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不同台阶高度对中心分级燃烧室点火熄火性能的影响
引用本文:付镇柏,林宇震,傅奇慧,张弛.不同台阶高度对中心分级燃烧室点火熄火性能的影响[J].航空动力学报,2014,29(5):1062-1070.
作者姓名:付镇柏  林宇震  傅奇慧  张弛
作者单位:北京航空航天大学 能源与动力工程学院 航空发动机气动热力国家级重点实验室, 北京 100191;北京航空航天大学 能源与动力工程学院 航空发动机气动热力国家级重点实验室, 北京 100191;北京航空航天大学 能源与动力工程学院 航空发动机气动热力国家级重点实验室, 北京 100191;北京航空航天大学 能源与动力工程学院 航空发动机气动热力国家级重点实验室, 北京 100191
摘    要:设计了一种贫油燃烧中心分级燃烧室,采用单头部矩形试验件,试验研究了3种不同台阶高度对点火熄火性能的影响.试验中只有预燃级喷嘴供油工作,在常温常压、常温低压条件下进行了贫油点火试验,在常温常压、加温常压下进行了贫油熄火试验.结果表明:台阶高度越大,贫油点火边界越宽,同时贫油熄火边界越宽;进口温度的升高有助于改善贫油熄火性能,并缩小3种方案贫油熄火油气比的差距,在320~570K的进口温度范围内,贫油熄火油气比的最大差距由40%减小到13%;3种方案都具有较好的常温负压点火性能,且在0.5%~1.5%的火焰筒进出口总压降下,贫油点火油气比差异不大,最大相差不超过10%.

关 键 词:低污染  中心分级燃烧室  点火  熄火  台阶高度
收稿时间:3/5/2013 12:00:00 AM

Effect of different step heights on ignition and blowout performance of internally-staged combustor
FU Zhen-bo,LIN Yu-zhen,FU Qi-hui and ZHANG Chi.Effect of different step heights on ignition and blowout performance of internally-staged combustor[J].Journal of Aerospace Power,2014,29(5):1062-1070.
Authors:FU Zhen-bo  LIN Yu-zhen  FU Qi-hui and ZHANG Chi
Institution:National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
Abstract:A lean-burn internally-staged combustor was designed.Using a single module rectangular test article,the effects of three different step heights on ignition and blowout performance were studied herein.Only the pilot stage nozzle was fueled in the tests.The lean ignition test was operated with normal and negative inlet pressures under normal inlet temperatures condition,and the lean blowout test was operated with the normal and raised inlet temperature under the normal inlet pressure condition.The experimental results indicate that the lean ignition and blowout boundaries are simultaneously widened with the increasing the step height;the inlet temperature rise is good for lean blowout performance with narrowing the lean blowout fuel air ratio differences in these three cases,and the maximum differences decrease from 40% to 13% under the test condition of the inlet temperature of 320-570K;the ignition performance under the negative inlet pressure and normal inlet temperature condition is rather good for all three cases with little difference of the lean ignition fuel air ratio,and the maximum differences don't exceed 10% under the test condition of the liner total pressure drop of 0.5%-1.5%.
Keywords:low pollution  internally-staged combustor  ignition  blowout  step height
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