Prediction of pressure oscillations in a premixed swirl combustor flow and comparison to measurements

被引:12
|
作者
Habisreuther, P. [1 ]
Bender, C. [1 ]
Petsch, O. [1 ]
Buecher, H. [1 ]
Bockhorn, H. [1 ]
机构
[1] Univ Karlsruhe, Engler Bunte Inst, Div Combust Technol, D-76128 Karlsruhe, Germany
关键词
swirl combustion; combustion noise; LDV-measurement; microphone measurement; LES-simulation;
D O I
10.1007/s10494-006-9041-7
中图分类号
O414.1 [热力学];
学科分类号
摘要
The most common and reliable technique used for flame stabilization of industrial combustors with high thermal loads is the application of strongly swirling flows. In addition to stabilization, swirl flames offer the possibility to influence emission characteristics by simply changing the swirl intensity or the type of swirl generation. Despite of these major advantages, swirling flows tend to evolve flow instabilities, that considerably constitute a significant source of noise. In general, noise generation is substantially enhanced, when such a swirling flow is employed for flames. Thus, the minimization of the resulting noise emissions under conservation of the benefit of high ignition stability is one major design challenge for the development of modern swirl stabilized combustion devices. The present investigation makes an attempt to determine mechanisms and processes to influence the noise generation of flames with underlying swirling flows. Therefore, a new burner has been designed, that offers the possibility to vary geometrical parameters as well as the type of swirl generation, typically applied in industrial devices. Experimental data has been acquired for the isothermal flow as well as swirl flames by means of 3-D-LDV-diagnostics comprising the components of long-time averaged mean and rms-velocities as well as spectrally resolved velocity fluctuations for all components. The noise emission data was acquired with microphone probes resulting in sound pressure levels outside the zone of the perceptible fluid flow. Along to the experiments, numerical simulations using RANS and LES have been carried out for isothermal cases with different burner outlet geometries. The results of the measurements show a distinct rise of the sound pressure level, obtained by changing both the test setup from the isothermal into the flame configuration as well as the geometrical parameters. This is also resembled by the LES simulation results. Furthermore, a physical model has been developed from experiments and verified by the LES simulation, that explains the formation of coherent flow structures and allows to separate their contribution to the overall noise emission from ordinary turbulent noise sources.
引用
收藏
页码:147 / 160
页数:14
相关论文
共 50 条
  • [1] Prediction of Pressure Oscillations in a Premixed Swirl Combustor Flow and Comparison to Measurements
    P. Habisreuther
    C. Bender
    O. Petsch
    H. Büchner
    H. Bockhorn
    [J]. Flow, Turbulence and Combustion, 2006, 77 : 147 - 160
  • [2] Prediction of pressure oscillations in a premixed swirl combustor flow and comparison to measurements
    Habisreuther, P
    Bender, C
    Petsch, O
    Büchner, H
    Bockhorn, H
    [J]. ENGINEERING TURBULENCE MODELLING AND EXPERIMENTS 6, 2005, : 855 - 864
  • [3] EFFECT OF FLOW PULSATIONS IN PREMIXED, SWIRL STABILIZED COMBUSTOR
    Sharma, Aayush K.
    Sen, Uddalok
    Mahapatra, Pallab Sinha
    Sen, Swarnendu
    Mukhopadhyay, Achintya
    [J]. PROCEEDINGS OF THE ASME GAS TURBINE INDIA CONFERENCE, 2014, 2014,
  • [4] FLOW MEASUREMENTS IN A MODEL SWIRL COMBUSTOR
    VU, BT
    GOULDIN, FC
    [J]. AIAA JOURNAL, 1982, 20 (05) : 642 - 651
  • [5] Statistical characteristics of pressure oscillations in a premixed combustor
    Lieuwen, TC
    [J]. JOURNAL OF SOUND AND VIBRATION, 2003, 260 (01) : 3 - 17
  • [6] Flow Field and Wall Temperature Measurements for Reacting Flow in a Lean Premixed Swirl Stabilized Can Combustor
    Park, Suhyeon
    Gomez-Ramirez, David
    Gadiraju, Siddhartha
    Kedukodi, Sandeep
    Ekkad, Srinath V.
    Moon, Hee-Koo
    Kim, Yong
    Srinivasan, Ram
    [J]. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2018, 140 (09):
  • [7] Effects of Swirl Number and Central Rod on Flow in a Lean Premixed Swirl Combustor
    Yellugari, Kranthi
    Gomez, Rodrigo Villalva
    Gutmark, Ephraim
    [J]. COMBUSTION SCIENCE AND TECHNOLOGY, 2023,
  • [8] CHARACTERISTICS OF AN ULTRA-LEAN SWIRL COMBUSTOR FLOW BY LES AND COMPARISON TO MEASUREMENTS
    Kern, Matthias
    Marinov, Svetoslav
    Habisreuther, Peter
    Zarzalis, Nikolaos
    Peschiulli, Antonio
    Turrini, Fabio
    [J]. PROCEEDINGS OF THE ASME TURBO EXPO 2011, VOL 2, PTS A AND B, 2011, : 321 - 330
  • [9] Intermittent Pressure Oscillations in a Cylindrical Combustor With a Swirl Coaxial Injector
    Yang, Shangrong
    Wang, Yong
    Zhang, Feng
    Yang, Baoe
    Wang, Muxin
    [J]. Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics, 2022, 43 (07): : 1986 - 1991
  • [10] Swirl flow structure and flame characteristics in a model lean premixed combustor
    Anacleto, PM
    Fernandes, EC
    Heitor, MV
    Shtork, SI
    [J]. COMBUSTION SCIENCE AND TECHNOLOGY, 2003, 175 (08) : 1369 - 1388