Thermodynamics-Acoustics Coupling Studies on Self-Excited Combustion Oscillations Maximum Growth Rate

被引:25
作者
Zhao, Dan [1 ]
机构
[1] Univ Canterbury, Coll Engn, Dept Mech Engn, Private Bag 4800, Christchurch 8041, New Zealand
基金
新加坡国家研究基金会; 中国国家自然科学基金;
关键词
thermodynamics; acoustics; hydrocarbon; chemical reaction; energy conversion; thermo-acoustics; ACTIVE CONTROL; INSTABILITY; MODEL; PREDICTION; INJECTOR; FLAME;
D O I
10.1007/s11630-020-1361-8
中图分类号
O414.1 [热力学];
学科分类号
摘要
Unlike electric vehicles and electric aircrafts, hydrocarbon-fuelled (fossil) engine systems are much noisier. By conducting one-step chemical reaction-thermodynamics-acoustics coupling studies and experimental measurements, we explore the universal physics of how hydrocarbon-fuelled combustion is a noise maker. We also explain that how combustion-sustained noise at a particular frequencymis intrinsically selected. These frequencies correspond to the acoustic resonance nature of the combustor. We find that a reacting gas in which the rate of chemical reacting increases with temperature is intrinsically and naturally unstable with respect to acoustic wave motion, since its modal growth rate alpha is greater than 0. Acoustic disturbances tend to exponentially i.e. exp(alpha t) increase first and then are limited by nonlinear effects and finally grow into limit cycle oscillations. The growth rateais found to increase first and then decrease with the gradient of the heat release rate with respect to the temperature change, i.e. heat capacity. The maximum (alpha/omega)(max)depends on the specific heat ratio y, which is related to the speed of sound. The unstable nature could be changed by introducing some acoustic dissipative/damping mechanisms, such as the boundary layer viscous drag and boundary losses. It is shown that such losses could lead to increased critical heat capacity, below which stable combustors can be designed. Finally, the acoustical energy consisting of both potential and kinetic energy is found to grow exponentially faster by 100% than the acoustic disturbance amplitude.
引用
收藏
页码:1591 / 1603
页数:13
相关论文
共 51 条
  • [1] [Anonymous], 1878, NATURE, V18, P319, DOI [DOI 10.1038/018319A0, 10.1038/018319a0]
  • [2] A thermoacoustic Stirling heat engine
    Backhaus, S
    Swift, GW
    [J]. NATURE, 1999, 399 (6734) : 335 - 338
  • [3] Effects of self-pulsation on combustion instability in a liquid rocket engine
    Bai, Xiao
    Cheng, Peng
    Li, Qinglian
    Sheng, Liyong
    Kang, Zhongtao
    [J]. EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2020, 114
  • [4] Extracting flame describing functions in the presence of self-excited thermoacoustic oscillations
    Balusamy, Saravanan
    Li, Larry K. B.
    Han, Zhiyi
    Hochgreb, Simone
    [J]. PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2017, 36 (03) : 3851 - 3861
  • [5] ACOUSTIC FRIDGE TAKES TO SPACE
    BARINAGA, M
    [J]. SCIENCE, 1992, 255 (5044) : 534 - 534
  • [6] A Green's function approach to the rapid prediction of thermoacoustic instabilities in combustors
    Bigongiari, Alessandra
    Heckl, Maria A.
    [J]. JOURNAL OF FLUID MECHANICS, 2016, 798 : 970 - 996
  • [7] Active control of combustion instabilities on a Rijke tube using neural networks
    Blonbou, R
    Laverdant, A
    Zaleski, S
    Kuentzmann, P
    [J]. PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2000, 28 : 747 - 755
  • [8] REHEAT BUZZ - AN ACOUSTICALLY COUPLED COMBUSTION INSTABILITY .2. THEORY
    BLOXSIDGE, GJ
    DOWLING, AP
    LANGHORNE, PJ
    [J]. JOURNAL OF FLUID MECHANICS, 1988, 193 : 445 - 473
  • [9] A Novel Damping Device for Broadband Attenuation of Low-Frequency Combustion Pulsations in Gas Turbines
    Bothien, Mirko R.
    Noiray, Nicolas
    Schuermans, Bruno
    [J]. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2014, 136 (04):
  • [10] NOISE + OSCILLATIONS IN JET ENGINES
    BRAGG, SL
    [J]. NATURE, 1964, 201 (491) : 123 - &