Please wait a minute...
 首页  期刊介绍 期刊订阅 联系我们 横山亮次奖 百年刊庆
 
最新录用  |  预出版  |  当期目录  |  过刊浏览  |  阅读排行  |  下载排行  |  引用排行  |  横山亮次奖  |  百年刊庆
清华大学学报(自然科学版)  2023, Vol. 63 Issue (4): 487-504    DOI: 10.16511/j.cnki.qhdxxb.2023.25.024
  综述 本期目录 | 过刊浏览 | 高级检索 |
燃烧振荡声学抑制器的机理分析与设计优化
余志健1, 杨倩雯1, 王译晨1, 杨东2, 朱民1
1. 清华大学 能源与动力工程系, 北京 100084;
2. 南方科技大学 力学与航空航天工程系, 深圳 518055
Mechanism and design optimization of acoustic dampers for attenuating combustion instabilities
YU Zhijian1, YANG Qianwen1, WANG Yichen1, YANG Dong2, ZHU Min1
1. Department of Energy and Power Engineering, Tsinghua University, Beijing 100084, China;
2. Department of Mechanics and Aerospace Engineering, Southern University of Science and Technology, Shenzhen 518055, China
全文: PDF(15864 KB)   HTML
输出: BibTeX | EndNote (RIS)      
摘要 燃烧振荡是发展低排放燃气轮机燃烧室需要解决的关键问题之一,未来燃气轮机燃烧室运行温度更高、具有更宽的工况运行范围及更复杂的几何结构(如轴向分级、环形燃烧室等),燃烧振荡存在高振幅、多振荡频率、多振荡频率时变和多热声模态共存等特点。采用声学抑制器被动控制燃烧振荡具有抑制器结构简单、可靠性高、成本较低等优势。针对未来的燃烧室,现有抑制器方案将面临很大挑战,因此,亟需开展宽吸声带宽、可控制多模态的声学抑制器及系统级燃烧室多声学抑制器设计优化研究。该文概述了国内外声学抑制器机理和设计优化的研究进展,着重总结了作者近年来在常规及多频段声学抑制器机理、抑制效果分析计算和复杂热声系统参数对声学抑制器特性影响,以及基于伴随方法的多声学抑制器多参数快速优化等方面的研究工作,并对未来燃烧室声学抑制器的发展方向进行了讨论。
服务
把本文推荐给朋友
加入引用管理器
E-mail Alert
RSS
作者相关文章
余志健
杨倩雯
王译晨
杨东
朱民
关键词 热声振荡声学抑制器阻抗模型声涡耦合低阶网络模型伴随优化    
Abstract:[Significance] Combustion instability is a crucial issue in developing low-emission gas turbine combustors. Meanwhile, future combustors will possess higher temperatures, wider operation parameter ranges, and more complicated geometric structures (e.g., axially staged and annular). Thus, combustion instabilities have the features of high amplitude levels, multiple and time-varying frequencies, and the coexistence of several modes. Passive control employing acoustic dampers for attenuating oscillations has many advantages, such as simple structures, high reliabilities, and low costs. However, the present damper designs encounter great challenges for future combustors. Therefore, multimode wide-absorption acoustic dampers and systematic design optimization methods for multiple dampers must be investigated. [Progress] This paper briefly reviewed the research progress of mechanisms and optimization methods for acoustic dampers and the recent corresponding work conducted by the authors. First, the mechanisms for conventional and multi-bandwidth acoustic dampers were analyzed. Previous acoustic models for holes assumed that the thickness is ignorable and two open ends are inserted into semi-infinite space. A novel semianalytic acoustic model for short holes was proposed to consider sound-vortex interactions in detail. Sound generation and absorption can be well predicted by this model. Additionally, the performance of holes was sensitive to the shape of the hole edges. To broaden the absorption bandwidth of the Helmholtz resonators, parallel perforated materials were installed at the neck of the resonators. A theoretical model was derived to calculate the sound absorption coefficient of this type of resonator and effectively captured the nonlinear effect at the neck. Traditional resonators only possess a single frequency band for suppressing instabilities. Two multi-bandwidth resonators based on elastic membranes and multiple cavities were proposed by the authors. The results showed that elastic membranes and multiple cavities may introduce new frequency bands. Meanwhile, a low-order network model coupled with nonlinear flame dynamics and the acoustic models of resonators was developed to successfully predict thermoacoustic instabilities in cylindrical and annular combustors. The stability of annular combustors could be affected by the asymmetrical flame responses after introducing acoustic resonators. Subsequently, we examined the effects of complex thermoacoustic parameters on the acoustic characteristics of resonators and optimization strategies for designing multiple resonators. A theoretical model combined with the energy equation was established to explore the effect of a temperature difference on resonator performances. The results showed that the entropy disturbance caused by large temperature differences could affect the thermoacoustic stabilities of combustors. The cross-section of resonators was another critical factor in influencing the resonator properties. The acoustic characteristics of perforated liners with variable cross sections were theoretically and experimentally explored. Decreasing the cross-section increased the range of absorption frequency bands. The introduction of resonators for suppressing thermoacoustic instabilities changes the acoustic modes of combustors and the intrinsic modes of flames. An available strategy considering these influences was determined for reasonably designing the resonators. There are many adjustable parameters when multiple resonators are employed simultaneously. An efficient multiparameter adjoint-based optimization strategy for multiple resonators was developed. This algorithm is based on treating the low-order network model by performing the adjoint method. [Conclusions and Prospects] The next generation of multimode wide-absorption acoustic resonators urgently needs to be explored. Moreover, the effects and mechanisms of nonlinearity, mean flow, temperature difference, and other complex physical parameters on the properties of acoustic resonators need to be further explored. Meanwhile, the effectiveness and robustness of current optimization strategies for designing multiple resonators must be improved.
Key wordsthermoacoustic instability    acoustic damper    impedance model    sound-vortex interaction    low-order network model    adjoint-based optimization
收稿日期: 2022-10-30      出版日期: 2023-04-22
基金资助:国家重大科技专项(J2019-III-0020-0064);国家自然科学基金项目(52106159)
通讯作者: 杨东,副教授,E-mail:yangd3@sustech.edu.cn     E-mail: yangd3@sustech.edu.cn
作者简介: 余志健(1993-),男,博士后。
引用本文:   
余志健, 杨倩雯, 王译晨, 杨东, 朱民. 燃烧振荡声学抑制器的机理分析与设计优化[J]. 清华大学学报(自然科学版), 2023, 63(4): 487-504.
YU Zhijian, YANG Qianwen, WANG Yichen, YANG Dong, ZHU Min. Mechanism and design optimization of acoustic dampers for attenuating combustion instabilities. Journal of Tsinghua University(Science and Technology), 2023, 63(4): 487-504.
链接本文:  
http://jst.tsinghuajournals.com/CN/10.16511/j.cnki.qhdxxb.2023.25.024  或          http://jst.tsinghuajournals.com/CN/Y2023/V63/I4/487
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
  
[1] CANDEL S. Combustion dynamics and control progress and challenges[J]. Proceedings of the Combustion Institute, 2002, 29(1):1-28.
[2] LIEUWEN T C, YANG V. Combustion instabilities in gas turbine engines:Operational experience, fundamental mechanisms, and modeling[M]. Reston:American Institute of Aeronautics and Astronautics, 2005.
[3] NOBLE D, WU D, EMERSON B, et al. Assessment of current capabilities and near-term availability of hydrogen-fired gas turbines considering a low-carbon future[J]. Journal of Engineering for Gas Turbines and Power, 2021, 143(4):041002.
[4] RAYLEIGH J W S, LINDSAY R B. The theory of sound[M]. 2nd ed. New York:Dover Publications, 1945.
[5] DOWLING A P, FFOWCS WILLIAMS J E. Sound and sources of sound[M]. Chichester:Ellis Horwood, 1983.
[6] NAGARAJA S B, GRAHAM O, KIM K, et al. Acoustic damper for gas turbine engine combustors:20180313540[P]. 2018-11-01.
[7] WASIF S P, JOHNSON C E. Acoustic resonator with impingement cooling tubes:7413053[P]. 2008-08-19.
[8] TANIMURA S, NOSE M, ISHIZAKA K, et al. Advanced dry low NOx combustor for Mitsubishi G class gas turbines[C]//Proceedings of ASME Turbo Expo 2008:Power for Land, Sea, and Air. Berlin, Germany:ASME, 2008:GT2008-50819.
[9] BELLUCCI V, FLOHR P, PASCHEREIT C O, et al. On the use of Helmholtz resonators for damping acoustic pulsations in industrial gas turbines[J]. Journal of Engineering for Gas Turbines and Power, 2004, 126(2):271-275.
[10] BOTHIEN M R, PENNELL D A, ZAJADATZ M, et al. On key features of the AEV burner engine implementation for operational flexibility[C]//Proceedings of ASME Turbo Expo 2013:Turbine Technical Conference and Exposition. San Antonio, USA:ASME, 2013:GT2013-95693.
[11] ZAHIROVIC S, KNAPP K. Ansaldo GT26 sequential combustor performance in long-term commercial operation[C]//Proceedings of ASME Turbo Expo 2017:Turbomachinery Technical Conference and Exposition. Charlotte, USA:ASME, 2017:GT2017-64289.
[12] SCHUERMANS B, BOTHIEN M, MAURER M, et al. Combined acoustic damping-cooling system for operational flexibility of GT26/GT24 reheat combustors[C]//Proceedings of ASME Turbo Expo 2015:Turbine Technical Conference and Exposition. Montreal, Canada:ASME, 2015:GT2015-42287.
[13] CERUTTI M, GIANNINI N, SCHUERMANS B, et al. Combustion instabilities damping system development for dry low NOx emissions operability enhancement of a heavy-duty gas turbine[C]//Proceedings of ASME Turbo Expo 2019:Turbomachinery Technical Conference and Exposition. Phoenix, USA:ASME, 2019:GT2019-91246.
[14] POINSOT T. Prediction and control of combustion instabilities in real engines[J]. Proceedings of the Combustion Institute, 2017, 36(1):1-28.
[15] KARIM H, NATARAJAN J, NARRA V, et al. Staged combustion system for improved emissions operability and flexibility for 7HA class heavy duty gas turbine engine[C]//Proceedings of the ASME Turbo Expo 2017:Turbomachinery Technical Conference and Exposition. Charlotte, USA:ASME, 2017:GT2017-63998.
[16] BAUERHEIM M, NICOUD F, POINSOT T. Progress in analytical methods to predict and control azimuthal combustion instability modes in annular chambers[J]. Physics of Fluids, 2016, 28(2):021303.
[17] HOWE M. On the theory of unsteady high Reynolds number flow through a circular aperture[J]. Proceedings of the Royal Society A Mathematical, Physical and Engineering Sciences, 1979, 366(1725):205-223.
[18] JING X D, SUN X F. Experimental investigations of perforated liners with bias flow[J]. The Journal of the Acoustical Society of America, 1999, 106(5):2436-2441.
[19] SU J, RUPP J, GARMORY A, et al. Measurements and computational fluid dynamics predictions of the acoustic impedance of orifices[J]. Journal of Sound and Vibration, 2015, 352:174-191.
[20] YANG D, MORGANS A S. A semi-analytical model for the acoustic impedance of finite length circular holes with mean flow[J]. Journal of Sound and Vibration, 2016, 384:294-311.
[21] YANG D, MORGANS A S. The acoustics of short circular holes opening to confined and unconfined spaces[J]. Journal of Sound and Vibration, 2017, 393:41-61.
[22] GUZMÁN-IÑIGO J, YANG D, JOHNSON H G, et al. Sensitivity of the acoustics of short circular holes with bias flow to inlet edge geometries[J]. AIAA Journal, 2019, 57(11):4835-4844.
[23] YANG D, WANG X L, ZHU M. The impact of the neck material on the sound absorption performance of Helmholtz resonators[J]. Journal of Sound and Vibration, 2014, 333(25):6843-6857.
[24] 杨东.通过颈部材料优化亥姆霍兹共振器的理论和实验研究[D].北京:清华大学, 2013. YANG D. Theoretical and experimental study of Helmholtz resonator optimization with neck materials[D]. Beijing:Tsinghua University, 2013.(in Chinese)
[25] 高原.亥姆霍兹共振器吸声特性改进方法研究[D].北京:清华大学, 2011. GAO Y. An improvement on the sound absorption performance of Helmholtz resonators[D]. Beijing:Tsinghua University, 2011.(in Chinese)
[26] CHEN H J, ZENG H C, DING C L, et al. Double-negative acoustic metamaterial based on hollow steel tube meta-atom[J]. Journal of Applied Physics, 2013, 113(10):104902.
[27] BRAVO T, MAURY C, PINHEDE C. Enhancing sound absorption and transmission through flexible multi-layer micro-perforated structures[J]. The Journal of the Acoustical Society of America, 2013, 134(5):3663-3673.
[28] TAKASUGI S, WATANABE K, MISAWA M, et al. Low-frequency sound absorbing metasurface using multilayer split resonators[J]. Japanese Journal of Applied Physics, 2021, 60(SD):SDDA01.
[29] BOTHIEN M R, NOIRAY N, SCHUERMANS B. A novel damping device for broadband attenuation of low-frequency combustion pulsations in gas turbines[J]. Journal of Engineering for Gas Turbines and Power, 2014, 136(4):041504.
[30] WANG S W, HAN F, MUELLER M A. Acoustic damping device for use in gas turbine engine:8469141[P]. 2013-06-25.
[31] GRIFFIN S, LANE S A, HUYBRECHTS S. Coupled Helmholtz resonators for acoustic attenuation[J]. Journal of Vibration and Acoustics, 2001, 123(1):11-17.
[32] NUDEHI S S, DUNCAN G S, FAROOQ U. Modeling and experimental investigation of a helmholtz resonator with a flexible plate[J]. Journal of Vibration and Acoustics, 2013, 135(4):041102.
[33] MUNJAL M L. Acoustics of ducts and mufflers[M]. 2nd ed. New Delhi:Wiley, 2014.
[34] YU Z J, YANG Y. Investigation of thermoacoustic oscillation attenuation by modified Helmholtz dampers with dual frequency bands[J]. Applied Acoustics, 2022, 185:108433.
[35] YU Z J, YANG Y. Impact of dual-volume Helmholtz dampers on longitudinal and azimuthal thermo-acoustic instabilities in an annular combustor[J]. Journal of Thermal Science, 2022, 31(6):2225-2243.
[36] 余志健,杨旸.亥姆霍兹共振器对热声不稳定极限环的预测[J].航空动力学报, 2021, 36(5):997-1006. YU Z J, YANG Y. Prediction of Helmholtz dampers on limit cycle of thermoacoustic instabilities[J]. Journal of Aerospace Power, 2021, 36(5):997-1006.(in Chinese)
[37] SELLE L, LARTIGUE G, POINSOT T, et al. Compressible large eddy simulation of turbulent combustion in complex geometry on unstructured meshes[J]. Combustion and Flame, 2004, 137(4):489-505.
[38] 王译晨,朱民.火焰动力学及其对热声稳定性的影响[J].清华大学学报(自然科学版), 2022, 62(4):785-793. WANG Y C, ZHU M. Flame dynamics and their effect on thermoacoustic instabilities[J]. Journal of Tsinghua University (Science and Technology), 2022, 62(4):785-793.(in Chinese)
[39] 翁方龙,周少伟,朱民.基于描述函数的燃烧振荡建模与仿真[J].推进技术, 2021, 42(10):2306-2314. WENG F L, ZHAO S W, ZHU M. Modeling and simulation of combustion oscillations based on describing function method[J]. Journal of Propulsion Technology, 2021, 42(10):2306-2314.(in Chinese)
[40] ZHU M, DOWLING A P, BRAY K N C. Integration of CFD and low-order models for combustion oscillations in aero-engines[C]//Proceedings, XV International Symposium on Air-breathing Engines. Bangalore, India:AIAA Isabe, 2001:ISABE-2001-1088.
[41] 李春炎,杨锐,尹洪,等.燃气轮机燃烧室变工况运行稳定性的建模与分析[J].工程热物理学报, 2016, 37(8):1808-1815. LI C Y, YANG R, YIN H, et al. Modelling and simulation of operation stability of gas turbine combustor under varying duty[J]. Journal of Engineering Thermophysics, 2016, 37(8):1808-1815.(in Chinese)
[42] 高原,朱民.亥姆霍兹共振器抑制振荡燃烧理论分析[J].工程热物理学报, 2009, 30(6):1048-1050. GAO Y, ZHU M. Theoretical analysis of combustion oscillation suppression with Helmholtz resonators[J]. Journal of Engineering Thermophysics, 2009, 30(6):1048-1050.(in Chinese)
[43] LI C Y, ZHU M, MOECK J P. An analytical study of the flame dynamics of a transversely forced asymmetric two-dimensional Bunsen flame[J]. Combustion Theory and Modelling, 2017, 21(5):976-995.
[44] LI C Y, YANG D, LI S H, et al. An analytical study of the effect of flame response to simultaneous axial and transverse perturbations on azimuthal thermoacoustic modes in annular combustors[J]. Proceedings of the Combustion Institute, 2019, 37(4):5279-5287.
[45] LEFEBVRE A H, BALLA D R. Gas turbine combustion:Alternative fuels and emissions:3rd ed[M]. Boca Raton:CRC Press, 2010.
[46] MAHESH K. The interaction of jets with crossflow[J]. Annual Review of Fluid Mechanics, 2013, 45:379-407.
[47] WEILENMANN M, XIONG Y, NOIRAY N. On the dispersion of entropy waves in turbulent flows[J]. Journal of Fluid Mechanics, 2020, 903:R1.
[48] YANG D, MORGANS A S. Acoustic models for cooled Helmholtz resonators[J]. AIAA Journal, 2017, 55(9):3120-3127.
[49] LESSHAFFT L. Nonlinear global modes and sound generation in hot jets[D]. Palaiseau:Ecole Polytechnique, 2006.
[50] LIVESCU D. Turbulence with large thermal and compositional density variations[J]. Annual Review of Fluid Mechanics, 2020, 52:309-341.
[51] 甘振鹏,杨东.带冷却气流的亥姆霍兹共振器的声类比模型[J].力学学报, 2022, 54(3):577-587. GAN Z P, YANG D. An acoustic analogy model for Helmholtz resonators with cooling bias flow[J]. Chinese Journal of Theoretical and Applied Mechanics, 2022, 54(3):577-587.(in Chinese)
[52] YANG D, GUZMÁN-IÑIGO J, MORGANS A S. Sound generation by entropy perturbations passing through a sudden flow expansion[J]. Journal of Fluid Mechanics, 2020, 905:R2.
[53] YANG D, GUZMÁN-IÑIGO J, MORGANS A S. Sound generated by axisymmetric non-plane entropy waves passing through flow contractions[J]. International Journal of Aeroacoustics, 2022, 21(5-7):521-536.
[54] 许子诺.变截面管道声衬吸声机理的分析与实验研究[D].北京:清华大学, 2021. XU Z N. Acoustic liner sound absorption mechanism analysis and experiment in non-uniform duct application[D]. Beijing:Tsinghua University, 2021.(in Chinese)
[55] BOURQUARD C, NOIRAY N. Stabilization of acoustic modes using Helmholtz and quarter-wave resonators tuned at exceptional points[J]. Journal of Sound and Vibration, 2019, 445:288-307.
[56] CAZZOLATO B S, HOWARD C Q, HANSEN C H. Finite element analysis of an industrial reactive silencer[C]//The Fifth International Congress of Sound and Vibration, Australia. Adelaide, Australia:IIAV, 1997:1659-1667.
[57] WANG X, MAK C M. Wave propagation in a duct with a periodic Helmholtz resonators array[J]. The Journal of the Acoustical Society of America, 2012, 131(2):1172-1182.
[58] BETZ M, ZAHN M, HIRSCH C, et al. Impact of damper placement on the stability margin of an annular combustor test rig[C]//Proceedings of ASME Turbo Expo 2019:Turbomachinery Technical Conference and Exposition. Phoenix, USA:ASME, 2019:GT2019-90238.
[59] MAZUR M, NYGÅRD H T, DAWSON J, et al. Experimental study of damper position on instabilities in an annular combustor[C]//Proceedings of ASME Turbo Expo 2018:Turbomachinery Technical Conference and Exposition. Oslo, Norway:ASME, 2018:GT2018-75070.
[60] DAWSON J R, WORTH N A. The effect of baffles on self-excited azimuthal modes in an annular combustor[J]. Proceedings of the Combustion Institute, 2015, 35(3):3283-3290.
[61] 王译晨,杨东,李苏辉,等.非对称性对环形燃烧室与集气室热声耦合影响的研究[C/OL].中国力学学会.(2020-12-03)[2022-10-15]. DOI:10.26914/c.cnkihy.2020.035569. WANG Y C, YANG D, LI S H, et al. Effect ofasymmetry onthermoGacousticcoupling ofthe combustion chamber and plenumin an annular combustor[C/OL]. The Chinese Society of Theoretical and Applied Mechanics.(2020-12-03)[2022-10-15]. DOI:10.26914/c.cnkihy.2020.035569.(in Chinese)
[62] MENSAH G A, MAGRI L, SILVA C F, et al. Exceptional points in the thermoacoustic spectrum[J]. Journal of Sound and Vibration, 2018, 433:124-128.
[63] DOKUMACI E. Duct acoustics:Fundamentals and applications to mufflers and silencers[M]. Cambridge:Cambridge University Press, 2021.
[64] JUNIPER M P, SUJITH R I. Sensitivity and nonlinearity of thermoacoustic oscillations[J]. Annual Review of Fluid Mechanics, 2018, 50:661-689.
[65] MAGRI L. Adjoint methods as design tools in thermoacoustics[J]. Applied Mechanics Reviews, 2019, 71(2):020801.
[66] YANG D, SOGARO F M, MORGANS A S, et al. Optimising the acoustic damping of multiple Helmholtz resonators attached to a thin annular duct[J]. Journal of Sound and Vibration, 2019, 444:69-84.
[1] 戚俊毅, 方儒卿, 吴勇民, 汤卫平, 李哲. 全固态薄膜锂电池倍率性能[J]. 清华大学学报(自然科学版), 2023, 63(9): 1440-1451.
[2] 王译晨, 朱民. 火焰动力学及其对热声稳定性的影响[J]. 清华大学学报(自然科学版), 2022, 62(4): 785-793.
[3] 刘威, 谢小荣, 姜齐荣, 毛航银. 变流式新能源机组的次/超同步振荡、小扰动同步稳定性与阻抗模型分析[J]. 清华大学学报(自然科学版), 2022, 62(10): 1706-1714.
Viewed
Full text


Abstract

Cited

  Shared   
  Discussed   
版权所有 © 《清华大学学报(自然科学版)》编辑部
本系统由北京玛格泰克科技发展有限公司设计开发 技术支持:support@magtech.com.cn