CLEANERFLAMES · CompLex thErmoAcoustic iNteraction mEchanisms in spRay Flames in Low-nox Annular coMbustion chambErS
Horizon 2020 — Marie Skłodowska-Curie Actions
- Duration
- 2019-09-16 → 2021-09-15
- EU contribution
- €184,708
- Participants
- 1
- Scheme
- MSCA-IF-EF-SE
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Results in brief
CompLex thErmoAcoustic iNteraction mEchanisms in spRay Flames in Low-nox Annular coMbustion chambErS
Modern land-base gas turbines and aeroengines operating in lean conditions to reduce the production of pollutants, such as NOx, are known to be prone to thermoacoustic instabilities, an undesirable behaviour that needs to be avoided. It is well known that at the origin of these phenomena is the closure of a feedback loop between the noise produced by the flame and the response of the flame itself to acoustic waves. However, a complete understanding of all the mechanisms leading to this coupling still remains a challenge. To this scope, the impossibility of having full access to the combustion chamber and the burner limit the experimental analyses. Studies relying on high-fidelity numerical simulations are therefore necessary. During the project CLEANERFLAMES, multiple activities have been accomplished to understand this coupling for liquid fuelled flames. At first, the capability of reproducing self-sustained limit cycle via high-fidelity simulations with an Euler-Lagrange approach have been proved. Numerical results have been used to complement experimental observation revelling coupling mechanisms between liquid phase and acoustic of the system. Finally, results from LES simulations have been used inside a novel low-order acoustic network modeling tool STORM (State-space Reduced- Order-Modeling) able to perform stability analysis of annular combustion chambers.
Data: CORDIS, © European Union
Project objective
This project is focused on the fundamental problem of combustion dynamics that has many practical implications. It specifically considers annular systems like those used in land based gas turbines and aeroengines. The corresponding combustors feature new architectures that reduce pollutant NOx emissions to comply with increasingly stringent regulations. However, these new designs and the essentially lean premixed mode they employ also promote a resonant coupling between combustion and acoustic modes. These combustion instabilities have many detrimental effects leading in extreme cases to mechanical failure. Despite the large number of investigations concerning instabilities arising with premixed flames yet few are the studies dealing with cases where the fuel is injected as a spray. Furthermore, the limited availability of engine data is a further obstacle for these studies in a real combustor. The present project aims to fill this gap of knowledge by proposing combined numerical and experimental investigations on spray flame dynamics and spray flame coupling with azimuthal modes in annular systems. The project first focuses on the analysis of the nonlinear response of a single spray flame to incoming acoustic perturbations via Large Eddy Simulations. The study is then extended to a multiple swirl spray injector injector system to investigate the impact on the flame response of the interaction between multiple adjacent flames. Numerical results are compared with experiments carried out in unique facilities available at EM2C Laboratory including the annular MICCA-Spray combustor. Theoretical and numerical procedures involving advanced coupling of the combustor acoustics with the obtained flame responses are developed to predict the limit cycles observed during experiments. Finally, the combustion dynamics observed experimentally in a Safran Aircraft Engine combustor will be investigated to verify the transferability of the developed techniques to a full-scale system.
Original text from CORDIS.
Participants
- CENTRE EUROPEEN DE RECHERCHE ET DEFORMATION AVANCEE EN CALCUL SCIENTIFIQUE · TOULOUSE CEDEXCoordinatorFrance
Links
Data: CORDIS, © European Union