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首页> 外文期刊>Journal of Zhejiang University. Science, A >Emission characteristics and combustion instabilities in an oxy-fuel swirl-stabilized combustor
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Emission characteristics and combustion instabilities in an oxy-fuel swirl-stabilized combustor

机译:氧燃料旋流稳定燃烧器中的排放特性和燃烧不稳定性

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This paper presents an experimental study on the emission characteristics and combustion instabilities of oxy-fuel combustions in a swirl-stabilized combustor. Different oxygen concentrations (Xoxy=25%~45%, where Xoxy is oxygen concentration by volume), equivalence ratios (Φ=0.75~1.15) and combustion powers (CP=1.08~2.02 kW) were investigated in the oxy-fuel (CH4/CO2/O2) combustions, and reference cases (Xoxy=25%~35%, CH4/N2/O2 flames) were covered. The results show that the oxygen concentration in the oxidant stream significantly affects the combustion delay in the oxy-fuel flames, and the equivalence ratio has a slight effect, whereas the combustion power shows no impact. The temperature levels of the oxy-fuel flames inside the combustion chamber are much higher (up to 38.7%) than those of the reference cases. Carbon monoxide was vastly produced when Xoxy>35% or Φ>0.95 in the oxy-fuel flames, while no nitric oxide was found in the exhaust gases because no N2 participates in the combustion process. The combustion instability of the oxy-fuel combustion is very different from those of the reference cases with similar oxygen content. oxy-fuel combustions excite strong oscillations in all cases studied Xoxy=25%~45%. However, no pressure fluctuations were detected in the reference cases when Xoxy>28.6% accomplished by heavily sooting flames which were not found in the oxy-fuel combustions. Spectrum analysis shows that the frequency of dynamic pressure oscillations exhibits randomness in the range of 50~250 Hz, therefore resulting in a very small resultant amplitude. Temporal oscillations are very strong with amplitudes larger than 200 Pa, even short time fast Fourier transform (FFT) analysis (0.08 s) shows that the pressure amplitude can be larger than 40 Pa.
机译:本文介绍了旋流稳定燃烧器中氧燃料燃烧的排放特性和燃烧不稳定的实验研究。不同的氧浓度(xOxy = 25%〜45%,其中氧化氧基体积氧浓度),在氧气燃料中研究了等当量比(φ= 0.75〜1.15)和燃烧功率(CP = 1.08〜2.02 kW)(CH4 / CO2 / O2)燃烧,并参考案例(XOXY = 25%〜35%,CH4 / N2 / O2火焰)被覆盖。结果表明,氧化剂流中的氧浓度显着影响氧燃料火焰中的燃烧延迟,等效率具有轻微的效果,而燃烧动力显示出影响。燃烧室内的氧燃料火焰的温度水平高于参考病例的氧燃料火焰的温度水平比参考病例高得多(高达38.7%)。当氧化燃料火焰中的氧化氧氧> 35%或φ> 0.95时大量产生一氧化碳,而废气中没有发现一氧化氮,因为没有N2参与燃烧过程。氧燃料燃烧的燃烧不稳定性与具有相似氧含量的参考病例的燃烧不稳定性均不同。氧气燃料燃烧在所有案例中激发强烈的振荡XOXY = 25%〜45%。然而,当XOXY> 28.6%通过在氧气燃料燃烧中未发现的烟雾大量烟道而完成的XOXY> 28.6%没有检测到压力波动。光谱分析表明,动态压力振荡的频率在50〜250Hz的范围内表现出随机性,因此导致具有非常小的合成幅度。时间振荡与大于200Pa的幅度非常强,甚至短时间快速傅里叶变换(FFT)分析(0.08秒)表示压力幅度可以大于40Pa。

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