adam Bagwell

Marc Gavin Lindenmuth

Robert Joseph Loeven, Ii

Mark Disch

Steve W Backman

Anju Narendra

Scott Michael Schaberg

Amanda Rose Peck

Alberto José Negroni

John Paul Metz

Sree Rama Raju Vetukuri

Garth Frederick, Ii

Scott Schaberg

A fluid monitoring system includes a controller configured to determine that a value of at least one fluid property of a fluid is greater than a threshold value, and to control actuators to identify which fluid source has the fluid with the value of the at least one fluid property greater than the threshold value. Each actuator is configured to drive a respective crossover valve between a first position and a second position to direct the fluid from a respective first fluid source to a first manifold or a second manifold and to direct the fluid from a respective second fluid source to the first manifold or the second manifold. In addition, the first manifold is configured to direct the fluid to a first sensor assembly, and the second manifold is configured to direct the fluid to a second sensor assembly.

Fluid monitoring system

A method of controlling an operating temperature of a first combustion zone of a combustor of a rotary machine includes determining a current operating temperature and a target operating temperature of a first combustion zone using a digital simulation. The method further includes determining a derivative of the current operating temperature with respect to a current fuel split using the digital simulation. The fuel split apportions a total flow of fuel to the combustor between the first combustion zone and a second combustion zone. The method also includes calculating a calculated fuel split that results in a calculated operating temperature approaching the target operating temperature. The method further includes channeling a first flow of fuel to the first combustion zone and a second flow of fuel to the second combustion zone.

Systems and methods for determination of gas turbine fuel split for head end temperature control

A system includes a control system configured to control one or more parameters of an exhaust gas recirculation (EGR) gas turbine system to control a portion of electrical power for export from a generator driven by the turbine to an electrical grid. The control system includes a closed-loop controller configured to control parameters of the EGR gas turbine system and an open-loop controller configured to temporarily control the parameters of the EGR gas turbine system to increase the portion of the electrical power exported to the electrical grid to provide a Primary Frequency Response (PFR) in response to a transient event associated with the electrical power. The open-loop controller is configured to provide control signals to increase a concentration of an oxidant in a combustor to provide the PFR in response to the transient event when the EGR gas turbine system is operating in an emissions compliant mode.

System and method for a stoichiometric exhaust gas recirculation gas turbine system

A dispatch optimization system leverages ambient and market forecast data as well as asset performance and parts-life models to generate recommended operating schedules for gas turbines or other power-generating plant assets that substantially maximize profit while satisfying parts-life constraints. The system generates operating profiles that balance optimal peak fire opportunities with optimal cold part-load opportunities within a maintenance interval or other operating horizon. During real-time operation of the assets, the optimization system can update the operating schedule based on actual market, ambient, and operating data. The system provides information that can assist operators in determining suitable conditions in which to cold part-load or peak-fire the assets in an optimally profitable manner without violating target life constraints.

Gas turbine dispatch optimizer real-time command and operations

A gas turbine system includes a combustor configured to combust an oxidant and a fuel in the presence of an exhaust gas diluent to produce combustion products, an oxidant supply path fluidly coupled to the combustor and configured to flow the oxidant to the combustor at an oxidant flow rate, and a turbine configured to extract work from the combustion products to produce an exhaust gas used to generate the exhaust gas diluent. The turbine causes a shaft of the gas turbine system to rotate when the work is extracted from the combustion products. The system also includes an electrical generator that generates electrical power in response to rotation by the shaft, and a controller that performs load control in response to a target load by adjusting the oxidant flow rate along the oxidant flow path as a primary load control parameter.

Gas turbine load control system

A non-transitory, computer readable medium stores instructions executable by a processor of an electronic device. The instructions include instructions to determine that a transient event is occurring in an electrical grid coupled to an EGR gas turbine system, wherein the transient event is an under-frequency or an under-voltage event. The instructions also include instructions to increase a flow rate of fuel to a combustor of the EGR gas turbine system in response to the transient event when the EGR gas turbine system is operating in a non-stoichiometric combustion mode. The instructions further include instructions to increase a flow rate of oxidant to the combustor before increasing the flow rate of fuel to the combustor, or to decrease a local consumption of the electrical power to increase a portion of the electrical power that is exported to the attached electrical grid, or both, in response to the transient event when the EGR gas turbine system is operating in a stoichiometric combustion mode.

A method of controlling an exhaust gas recirculation (EGR) gas turbine system includes adjusting an angle of a plurality of inlet guide vanes of an exhaust gas compressor of the EGR gas turbine system, wherein the plurality of inlet guide vanes have a first range of motion defined by a minimum angle and a maximum angle, and wherein the angle is adjusted based on one or more monitored or modeled parameters of the EGR gas turbine system. The method further includes adjusting a pitch of a plurality of blower vanes of a recycle blower disposed upstream of the exhaust gas compressor, wherein the plurality of blower vanes have a second range of motion defined by a minimum pitch and a maximum pitch, and the pitch of the plurality of blower vanes is adjusted based at least on the angle of the plurality of inlet guide vanes.

Systems and methods for controlling exhaust gas flow in exhaust gas recirculation gas turbine systems

A normal space data source stores, for each of a plurality of threat nodes, a series of normal values that represent normal operation of an industrial asset control system, and a threatened space data source stores a series of threatened values. A model creation computer may generate sets of normal and threatened feature vectors. The computer may also calculate and output at least one decision boundary for a threat detection model based on the normal and threatened feature vectors. The plurality of threat nodes may then generate a series of current values from threat nodes that represent a current operation of the asset control system. A threat detection computer may receive the series of current values from threat nodes, generate a set of current feature vectors, execute the threat detection model, and transmit a threat alert signal based on the current feature vectors and at the least one decision boundary.

Domain level threat detection for industrial asset control system

A system includes an exhaust gas recirculation (EGR) gas turbine system which includes a combustor configured to receive and combust a fuel with an oxidant and a turbine driven by combustion products from the combustor and a turbine driven by combustion products from the combustor. The EGR gas turbine system further includes an exhaust gas recirculation section fluidly coupled to the turbine and to the combustor, wherein the exhaust gas recirculation section is configured to intake an exhaust gas from the turbine and to recirculate at least a portion of the exhaust gas to the combustor as a diluent. The EGR gas turbine system additionally includes a control system, comprising one or more processors configured to receive a first signal representative of an exhaust flow composition of the exhaust gas and to receive a second signal representative of a diluent flow composition of the diluent.

Systems and methods of estimating a combustion equivalence ratio in a gas turbine with exhaust gas recirculation

A method includes combusting a fuel and an oxidant in a combustor of an exhaust gas recirculation (EGR) gas turbine system that produces electrical power and provides a portion of the electrical power to an electrical grid. The method further includes controlling, via one or more processors, one or more parameters of the EGR gas turbine system to decrease the portion of the electrical power provided to the electrical grid in response to an over-frequency event associated with the electrical grid, wherein controlling the one or more parameters comprises decreasing a flow rate of fuel to the combustor in response to the over-frequency event.

Systems and methods to respond to grid overfrequency events for a stoichiometric exhaust recirculation gas turbine

A dynamic alarm system for operating a power plant is disclosed. The dynamic alarm system includes a sensor configured to generate a signal related to a measurement of an operation of the power plant. An interface displays a generated alarm to an operator and receives a dynamic rating value from the operator related to the generated alarm. A processor generates the alarm using the generated signal, compiles the rating value and alters an operation of the power plant from the compiled rating value.

Dynamic alarm system for operating a power plant and method of responding to same

A system and method for enhancing operation of a power generation system. The method includes receiving forecasts at a predictive control unit. The method also includes accessing via a controller real-time lifing models or near real-time lifing models in the predictive control unit. Additionally, the method includes accessing via the controller an enhancer configured to simulate operation of a power generating unit in the power generation system to generate an enhancement of the power generation system based on the forecasts and the real-time or near real-time lifing models.

System and method for enhancement of power generation facilities

A system and method to reduce the gas fuel supply pressure requirements of a gas turbine, which results in an increased operability range and a reduction in gas turbine trips. According to the method, the gas turbine is allowed to start and operate at supply pressures determined as a function of ambient conditions and gas turbine compressor pressure ratio. This increases the operability window, and reduces or eliminates the need for gas fuel compressors.

Pressure control method and system to reduce gas turbine fuel supply pressure requirements

An embodiment of the present invention may incorporate a physics based approach (hereinafter 'model') to determine the level of the liquid. The model may incorporate the physical properties of the fluids within the container, and measurements of the fluid under consideration. The model may also incorporate data from measuring devices, such as, but not limiting of, a delta-pressure (DP) transmitter. The model may then calculate, within a reasonable level of accuracy, the level of the fluid within the container.

System and method for measuring a level of a liquid in a container

Systems and methods for controlling the clearance in a gas turbine are provided. A temperature of a shaft of the gas turbine may be determined, and a desired temperature of an inner turbine shell of the turbine may be determined based upon the temperature of the shaft. The desired temperature of the inner turbine shell may be associated with a turbine clearance at which the gas turbine may be ignited. The temperature of the inner turbine shell may be altered by controlling the temperature of a gas that is circulated within the inner turbine shell, and a determination may be made that the temperature of the inner turbine shell exceeds the desired temperature. The gas turbine may be ignited subsequent to the determination that the temperature of the inner turbine shell exceeds the desired temperature.

Methods and systems for controlling gas turbine clearance

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Pendleton, SC, United States of America

Jonathan Carl Thatcher