Abstract
Thermo-acoustic instabilities in gas turbine engines are studied to avoid engine failure. Compared to the engines with annular combustors, the can-annular combustor design should be less vulnerable to acoustic burner-to-burner interaction, since the burners are acoustically coupled only by the turbine stator stage and the plenum. However, non-negligible cross-talk between neighboring cans has been observed in measurements in such machines. This study is focused on the analysis of the acoustic interaction between the cans. Simplified two-dimensional (2D) and three-dimensional (3D) equivalent systems representing the corresponding engine alike turbine design are investigated. Thermo-acoustic instabilities are reproduced using a forced response approach. Compressible large eddy simulation based on the open source computational fluid dynamics OpenFOAM framework is used applying accurate boundary conditions for the flow and the acoustics. A study of the reflection coefficient and of the transfer function between the cans has been performed. Comparisons between 2D and 3D equivalent configurations have been evaluated.
Original language | English |
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Pages (from-to) | 452-469 |
Number of pages | 18 |
Journal | International journal of spray and combustion dynamics |
Volume | 9 |
Issue number | 4 |
DOIs | |
Publication status | Published - 1 Dec 2017 |
Keywords
- combustion instabilities
- cross-talk
- reflection coefficient
- Thermo-acoustics
- transmission coefficient