Volume 42 Issue 1
Jan.  2027
Turn off MathJax
Article Contents
Tang Jiayuan, Du Jingtao, Bai Yang, et al. Analysis of thermoacoustic instability characteristics in combustion chambers under variable operating conditions[J]. Journal of Aerospace Power, 2026, 42(X):20250277 doi: 10.13224/j.cnki.jasp.20250277
Citation: Tang Jiayuan, Du Jingtao, Bai Yang, et al. Analysis of thermoacoustic instability characteristics in combustion chambers under variable operating conditions[J]. Journal of Aerospace Power, 2026, 42(X):20250277 doi: 10.13224/j.cnki.jasp.20250277

Analysis of thermoacoustic instability characteristics in combustion chambers under variable operating conditions

doi: 10.13224/j.cnki.jasp.20250277
  • Received Date: 2025-06-10
    Available Online: 2026-10-07
  • To investigate thermoacoustic instability in combustors under variable operating conditions, this study employs an integrated approach combining gas path modeling with acoustic low-order network modeling to characterize thermoacoustic mode variations. A full-engine gas path model and combustor low-order network model were developed, where real-time gas path parameters were input through dual pathways (flame dynamics and flow field perturbations) to assess their modal effects. Results demonstrate significant sensitivity of modes to equivalence ratio and combustor inlet temperature, while pressure and mass flow effects were comparatively weaker. Except for equivalence ratio variations, flow field pathway contributions to modal shifts were less pronounced than flame pathway effects. Comprehensive thermoacoustic analysis requires concurrent consideration of real-time flow field and flame parameter updates to evaluate the flame-acoustic coupling mechanism described by Rayleigh's criterion. The prediction model was validated through combustion noise measurements under off-design conditions, establishing a framework to extend thermoacoustic research from combustor design to predictive instability control in variable operational regimes.

     

  • loading
  • [1]
    Dowling A P, Stow S R. Acoustic analysis of gas turbine combustors[J]. Journal of Propulsion and Power, 2003, 19(5): 751-764. doi: 10.2514/2.6192
    [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, 2006.
    [3]
    杨甫江, 郭志辉, 曾宇晖. 贫燃预混旋流火焰热声特性研究[J]. 航空动力学报, 2014, 29(12): 2854-2861. Yang Fujiang, Guo Zhihui, Zeng Yuhui. Study on thermoacoustic characteristic of lean premixed swirling flames[J]. Journal of Aerospace Power, 2014, 29(12): 2854-2861. (in Chinese doi: 10.13224/j.cnki.jasp.2014.12.010

    Yang Fujiang, Guo Zhihui, Zeng Yuhui. Study on thermoacoustic characteristic of lean premixed swirling flames[J]. Journal of Aerospace Power, 2014, 29(12): 2854-2861. (in Chinese) doi: 10.13224/j.cnki.jasp.2014.12.010
    [4]
    Dowling A P, Mahmoudi Y. Combustion noise[J]. Proceedings of the Combustion Institute, 2015, 35(1): 65-100. doi: 10.1016/j.proci.2014.08.016
    [5]
    Marble F E, Candel S M. Acoustic disturbance from gas non-uniformities convected through a nozzle[J]. Journal of Sound and Vibration, 1977, 55(2): 225-243. doi: 10.1016/0022-460X(77)90596-X
    [6]
    Bake F, Richter C, Mühlbauer B, et al. The Entropy Wave Generator (EWG): a reference case on entropy noise[J]. Journal of Sound and Vibration, 2009, 326(3/4/5): 574-598. doi: 10.1016/j.jsv.2009.05.018
    [7]
    Hoeijmakers M, Kornilov V, Lopez Arteaga I, et al. Intrinsic instability of flame–acoustic coupling[J]. Combustion and Flame, 20140, 161(11): 2860-2867. doi: 10.1016/j.combustflame.2014.05.009
    [8]
    Hoeijmakers M, Kornilov V, Arteaga I L, et al. Flame dominated thermoacoustic instabilities in a system with high acoustic losses[J]. Combustion and Flame, 2016, 169: 209-215. doi: 10.1016/j.combustflame.2016.03.009
    [9]
    Wolf P, Staffelbach G, Gicquel L Y M, et al. Acoustic and Large Eddy Simulation studies of azimuthal modes in annular combustion chambers[J]. Combustion and Flame, 2012, 159(11): 3398-3413. doi: 10.1016/j.combustflame.2012.06.016
    [10]
    Silva C F. Intrinsic thermoacoustic instabilities[J]. Progress in Energy and Combustion Science, 2023, 95: 101065. doi: 10.1016/j.pecs.2022.101065
    [11]
    Li Jingxuan, Morgans A S. Time domain simulations of nonlinear thermoacoustic behaviour in a simple combustor using a wave-based approach[J]. Journal of Sound and Vibration, 2015, 346: 345-360. doi: 10.1016/j.jsv.2015.01.032
    [12]
    Yang Dong, Laera D, Morgans A S. A systematic study of nonlinear coupling of thermoacoustic modes in annular combustors[J]. Journal of Sound and Vibration, 2019, 456: 137-161. doi: 10.1016/j.jsv.2019.04.025
    [13]
    Hobson D E, Fackrell J E, Hewitt G. Combustion instabilities in industrial gas turbines: measurements on operating plant and thermoacoustic modeling[J]. Journal of Engineering for Gas Turbines and Power, 2000, 122(3): 420-428. doi: 10.1115/1.1287238
    [14]
    闫斌斌. 基于气路性能混合模型的燃气轮机叶片故障预警及诊断方法研究[D]. 北京: 北京化工大学, 2021. Yan Binbin. Research on early warning and diagnosis method of gas turbine blade fault based on gas path performance hybrid model[D]. Beijing: Beijing University of Chemical Technology, 2021. (in Chinese

    Yan Binbin. Research on early warning and diagnosis method of gas turbine blade fault based on gas path performance hybrid model[D]. Beijing: Beijing University of Chemical Technology, 2021. (in Chinese)
    [15]
    王涛. 变几何三轴式燃气轮机总体性能及控制规律研究[D]. 北京: 中国科学院大学, 2019. Wang Tao. Characteristic and control law investigations on variable geometry triaxial gas turbine[D]. Beijing: University of Chinese Academy of Sciences, 2019. (in Chinese

    Wang Tao. Characteristic and control law investigations on variable geometry triaxial gas turbine[D]. Beijing: University of Chinese Academy of Sciences, 2019. (in Chinese)
    [16]
    Stow S R, Dowling A P. A time-domain network model for nonlinear thermoacoustic oscillations[J]. Journal of Engineering for Gas Turbines and Power, 2009, 131(3): 031502. doi: 10.1115/1.2981178
    [17]
    Liu Yang, Du Jingtao, Cheng Li. Thermoacoustic modal instability and its suppression with locally resonant flexible membranes[J]. Combustion and Flame, 2022, 237: 111859. doi: 10.1016/j.combustflame.2021.111859
    [18]
    Guo Fanhao, Du Jingtao, Liu Yang. Dynamic behavior modeling and energy conversion characteristic analysis of a thermoacoustic-piezoelectric generator with the consideration of thermal and viscous losses[J]. Journal of Sound and Vibration, 2024, 577: 118338. doi: 10.1016/j.jsv.2024.118338
    [19]
    张澄宇, 李磊, 孙晓峰. 加力燃烧室热声振荡纵向传播特性及控制[J]. 航空动力学报, 2010, 25(2): 278-283. Zhang Chengyu, Li Lei, Sun Xiaofeng. Thermoacoustic oscillating calculation of longitudinal equivalence frequency and stability in aero-engine afterburner[J]. Journal of Aerospace Power, 2010, 25(2): 278-283. (in Chinese doi: 10.13224/j.cnki.jasp.2010.02.001

    Zhang Chengyu, Li Lei, Sun Xiaofeng. Thermoacoustic oscillating calculation of longitudinal equivalence frequency and stability in aero-engine afterburner[J]. Journal of Aerospace Power, 2010, 25(2): 278-283. (in Chinese) doi: 10.13224/j.cnki.jasp.2010.02.001
    [20]
    Schuermans B. Modeling and control of thermoacoustic instabilities[D]. Lausanne: EPFL, 2003.
    [21]
    Hoeijmakers P G M. Flame-acoustic coupling in combustion instabilities[D]. Eindhoven: Technische Universiteit Eindhoven, 2014.
    [22]
    Tay Wo Chong L, Komarek T, Kaess R, et al. Identification of flame transfer functions from LES of a premixed swirl burner[C]// ASME Turbo Expo 2010: Power for Land, Sea, and Air. Glasgow, UK: ASMEDC , 2010: 623-635.
    [23]
    Polifke W. Modeling and analysis of premixed flame dynamics by means of distributed time delays[J]. Progress in Energy and Combustion Science, 2020, 79: 100845. doi: 10.1016/j.pecs.2020.100845
    [24]
    Schuermans B, Guethe F, Pennell D, et al. Thermoacoustic modeling of a gas turbine using transfer functions measured under full engine pressure[J]. Journal of Engineering for Gas Turbines and Power, 2010, 132(11): 111503. doi: 10.1115/1.4000854
    [25]
    Abbott D, Giannotta A, Sun X X, et al. Thermoacoustic behaviour of a hydrogen micromix aviation gas turbine combustor under typical flight conditions[C]// Turbo Expo: Power for Land, Sea, and Air. , New York: American Society of Mechanical Engineers, 2021: V006T03A013
    [26]
    Eder A, Fischer A, Lahiri C, et al. Identification of the dynamics of a turbulent spray flame at high pressure[R]. Zürich, Switzerland: Symposium on Thermoacoustics in Combustion: Industry Meets Academia (SoTiC 2023), 2023.
    [27]
    Mirat C, Durox D, Schuller T. Analysis of the spray and transfer function of swirling spray flames from a multi-jet steam assisted liquid fuel injector[C]// ASME Turbo Expo 2014: Turbine Technical Conference and Exposition, New York: American Society of Mechanical Engineers, 2014, : V04AT04A008.
    [28]
    Badhe A, Laera D, Gicquel L. High-fidelity Large Eddy Simulations of the Flame Transfer Function of a turbulent swirling spray flame[R]. Napoli, Italy: 10th European Combustion Meeting, 2021
    [29]
    杨晨, 刘勇, 张祥, 等. 基于实验数据的燃烧室火焰传递函数优化方法[J]. 航空动力学报, 2024, 39(2): 20220157. Yang Chen, Liu Yong, Zhang Xiang, et al. Optimization method on flame transfer function of combustor based on experimental data[J]. Journal of Aerospace Power, 2024, 39(2): 20220157. (in Chinese doi: 10.13224/j.cnki.jasp.20220157

    Yang Chen, Liu Yong, Zhang Xiang, et al. Optimization method on flame transfer function of combustor based on experimental data[J]. Journal of Aerospace Power, 2024, 39(2): 20220157. (in Chinese) doi: 10.13224/j.cnki.jasp.20220157
    [30]
    Wang Y, Rutland C J. Effects of temperature and equivalence ratio on the ignition of n-heptane fuel spray in turbulent flow[J]. Proceedings of the Combustion Institute, 2005, 30(1): 893-900. doi: 10.1016/j.proci.2004.08.074
    [31]
    王昆, 房爱兵, 邢双喜, 等. 基于火焰面波动机理的热释放模型理论推导及其模态分析[J]. 航空动力学报, 2016, 31(6): 1309-1317. Wang Kun, Fang Aibing, Xing Shuangxi, et al. Heat release model related to flame variation mechanism and modal analysis[J]. Journal of Aerospace Power, 2016, 31(6): 1309-1317. (in Chinese doi: 10.13224/j.cnki.jasp.2016.06.005

    Wang Kun, Fang Aibing, Xing Shuangxi, et al. Heat release model related to flame variation mechanism and modal analysis[J]. Journal of Aerospace Power, 2016, 31(6): 1309-1317. (in Chinese) doi: 10.13224/j.cnki.jasp.2016.06.005
    [32]
    Di Sabatino F, Guiberti T F, Moeck J P, et al. Fuel and equivalence ratio effects on transfer functions of premixed swirl flames[J]. Journal of Propulsion and Power, 2019, 36(2): 271-284. doi: 10.2514/1.b37537
    [33]
    Shreekrishna, Hemchandra S, Lieuwen T. Premixed flame response to equivalence ratio perturbations[J]. Combustion Theory and Modelling, 2010, 14(5): 681-714. doi: 10.1080/13647830.2010.502247
    [34]
    Xu Liangliang, Zheng Jianyi, Wang Guoqing, et al. Investigation on the intrinsic thermoacoustic instability of a lean-premixed swirl combustor with an acoustic liner[J]. Proceedings of the Combustion Institute, 2021, 38(4): 6095-6103. doi: 10.1016/j.proci.2020.06.155
    [35]
    Yi Tongxun, Santavicca D A. Flame transfer functions for liquid-fueled swirl-stabilized turbulent lean direct fuel injection combustion[J]. Journal of Engineering for Gas Turbines and Power, 2010, 132(2): 021506. doi: 10.1115/1.3157101
    [36]
    Zhang Bo, Shahsavari M, Rao Zhuming, et al. Effects of the fresh mixture temperature on thermoacoustic instabilities in a lean premixed swirl-stabilized combustor[J]. Physics of Fluids, 2020, 32(4): 047101. doi: 10.1063/1.5133859
    [37]
    Freitag E, Konle H, Lauer M, et al. Pressure influence on the flame transfer function of a premixed swirling flame[C]// ASME Turbo Expo 2006: Power for Land, Sea, and Air, New York: American Society of Mechanical Engineers, 2006: 477-486.
    [38]
    Zhu Rongjun, Pan Deng, Ji Chenzhen, et al. Combustion instability analysis on a partially premixed swirl combustor by thermoacoustic experiments and modeling[J]. Energy, 2020, 211: 118884. doi: 10.1016/j.energy.2020.118884
    [39]
    Eder A J, Merk M, Hollweck T, et al. Model-based inference of flame transfer matrices from acoustic measurements in an aero-engine test rig[J]. Journal of Engineering for Gas Turbines and Power, 2025, 147(3): 031022. doi: 10.1115/1.4066366
    [40]
    杨甫江, 郭志辉, 付虓. 基于热声网络法的燃烧不稳定性分析研究[J]. 推进技术, 2014, 35(6): 822-829. Yang Fujiang, Guo Zhihui, Fu Xiao. Analytic study on combustion instability with a thermoacoustic network model[J]. Journal of Propulsion Technology, 2014, 35(6): 822-829. (in Chinese doi: 10.13675/j.cnki.tjjs.2014.06.015

    Yang Fujiang, Guo Zhihui, Fu Xiao. Analytic study on combustion instability with a thermoacoustic network model[J]. Journal of Propulsion Technology, 2014, 35(6): 822-829. (in Chinese) doi: 10.13675/j.cnki.tjjs.2014.06.015
    [41]
    隋永枫, 张宇明, 臧鹏, 等. 轴向分级燃烧室热声稳定性的试验研究[J]. 工程热物理学报, 2024, 45(6): 1625-1633. Sui Yongfeng, Zhang Yuming, Zang Peng, et al. Experimental study on thermoacoustic instability of an axially staged combustor[J]. Journal of Engineering Thermophysics, 2024, 45(6): 1625-1633. (in Chinese

    Sui Yongfeng, Zhang Yuming, Zang Peng, et al. Experimental study on thermoacoustic instability of an axially staged combustor[J]. Journal of Engineering Thermophysics, 2024, 45(6): 1625-1633. (in Chinese)
    [42]
    罗守博, 张弛, 昌运鑫, 等. 掺氢比对阵列微管火焰燃烧噪声的影响研究[J]. 航空动力学报, 2025, 40(5): 20230606. Luo Shoubo, Zhang Chi, Chang Yunxin, et al. Study on influence of hydrogen doping ratio on combustion noise of array microtube flame[J]. Journal of Aerospace Power, 2025, 40(5): 20230606. (in Chinese doi: 10.13224/j.cnki.jasp.20230606

    Luo Shoubo, Zhang Chi, Chang Yunxin, et al. Study on influence of hydrogen doping ratio on combustion noise of array microtube flame[J]. Journal of Aerospace Power, 2025, 40(5): 20230606. (in Chinese) doi: 10.13224/j.cnki.jasp.20230606
    [43]
    Sujith R I, Unni V R. Complex system approach to investigate and mitigate thermoacoustic instability in turbulent combustors[J]. Physics of Fluids, 2020, 32(6): 061401. doi: 10.1063/5.0003702
    [44]
    Muthukrishnan M, Strahle W C, Neale D H. Separation of hydrodynamic, entropy, and combustion noise in a gas turbine combustor[J]. AIAA Journal, 1978, 16(4): 320-327. doi: 10.2514/3.60895
    [45]
    Strahle W C, Muthukrishnan M, Neale D H. Coherence between internal and external noise generated by a gas turbine combustor[J]. AIAA Journal, 1977, 15(7): 1018-1024. doi: 10.2514/3.60744
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (39) PDF downloads(2) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return