Gas turbine engine control system
AssigneeROLLS-ROYCE plc
InventorMarcus S Horobin
Life of this patent
Estimating the term…
Loading patent…
AssigneeROLLS-ROYCE plc
InventorMarcus S Horobin
Estimating the term…
A computer-based control system for a gas turbine engine includes: a controller including control logic, the controller obtains a set of inputs formed by measurements of one or more process variables and values of one or more engine operation set points, and the control logic determines one or more process command values gas turbine engine operation in response to the set of inputs; and an event detection unit obtaining further measurements of one or more process variables and determine whether an abnormal event has occurred based on the further measurements of one or more process variables. The controller also updates the tuning variables using an event accommodation data array, a given tuning variable being changed in response to detection of a given abnormal event when the respective element in the event accommodation data array is assigned an intervention value.
A computer-based control system for a gas turbine engine, comprising:
A computer implemented method of detecting and accommodating an abnormal event in the operation of a gas turbine engine using a control system, wherein:
Dependencies are inferred from the claim text.