TY - GEN
T1 - Stability limits of methane/oxygen mixtures diluted by n2 and CO2 under various oxygen contents
AU - Zhao, Xiaoyao
AU - Shi, Baolu
AU - Wang, Guoxing
AU - Gao, Wei
AU - Ma, Kang
AU - Li, Junwei
N1 - Publisher Copyright:
© 2018, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2018
Y1 - 2018
N2 - For safe utility of methane, including underground mining, ordinary air combustion and oxygen enhanced combustion, stability limits of methane mixtures diluted by nitrogen and carbon dioxide were experimentally investigated by using a swirl type tubular flame burner. The oxygen mole fraction (β) in the oxidizer was varied to determine the minimum β to sustain the methane combustion, and then gradually increased to 1.0 (pure oxygen). In the tests of β less than 0.4, the premixed mode combustion (PM), in which a pre-mixture was tangential injected into a cylindrical burner, was adopted to examine the flame structure and stability limits. In the case of β above 0.4, to avoid flame flash back, the rapidly mixed mode (RM) was conducted, in which the fuel and oxidizer were individually injected. The results show that RM can obtain the same stability limit as that of PM. The flammable range of N2 diluted mixture was much larger than that of CO2 dilution. The minimum β to sustain the combustion was 0.11 and 0.2 for N2 and CO2 diluted mixture, respectively. For the lean stability limit of N2 diluted mixture, the fuel volume percentage in the overall reactants was maintained around 5% under various oxygen mole fractions; that for CO2 diluted combustion gradually decreased from 8% to 6%. The differences between two diluents were also evaluated.
AB - For safe utility of methane, including underground mining, ordinary air combustion and oxygen enhanced combustion, stability limits of methane mixtures diluted by nitrogen and carbon dioxide were experimentally investigated by using a swirl type tubular flame burner. The oxygen mole fraction (β) in the oxidizer was varied to determine the minimum β to sustain the methane combustion, and then gradually increased to 1.0 (pure oxygen). In the tests of β less than 0.4, the premixed mode combustion (PM), in which a pre-mixture was tangential injected into a cylindrical burner, was adopted to examine the flame structure and stability limits. In the case of β above 0.4, to avoid flame flash back, the rapidly mixed mode (RM) was conducted, in which the fuel and oxidizer were individually injected. The results show that RM can obtain the same stability limit as that of PM. The flammable range of N2 diluted mixture was much larger than that of CO2 dilution. The minimum β to sustain the combustion was 0.11 and 0.2 for N2 and CO2 diluted mixture, respectively. For the lean stability limit of N2 diluted mixture, the fuel volume percentage in the overall reactants was maintained around 5% under various oxygen mole fractions; that for CO2 diluted combustion gradually decreased from 8% to 6%. The differences between two diluents were also evaluated.
KW - CO dilution
KW - N dilution
KW - Oxygen content
KW - Stability limit
KW - Tubular flame
UR - https://www.scopus.com/pages/publications/85083937719
U2 - 10.2514/6.2018-4802
DO - 10.2514/6.2018-4802
M3 - Conference contribution
AN - SCOPUS:85083937719
SN - 9781624105715
T3 - 2018 International Energy Conversion Engineering Conference
BT - 2018 International Energy Conversion Engineering Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 14th International Energy Conversion Engineering Conference, IECEC 2018
Y2 - 9 July 2018 through 11 July 2018
ER -