防务技术2024,Vol.39Issue(9) :114-122.DOI:10.1016/j.dt.2024.04.019

Experimental investigation for temperature and emissivity by flame emission spectrum in a cavity of rocket based combined cycle combustor chamber

Weiguang Cai Shu Zheng Yan Wang Bing Liu Shaohua Zhu Li Zhao Qiang Lu
防务技术2024,Vol.39Issue(9) :114-122.DOI:10.1016/j.dt.2024.04.019

Experimental investigation for temperature and emissivity by flame emission spectrum in a cavity of rocket based combined cycle combustor chamber

Weiguang Cai 1Shu Zheng 1Yan Wang 1Bing Liu 2Shaohua Zhu 2Li Zhao 1Qiang Lu1
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作者信息

  • 1. National Engineering Research Center of New Energy Power Generation,North China Electric Power University,Beijing 102206,China
  • 2. Science and Technology on Combustion,Internal Flow and Thermal-structure Laboratory,Northwestern Polytechnical University,Xi'an 710072,China
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Abstract

Flame temperature and spectral emissivity were the important parameters characterizing the sufficient degree of fuel combustion and the particle radiative characteristics in the Rocket Based Combined Cycle(RBCC)combustor.To investigate the combustion characteristics of the complex supersonic flame in the RBCC combustor,a new radiation thermometry combined with Levenberg-Marquardt(LM)algorithm and the least squares method was proposed to measure the temperature,emissivity and spectral radi-ative properties based on the flame emission spectrum.In-situ measurements of the flame temperature,emissivity and spectral radiative properties were carried out in the RBCC direct-connected test bench with laser-induced plasma combustion enhancement(LIPCE)and without LIPCE.The flame average temperatures at fuel global equivalence ratio(α)of 1.0b and 0.6 with LIPCE were 4.51%and 2.08%higher than those without LIPCE.The flame combustion oscillation of kerosene tended to be stable in the recirculation zone of cavity with the thermal and chemical effects of laser induced plasma.The differ-ences of flame temperature at α=1.0b and 0.6 were 503 K and 523 K with LIPCE,which were 20.07%and 42.64%lower than those without LIPCE.The flame emissivity with methane assisted ignition was 80.46%lower than that without methane assisted ignition,due to the carbon-hydrogen ratio of kerosene was higher than that of methane.The spectral emissivities at 600 nm with LIPCE were 1.25%,22.2%,and 4.22%lower than those without LIPCE at α=1.0a(with methane assisted ignition),1.0b(without methane assisted ignition)and 0.6.The effect of concentration in the emissivity was removed by normalization to analyze the flame radiative properties in the RBCC combustor chamber.The maximum differences of flame normalized emissivity were 50.91%without LIPCE and 27.53%with LIPCE.The flame radiative properties were stabilized under the thermal and chemical effects of laser induced plasma at a=0.6.

Key words

Rocket-based combined-cycle/Supersonic combustion/Flame temperature measurement/Emissivity/Laser induced plasma combustion/enhancement

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基金项目

National Natural Science Foundation of China(52276185)

National Natural Science Foundation of China(52276189)

National Natural Science Foundation of China(51976057)

Fundamental Research Funds for the Central Universities(2021MS126)

Natural Science Foundation of Jiangsu Province(BK20231209)

Proofof-Concept Project of Zhongguancun Open Laboratory(20220981113)

出版年

2024
防务技术
中国兵工学会

防务技术

CSTPCD
影响因子:0.358
ISSN:2214-9147
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