Dynamic tuning of a gas turbine engine to detect and prevent lean blowout
AssigneeAnsaldo Energia IP UK Limited
InventorsPeter John Stuttaford, Sumit Soni, Donald Gauthier, Hany Rizkalla
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AssigneeAnsaldo Energia IP UK Limited
InventorsPeter John Stuttaford, Sumit Soni, Donald Gauthier, Hany Rizkalla
Estimating the term…
A method for tuning a combustor of a gas turbine engine based on one or more monitored operating conditions is provided. One or more operating conditions of the gas turbine engine are monitored. The monitored operating conditions may include, for example, a low frequency tone, a high frequency tone, and a ratio of the low frequency tone to the high frequency tone. It is determined whether the ratio of the low frequency tone to the high frequency tone is within a first predefined normal range. If the ratio of the low frequency tone to the high frequency tone is within the first predefined normal range, a determination is made not to tune the gas turbine engine. But, if the ratio of the low frequency tone to the high frequency tone is not within the first predefined normal range, a determination is made to tune the gas turbine engine.
One or more non-transitory computer-readable media that, when invoked by computer-executable instructions, perform a method for tuning a combustor of a gas turbine engine based on one or more monitored operating conditions, the method comprising:
A system for automatically tuning a combustor of a gas turbine engine based on one or more monitored operating conditions, the system comprising:
One or more non-transitory computer-readable media that, when invoked by computer-executable instructions, perform a method for tuning a combustor of a gas turbine engine based on one or more monitored operating conditions, the method comprising:
Dependencies are inferred from the claim text.