Experimental and numerical characterization of hydrogen combustion in a reverse-flow micro gas turbine combustor

被引:4
|
作者
Jamshidiha, M. [1 ,2 ,3 ]
Kamal, M. M. [1 ,2 ,3 ]
Cafiero, M. [1 ,2 ,3 ]
Coussement, A. [1 ,2 ,3 ]
Parente, A. [1 ,2 ,3 ]
机构
[1] Univ Libre Bruxelles, Ecole Polytech Bruxelles, Aerothermo Mech Lab, Brussels, Belgium
[2] Univ Libre Bruxelles, Brussels, Belgium
[3] Vrije Univ Brussel, Brussels Inst Thermal Fluid Syst & Clean Energy BR, Brussels, Belgium
关键词
Non-premixed flames; Turbulent combustion; Micro gas turbine; Exhaust emissions; Chemiluminescence; Hydrogen combustion; NOX EMISSIONS; STEAM INJECTION; AIR; HYDROCARBON; INTENSITY; CHEMISTRY; OXIDATION; MIXTURES; REACTOR; FLAMES;
D O I
10.1016/j.ijhydene.2023.11.243
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
This study conducts experimental and numerical investigations on a stagnation-point, reverse-flow combustor to examine the effect of its design features on the combustion behavior and emission characteristics of non-premixed, turbulent hydrogen/air flames. The study covers a wide range of equivalence ratios, from ultra-lean to stoichiometric, and thermal power inputs varying between 5 kW and 20 kW. The main motivation behind this design is to achieve passive recirculation of flue gas within the combustor to enhance dilution of the incoming charge, thus potentially leading to relatively uniform thermal fields, lower temperatures, and suppressed NOx emissions. This design concept is implemented in a micro gas turbine - a practical energy conversion device tapped to play a major role in decarbonizing CHP systems suitable for small-scale industries. Optical chemiluminescence measurements, in addition to thermocouple-based temperature and Quantum Cascade Laser (QCL) spectroscopy-based exhaust emissions measurements, were conducted for all the test cases. Spatial OH* signal intensity is used as heat release signature to identify distinct features of the test flames, allowing for useful information on the nature and dynamics of the combustion process within the combustor. The results show stable hydrogen/air flames for all the operating conditions; however, a more distributed combustion is observed at higher powers for all the given equivalence ratios. Relatively higher NOx emissions at phi >0.2 suggest the lower achieved mixing between burnt and fresh gases, particularly in the non-preheated case, prevent a thorough dilution of the fresh mixture. The latter is necessary to achieve low-temperature, uniform thermal fields - an essential for low thermal NOx emissions in gas turbine combustors. Further, CFD results show that preheating considerably changes flow field dynamics and recirculation pattern for better mixing; however, this also dramatically increases thermal NOx emission, with the lowest levels observed at phi = 0.2, while the peak occurs at phi = 0.4. Finally, a 'brute-force' sensitivity analysis shows that thermal NO and NNH pathways contribute the most to NO formation in hydrogen/air flames.
引用
收藏
页码:1299 / 1311
页数:13
相关论文
共 50 条
  • [1] Numerical investigation of flow in the liner of a model reverse-flow gas turbine combustor
    Shojaeefard, M. H.
    Ariafar, K.
    Goudarzi, K.
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2009, 223 (G8) : 1083 - 1090
  • [2] Flow characteristics in the liner of a reverse-flow gas turbine combustor
    Bharani, S
    Singh, SN
    Agrawal, DP
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2001, 215 (A4) : 443 - 451
  • [3] Combustion Instability Modeling in a Reverse-Flow Gas Turbine Combustor using a Network Model
    Son, Juchan
    Kim, Daesik
    JOURNAL OF THE KOREAN SOCIETY OF COMBUSTION, 2021, 26 (04) : 20 - 28
  • [4] Numerical Investigation of Swirl's Effects in the Outer Annulus of a Reverse-flow Gas Turbine Combustor
    Tayeblou, Mostafa Ghanei
    Ariafar, Kavous
    CONTINUUM MECHANICS, FLUIDS, HEAT, 2010, : 262 - +
  • [5] Numerical Investigation of NOx Emission Reduction in Non-Premixed Lean Reverse-Flow Combustor in a Micro Gas Turbine Engine
    Jesline Joy
    Peng Cheng Wang
    Jeggathishwaran Panisilvam
    Simon Ching Man Yu
    Emission Control Science and Technology, 2020, 6 : 285 - 300
  • [6] Numerical Investigation of NOx Emission Reduction in Non-Premixed Lean Reverse-Flow Combustor in a Micro Gas Turbine Engine
    Joy, Jesline
    Wang, Peng Cheng
    Panisilvam, Jeggathishwaran
    Yu, Simon Ching Man
    EMISSION CONTROL SCIENCE AND TECHNOLOGY, 2020, 6 (02) : 285 - 300
  • [7] EXPERIMENTAL STUDY OF COMBUSTION ON A MICRO GAS TURBINE COMBUSTOR
    Wang Feng-Shan
    Kong Wen-Jun
    Wang Bao-Rui
    PROCEEDINGS OF THE ASME TURBO EXPO 2008, VOL 3, PTS A AND B, 2008, : 749 - 755
  • [8] Numerical and Experimental Study on Combustion Characteristics of Micro-Gas Turbine Biogas Combustor
    Liu, Aiguo
    Fan, Ruiyang
    Liu, Qiaochu
    Xi, Lei
    Zeng, Wen
    ENERGIES, 2022, 15 (21)
  • [9] Numerical and experimental study of a micro gas turbine combustor
    Reale, F.
    Calabria, R.
    Chiariello, F.
    Massoli, P.
    Pagliara, R.
    Piazzesi, R.
    THMT-12. PROCEEDINGS OF THE SEVENTH INTERNATIONAL SYMPOSIUM ON TURBULENCE, HEAT AND MASS TRANSFER, 2012, : 1547 - 1556
  • [10] Experimental Investigation on Flow Characteristics of a Reverse-Flow Combustor
    Hu, Ge
    Li, Jianzhong
    Jin, Wu
    Zhang, Jingzhou
    Yuan, Li
    Zhai, Weikuo
    INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2022, 2022