Impact of Heat Release Distribution on the Spinning Modes of an Annular Combustor With Multiple Matrix Burners

Author:

Laera Davide1,Prieur Kevin2,Durox Daniel3,Schuller Thierry3,Camporeale Sergio M.4,Candel Sébastien3

Affiliation:

1. DMMM, Sez. Macchine ed Energetica, Politecnico di Bari, Via Re David 200, Bari 70125, Italy e-mail:

2. Laboratoire EM2C, CNRS, CentraleSupélec, Université Paris-Saclay, Grande Voie des Vignes, Chatenay-Malabry cedex 92295, France; Safran Tech, E&P, Châteaufort, CS 80112, Magny-Les-Hameaux 78772, France

3. Laboratoire EM2C, CNRS, CentraleSupélec, Université Paris-Saclay, Grande Voie des Vignes, Chatenay-Malabry cedex 92295, France

4. DMMM, Sez. Macchine ed Energetica, Politecnico di Bari, Via Re David 200, Bari 70125, Italy

Abstract

The present article reports a numerical analysis of instability coupled by a spinning mode in an annular combustor. This corresponds to experiments carried out on the MICCA test facility equipped with 16 matrix burners. Each burner response is represented by means of a global experimental flame describing function (FDF). A harmonic balance nonlinear stability analysis is carried out by combining the FDF with a Helmholtz solver to determine the system dynamics trajectories in a frequency-growth rate plane. The influence of the distribution of the volumetric heat release corresponding to each burner is investigated in a first stage. Even though each of the 16 burners is compact with respect to the transverse mode wavelength, and the 16 flames occupy the same volume, this distribution of heat release is not compact in the azimuthal direction and simulations reveal an influence of this volumetric distribution on frequencies and growth rates. This study emphasizes the importance of providing a suitable description of the flame zone geometrical extension and correspondingly an adequate representation of the level of heat release rate fluctuation per unit volume. It is found that these two items can be deduced from a knowledge of the heat release distribution under steady-state operating conditions. Once the distribution of the heat release fluctuations is unequivocally defined, limit cycle simulations are performed. For the conditions explored, simulations retrieve the spinning nature of the self-sustained mode that was identified in the experiments both in the plenum and in the combustion chamber.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference45 articles.

1. Combustion Instabilities Coupled by Pressure Waves and Their Active Control;Symp. Combust.,1992

2. A New Pattern of Instability Observed in an Annular Combustor: The Slanted Mode;Proc. Combust. Inst.,2015

3. A Hysteresis Phenomenon Leading to Spinning or Standing Azimuthal Instabilities in an Annular Combustor;Combust. Flame

4. Durox, D., Bourgouin, J., Moeck, J., Philip, M., Schuller, T., and Candel, S., 2013, “Nonlinear Interactions in Combustion Instabilities Coupled by Azimuthal Acoustic Modes,” International Workshop on Non-Normal and Nonlinear Effects in Aero-and Thermo-Acoustics, Munich, Germany, June 18–21, pp. 18–21.https://mediatum.ub.tum.de/doc/1253524/1253524.pdf

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