Method of mitigating undesired gas turbine transient response using event based actions
AssigneeGeneral Electric Company
InventorsJason D. Fuller, Derrick W. Simons, Douglas E. Dean, Christopher T. Meadows
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AssigneeGeneral Electric Company
InventorsJason D. Fuller, Derrick W. Simons, Douglas E. Dean, Christopher T. Meadows
Estimating the term…
A method of managing transient events regularly seen during gas turbine operation that may cause undesirable operation and hardware damage. During certain transient operations, a lag may be seen between reference exhaust temperature and actual turbine exhaust temperature. This lag can result in an under-fired condition within the combustion system of variable magnitude and duration. Either fuel split schedules or a control algorithm can be positioned during these transients to prevent combustion dynamics or loss of flame. Combustion dynamics are known to cause damage that may require hardware replacement. Once the transient has completed, normal control operation is resumed.
A controller in a gas turbine having a compressor, a combustor and a turbine with a fuel split schedule, the controller comprising:
A method for mitigating undesired gas turbine transient response using event-based actions wherein a difference between a measured reference exhaust temperature and an actual turbine exhaust temperature may result in at least one of combustion dynamics or loss of flame;
A gas turbine comprising:
Dependencies are inferred from the claim text.