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Interactions between Multiple Unstable Transversal Modes in High-Frequency Thermoacoustic Systems

Subject Area Technical Thermodynamics
Term from 2017 to 2021
Project identifier Deutsche Forschungsgemeinschaft (DFG) - Project number 380974143
 
Final Report Year 2022

Final Report Abstract

This project deals with high-frequency thermoacoustic instabilities in lean-premixed gas turbine combustion systems. These instabilities increasingly often occur after commissioning of modern gas turbine combustors and may lead to hardware damage and/or decrease the operational window of the gas turbine. The research objective of this work represents the qualitative and quantitative prediction of thermoacoustic instabilities from a numerical and theoretical perspective. This allows systematic application of countermeasures to avoid or mitigate unstable behavior. An approach is introduced to predict thermoacoustic instabilities in three separated steps. These steps comprise 1.) the determination of the linear thermoacoustic stability limits, 2.) the identification of non-linear saturation mechanisms leading to the formation of limitcycle oscillations and 3.) the consideration of modal suppression phenomena between linearly unstable eigenmodes. The outcome of this project is an accurate, numerical prediction tool, which allows the efficient prediction of the temporal evolution of multiple, coupled acoustic eigenmodes. Additionally, fundamental numerical studies are carried out to enhance the understanding of the influence of vorticity perturbations on high-frequency thermoacoustic oscillations in general. To judge the performance of the computational tools and to validate numerical investigations, a lab-scale, swirl-stabilized combustor is used as benchmark system. For the first transversal (T1) eigenmode of this combustor extensive experimental data is available.

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