The effect of baffles on self-excited azimuthal modes in an annular combustor

被引:33
作者
Dawson, James R. [1 ]
Worth, Nicholas A. [2 ]
机构
[1] Norwegian Univ Sci & Technol, Dept Energy & Proc Engn, N-7491 Trondheim, Norway
[2] Univ Cambridge, Dept Engn, Cambridge CB2 1PZ, England
基金
英国工程与自然科学研究理事会;
关键词
Gas turbines; Azimuthal modes; Combustion instabilities; Baffles; Damping; PRECESSING VORTEX CORE; LARGE-EDDY SIMULATION; INSTABILITIES; OSCILLATIONS; FIELD;
D O I
10.1016/j.proci.2014.07.011
中图分类号
O414.1 [热力学];
学科分类号
摘要
In this paper the effect of inserting baffles on the self-excited azimuthal modes and unsteady heat release rate in an annular combustor are investigated experimentally. Particular attention is given to their effect on the time-varying behaviour of azimuthal modes observed in recent experiments and Large Eddy Simulations (LES) in azimuthally symmetric annular chambers. This time-varying behaviour causes the azimuthal modes to switch back and forth between spinning and standing wave modes. With the addition of a single baffle, the azimuthal symmetry of the chamber was broken leading to a coupling between the clockwise (CW) and anticlockwise (ACW) azimuthal acoustic waves. This eliminated the time-varying behaviour and promoted standing wave modes. It was found that three or more baffles were required to achieve significant damping of the modes. Since almost perfect standing wave modes occurred with the addition of a single baffle, high-speed chemiluminescence measurements were obtained to characterise the unsteady heat release rate at the pressure node and anti-node. Previous studies have shown that maximum and minimum heat release rate is produced at the anti-nodes and nodes respectively. As found previously, peak fluctuations at the anti-nodes result from axisymmetric fluctuations in heat release rate caused by pressure fluctuations driving axial mass flow fluctuations at the burner inlet. However, at the pressure nodes, an anti-symmetric structure was observed producing negligible heat release rate via the mechanism of cancellation. This latter result suggests that transverse velocity fluctuations play an important mechanistic role in ensuring that negligible heat release rate is produced at the node. (C) 2014 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
引用
收藏
页码:3283 / 3290
页数:8
相关论文
共 20 条
[1]  
Bourgouin J.F., 2013, ASME C P
[2]  
Dawson J.R., 2014, COMBUST FLAME
[3]   Azimuthal instabilities in annular combustors: standing and spinning modes [J].
Ghirardo, Giulio ;
Juniper, Matthew P. .
PROCEEDINGS OF THE ROYAL SOCIETY A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES, 2013, 469 (2157)
[4]   Influence of Transversal Acoustic Excitation of the Burner Approach Flow on the Flame Structure [J].
Hauser, Martin ;
Lorenz, Manuel ;
Sattelmayer, Thomas .
JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2011, 133 (04)
[5]   Thermoacoustic stability chart for high-intensity gas turbine combustion systems [J].
Krebs, W ;
Bernd Prade, PF ;
Hoffmann, S .
COMBUSTION SCIENCE AND TECHNOLOGY, 2002, 174 (07) :99-128
[6]   Responses of V-flames placed in an HF transverse acoustic field from a velocity to pressure antinode [J].
Lespinasse, Florian ;
Baillot, Francoise ;
Boushaki, Toufik .
COMPTES RENDUS MECANIQUE, 2013, 341 (1-2) :110-120
[7]   Nonlinear interaction between a precessing vortex core and acoustic oscillations in a turbulent swirling flame [J].
Moeck, Jonas P. ;
Bourgouin, Jean-Francois ;
Durox, Daniel ;
Schuller, Thierry ;
Candel, Sebastien .
COMBUSTION AND FLAME, 2012, 159 (08) :2650-2668
[8]   On the dynamic nature of azimuthal thermoacoustic modes in annular gas turbine combustion chambers [J].
Noiray, Nicolas ;
Schuermans, Bruno .
PROCEEDINGS OF THE ROYAL SOCIETY A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES, 2013, 469 (2151)
[9]   Investigation of azimuthal staging concepts in annular gas turbines [J].
Noiray, Nicolas ;
Bothien, Mirko ;
Schuermans, Bruno .
COMBUSTION THEORY AND MODELLING, 2011, 15 (05) :585-606
[10]   Disturbance Field Characteristics of a Transversely Excited Burner [J].
O'Connor, Jacqueline ;
Lieuwen, Tim .
COMBUSTION SCIENCE AND TECHNOLOGY, 2011, 183 (05) :427-443