Strong flame interaction-induced collective dynamics of multi-element lean-premixed hydrogen flames

被引:22
作者
Choi, Yongseok [1 ]
Kim, Kyu Tae [1 ]
机构
[1] Korea Adv Inst Sci & Technol KAIST, Dept Aerosp Engn, 291 Daehak Ro, Daejeon 34141, South Korea
基金
新加坡国家研究基金会;
关键词
Combustion instability; Gas turbine combustion; Flame-flame interaction; Higher harmonics; Hydrogen; Lean-premixed; EXCITED AZIMUTHAL MODES; LARGE-EDDY SIMULATION; COMBUSTION INSTABILITY; GAS; OSCILLATIONS; PERFORMANCE; GENERATION; INJECTOR; METHANE;
D O I
10.1016/j.ijhydene.2022.10.091
中图分类号
O64 [物理化学(理论化学)、化学物理学];
学科分类号
070304 ; 081704 ;
摘要
Multi-element injector configurations, typically comprising numerous small-scale jet nozzles, will be required to enable reliable lean-premixed gas turbine combustion operating with pure hydrogen or high hydrogen content fuels. The integration of large numbers of millimeter-scale injectors in tightly clustered arrays is highly likely to produce peculiar topological states determined by the collective dynamics of strongly interacting premixed hydrogen flames. To understand the influence of inter-element flame interactions in a multi-element nozzle environment, here we experimentally investigate the combustion dynamics of two different pure hydrogen flame ensembles, one relatively coarse array of 293 round jet nozzles, and the other a dense array of 421 nozzles. Measurements of self-induced instability were conducted for both configurations under 60-130 thermal power conditions, in conjunction with phase-synchronized OH PLIF and high-speed OH* chemiluminescence emission measurements. We demonstrate that for both cases the characteristic dimension of a single injector element is the main determinant of the fundamental frequency of self-induced pressure oscillations, and that the oscillations are primarily driven by the combination of coherent structure-related flame surface rollup and local extinction/pinch-off. Whereas the coarse injector arrangement exhibits well-organized parallel propagation and deformation of isolated vortical structures, the dense array case manifests strong repulsive interactions between adjacent coherent structures, naturally creating lateral flame surface modulations as well as limited streamwise oscillations. Importantly, collision-induced lateral flame dynamics play a mechanistic role in the substantial growth of higher harmonics in the frequency range of 1-2 kHz, leading to the creation of multiple frequency excitation states of commensurate amplitude, which uniquely define the thermoacoustic state of clustered lean-premixed hydrogen flames.(c) 2022 Hydrogen Energy Publications LLC. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:2030 / 2043
页数:14
相关论文
共 75 条
  • [1] Differential diffusion effects in counter-flow premixed hydrogen-enriched methane and propane flames
    Abbasi-Atibeh, Ehsan
    Bergthorson, Jeffrey M.
    [J]. PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2019, 37 (02) : 2399 - 2406
  • [2] Effects of jet diameter and spacing in a micromixer-like burner for clean oxy-fuel combustion in gas turbines
    Abdelhafez, Ahmed
    Hussain, Muzafar
    Nemitallah, Medhat A.
    Habib, Mohamed A.
    Ali, Asif
    [J]. ENERGY, 2021, 228
  • [3] The effect of hydrogen enrichment, flame-flame interaction, confinement, and asymmetry on the acoustic response of a model can combustor
    Aesoy, Eirik
    Indlekofer, Thomas
    Gant, Francesco
    Cuquel, Alexis
    Bothien, Mirko R.
    Dawson, James R.
    [J]. COMBUSTION AND FLAME, 2022, 242
  • [4] Performance of Multiple-Injection Dry Low-NOx Combustors on Hydrogen-Rich Syngas Fuel in an IGCC Pilot Plant
    Asai, Tomohiro
    Dodo, Satoschi
    Karishuku, Mitsuhiro
    Yagi, Nobuo
    Akiyama, Yasuhiro
    Hayashi, Akinori
    [J]. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2015, 137 (09):
  • [5] Experimental investigation of the nonlinear response of turbulent premixed flames to imposed inlet velocity oscillations
    Balachandran, R
    Ayoola, BO
    Kaminski, CF
    Dowling, AP
    Mastorakos, E
    [J]. COMBUSTION AND FLAME, 2005, 143 (1-2) : 37 - 55
  • [6] Combustion technology developments in power generation in response to environmental challenges
    Beér, JM
    [J]. PROGRESS IN ENERGY AND COMBUSTION SCIENCE, 2000, 26 (4-6) : 301 - 327
  • [7] High-Frequency Thermoacoustic Modulation Mechanisms in Swirl-Stabilized Gas Turbine Combustors-Part I: Experimental Investigation of Local Flame Response
    Berger, Frederik M.
    Hummel, Tobias
    Hertweck, Michael
    Kaufmann, Jan
    Schuermans, Bruno
    Sattelmayer, Thomas
    [J]. JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER-TRANSACTIONS OF THE ASME, 2017, 139 (07):
  • [8] Hydrogen enhancement on a mesoscale swirl stabilized burner array
    Choi, Jeongan
    Rajasegar, Rajavasanth
    Lee, Wooyoung
    Lee, Tonghun
    Yoo, Jihyung
    [J]. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 46 (46) : 23906 - 23915
  • [9] The effect of variable fuel staging transients on self-excited instabilities in a multiple-nozzle combustor
    Culler, Wyatt
    Chen, Xiaoling
    Samarasinghe, Janith
    Peluso, Stephen
    Santavicca, Domenic
    O'Connor, Jacqueline
    [J]. COMBUSTION AND FLAME, 2018, 194 : 472 - 484
  • [10] Flame dynamics and unsteady heat release rate of self-excited azimuthal modes in an annular combustor
    Dawson, James R.
    Worth, Nicholas A.
    [J]. COMBUSTION AND FLAME, 2014, 161 (10) : 2565 - 2578