Adaptive model-based control systems and methods for controlling a gas turbine
AssigneeGeneral Electric Company
InventorsBrent Jerome Brunell, Harry Kirk Mathews, Jr., Aditya Kumar
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AssigneeGeneral Electric Company
InventorsBrent Jerome Brunell, Harry Kirk Mathews, Jr., Aditya Kumar
Estimating the term…
Adaptive model-based control systems and methods are described so that performance and/or operability of a gas turbine in an aircraft engine, power plant, marine propulsion, or industrial application can be optimized under normal, deteriorated, faulted, failed and/or damaged operation. First, a model of each relevant system or component is created, and the model is adapted to the engine. Then, if/when deterioration, a fault, a failure or some kind of damage to an engine component or system is detected, that information is input to the model-based control as changes to the model, constraints, objective function, or other control parameters. With all the information about the engine condition, and state and directives on the control goals in terms of an objective function and constraints, the control then solves an optimization so the optimal control action can be determined and taken. This model and control may be updated in real-time to account for engine-to-engine variation, deterioration, damage, faults and/or failures using optimal corrective control action command(s).
An adaptive model-based control method for controlling a gas turbine engine to optimize either performance or operability of the engine, the method comprising:
An adaptable model-based control system for controlling a gas turbine engine to optimize either performance or operability of the engine, the system comprising:
An adaptable model-based control system capable of controlling a gas turbine engine to optimize either performance or operability of the engine, the control system comprising:
Dependencies are inferred from the claim text.