1. Hunan Aviation Powerplant Research Institute,Aero Engine (Group) Corporation of China,Hunan,Zhuzhou,China,412002
2. National Key Laboratory of Science and Technology on AeroEngine Aerothermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics,Beijing,China,100191
纸质出版:2017
移动端阅览
KANG Yao, LIN Yu-zhen. Influence of coupled characteristics on the internallystaged combustor under lowpower operation[J]. 航空动力学报, 2017, 32(1): 42-52.
doi: 10.13224/j.cnki.jasp.2017.01.007
KANG Yao, LIN Yu-zhen. Influence of coupled characteristics on the internallystaged combustor under lowpower operation[J]. 航空动力学报, 2017, 32(1): 42-52. DOI: 10.13224/j.cnki.jasp.2017.01.007.
doi: 10.13224/j.cnki.jasp.2017.01.007 DOI:
An ultralow emissions combustor
namely low emission stirred swirl (LESS) combustor was studied
based on a scheme of internallystaged/lean premixed and prevaporized (LPP) combustion. The LESS combustor consists of central pilot stage and outer surrounded coaxially main stage
between which there exists a physical isolation
namely the step height. The existence of step height delayed the pilot and main jets mixing. Experimental and numerical studies were carried out to investigate the influence of the step height on the combustion performance. A single dome rectangular combustor was utilized to conduct the lean lightoff and blowout experiments
and pollutant emission experiments. The experimental results showed that with the increase of step height by 38%
the lean lightoff and blowout fuel air ratio decreased by 574% and 375%
the NOx emission increased by 35.1%
and the combustion efficiency increased by 1.78%; while the CO
unburned hydrocarbons (UHC) emissions decreased. Furthermore
the total pressure loss was kept nearly constant. Nonreacting and reacting flow fields were numerically investigated to analyze the coupled characteristics of pilot and main jets with different step heights. A comparison of flow characteristics
spray structure
and combustion component as well as temperature field with different step heights was conducted. The numerical results showed that the increase of the step height shifted the peak velocity outwards. The enlargement of the primary recirculation zone (PRZ) resulted in the increase of the combustion efficiency and NOx emission
while the CO
UHC emissions decreeased.
An ultralow emissions combustor
namely low emission stirred swirl (LESS) combustor was studied
based on a scheme of internallystaged/lean premixed and prevaporized (LPP) combustion. The LESS combustor consists of central pilot stage and outer surrounded coaxially main stage
between which there exists a physical isolation
namely the step height. The existence of step height delayed the pilot and main jets mixing. Experimental and numerical studies were carried out to investigate the influence of the step height on the combustion performance. A single dome rectangular combustor was utilized to conduct the lean lightoff and blowout experiments
and pollutant emission experiments. The experimental results showed that with the increase of step height by 38%
the lean lightoff and blowout fuel air ratio decreased by 574% and 375%
the NOx emission increased by 35.1%
and the combustion efficiency increased by 1.78%; while the CO
unburned hydrocarbons (UHC) emissions decreased. Furthermore
the total pressure loss was kept nearly constant. Nonreacting and reacting flow fields were numerically investigated to analyze the coupled characteristics of pilot and main jets with different step heights. A comparison of flow characteristics
spray structure
and combustion component as well as temperature field with different step heights was conducted. The numerical results showed that the increase of the step height shifted the peak velocity outwards. The enlargement of the primary recirculation zone (PRZ) resulted in the increase of the combustion efficiency and NOx emission
while the CO
UHC emissions decreeased.
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