Study on Ignition Characteristics of Coaxial Graded Low-emission Combustion Chamber of Natural Gas

被引:0
|
作者
Ding, Wenhao [1 ]
Ran, Junhui [2 ]
Liu, Shizheng [2 ]
Xiang, Peng [1 ]
Liu, Xiao [1 ]
机构
[1] Harbin Engineering University, Harbin,150001, China
[2] 703 Research Institute of China Shipbuilding Corporation Limited, Harbin,150078, China
关键词
Combustion chambers - Gas turbines - Ignition - Numerical methods;
D O I
暂无
中图分类号
学科分类号
摘要
Aiming at the ignition characteristics of different factors under the ignition condition of a coaxial staged combustor, the numerical simulation method is used to study the influence of different ignition positions, hot jet velocity, hot jet duration and other factors on the ignition performance under the ignition condition. The best ignition scheme under the ignition condition is determined and the ignition process is simulated. It is found that when the ignition position is close to the outlet of the combustion chamber, it has better ignition performance, but the development speed of the fire core is slow. The higher the velocity of the hot jet flame, the smaller the influence of the axial velocity of the flow field, the better the ignition performance. The increase of the duration of the hot jet makes the volume of the fire core generated on the wall increase, and the ignition success rate increases. © 2024 Science Press. All rights reserved.
引用
收藏
页码:1197 / 1204
相关论文
共 50 条
  • [1] Low-emission combustion of a pre-chamber-type compression ignition natural gas engine
    Sasaki, H.
    Sekiyama, S.
    Hashimoto, M.
    Nakashima, K.
    INTERNATIONAL JOURNAL OF ENGINE RESEARCH, 2007, 8 (06) : 465 - 476
  • [2] Investigation of the Characteristics of a Low-Emission Gas Turbine Combustion Chamber Operating on a Mixture of Natural Gas and Hydrogen
    Serbin, Serhiy
    Burunsuz, Kateryna
    Chen, Daifen
    Kowalski, Jerzy
    POLISH MARITIME RESEARCH, 2022, 29 (02) : 64 - 76
  • [3] Study of Sequential Two-Stage Combustion in a Low-Emission Gas Turbine Combustion Chamber
    Bulysova L.A.
    Berne A.L.
    Vasil’ev V.D.
    Gutnik M.N.
    Gutnik M.M.
    Thermal Engineering, 2018, 65 (11) : 806 - 817
  • [4] Arrangement of low-emission combustion in the annular GTE combustion chamber
    Markushin A.N.
    Merkushin V.K.
    Byshin V.M.
    Baklanov A.V.
    Russian Aeronautics (Iz VUZ), 2009, 52 (3) : 361 - 364
  • [5] Study of a burner module of a low-emission combustion chamber of the GTE-45 gas turbine unit
    Bulysova L.A.
    Vasil'ev V.D.
    Gutnik M.N.
    Gutnik M.M.
    Ermolaev V.V.
    Rusetskii Yu.A.
    Thermal Engineering, 2009, 56 (4) : 293 - 298
  • [6] The effect of fuel and air agitation on the combustion process in a low-emission combustion chamber
    Bulysova L.A.
    Gorban' V.D.
    Thermal Engineering, 2013, Izdatel'stvo Nauka (60) : 619 - 627
  • [7] Low-emission gas turbines using catalytic combustion
    Vatcha, SR
    ENERGY CONVERSION AND MANAGEMENT, 1997, 38 (10-13) : 1327 - 1334
  • [8] Low-Emission combustion of fuel in aeroderivative gas turbines
    Bulysova L.A.
    Vasil’ev V.D.
    Berne A.L.
    Thermal Engineering, 2017, 64 (12) : 891 - 897
  • [9] A computational study of combustion in compression ignition natural gas engine with separated chamber
    Zheng, QP
    Zhang, HM
    Zhang, DF
    FUEL, 2005, 84 (12-13) : 1515 - 1523
  • [10] Influence of plasma-chemical products on process stability in a low-emission gas turbine combustion chamber
    Serbin, Serhiy
    Kozlovskyi, Artem
    Burunsuz, Kateryna
    INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2021,