System and method for turbine engine adaptive control for mitigation of instabilities
AssigneeHoneywell International Inc.
InventorsIan Critchley, Bruce Anson, Matthew Caspermeyer, Mike Scott
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AssigneeHoneywell International Inc.
InventorsIan Critchley, Bruce Anson, Matthew Caspermeyer, Mike Scott
Estimating the term…
The present invention provides an adaptive combustion controller and method for a turbine engine. The adaptive combustion controller and method modulates the fuel flow to the turbine engine combustor to reduce combustion instabilities. In particular, the adaptive combustion controller includes a fuel flow phase controller and a fuel flow magnitude controller. The adaptive combustion controller receives sensor data from the turbine engine. In response to the sensor data the fuel flow phase controller adjusts the phase of the modulated fuel flow to reduce instabilities in the combustor. Likewise, in response to the sensor data the fuel flow magnitude controller adjusts the magnitude of the modulated fuel flow to further reduce the instabilities in the combustor. By modulating the fuel flow to the combustor, and adaptively adjusting the phase and magnitude of the modulated fuel flow, the adaptive combustion controller is able to effectively reduce combustion instabilities.
An adaptive combustion controller for a turbine engine, the adaptive combustion controller receiving sensor data from a combustor in the turbine engine, the adaptive combustion controller comprising:
A method for reducing combustion instabilities in a turbine engine, the method comprising the steps of
An adaptive combustion controller for a turbine engine, the adaptive combustion controller comprising:
Dependencies are inferred from the claim text.