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Combustion instabilities.
Active control can be used to stabilize combustion instabilities.
At RGD, his work focuses on using nanosecond pulsed non-equilibrium plasma discharges to control combustion instabilities.
Combustion instabilities consist in self exited oscillations in combustion chambers and can cause structure degradations.
Thermoacoustic combustion instabilities are a frequently encountered problem in the operation of combustion equipment.
Lean premixed combustors produce lower NOx emissions, but are particularly prone to damaging combustion instabilities.
New generation combustion chambers are designed to reduce pollutant emissions and combustion instabilities.
Self-pulsation must be suppressed since this oscillation may cause combustion instabilities.
At MIT, he is presently working on understanding and control of combustion instabilities in swirl and backward step combustors that burn carbon-monoxide/hydrogen/propane blends.
The Prediction and Control of Combustion Instabilities in Industrial Gas Turbines (PRECCINSTA) project, financed by the European Commission Fifth Framework, concerns prediction and control of combustion instabilities in tubular and annular gas turbine combustors.
As lean premixed combustion systems are more susceptible to combustion instabilities than non-premixed systems, there is an increasing demand for improved numerical design tools that can predict the occurrence of combustion instabilities with high accuracy.
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