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单扇区、扇形、全环燃烧室热声不稳定性试验和模拟研究
引用本文:高贤智,何沛,冯晓星,邓向阳,蒋晶晶.单扇区、扇形、全环燃烧室热声不稳定性试验和模拟研究[J].航空动力学报,2021,36(8):1605-1613.
作者姓名:高贤智  何沛  冯晓星  邓向阳  蒋晶晶
作者单位:中国航空发动机集团有限公司商用航空发动机有限责任公司,上海200241
摘    要:贫油分级燃烧室在单扇区、扇形、全环燃烧室试验台上均会发生自激周期性燃烧不稳定现象,但振荡模态和频率存在差异.为研究这一差异并建立三者之间的联系,同时验证热声不稳定性模拟方法,对三种试验台的燃烧不稳定性进行了试验和数值模拟研究,获得了不同试验台的振荡特性,并对数值模拟和试验结果进行了对比.结果 表明:全环燃烧室存在两个失...

关 键 词:燃烧不稳定  热声振荡  失稳频率  全环燃烧室  扇形燃烧室
收稿时间:2020/11/12 0:00:00

Experimental and numerical investigation of thermo-acoustic instability in single-sector, sector and full annular combustors
GAO Xianzhi,HE Pei,FENG Xiaoxing,DENG Xiangyang,JIANG Jingjing.Experimental and numerical investigation of thermo-acoustic instability in single-sector, sector and full annular combustors[J].Journal of Aerospace Power,2021,36(8):1605-1613.
Authors:GAO Xianzhi  HE Pei  FENG Xiaoxing  DENG Xiangyang  JIANG Jingjing
Institution:Commercial Aircraft Engine Company Limited, Aero Engine Corporation of China, Shanghai 200241, China
Abstract:Self-excited periodic combustion instabilities in a staged lean burn combustor could be generated by operating the combustor at single-sector,sector and full annular combustor test rigs,but differences existed in oscillation modes and frequencies.In order to investigate the differences and establish the relationship among them,and to verify the thermo-acoustic instability simulation method,experiments and numerical simulations of combustion instabilities were carried out on these three kinds of test rigs,the oscillation characteristics of different test rigs were obtained,and the results were compared between simulations and experiments.The results showed that there were two unstable modes in full annular combustor,while only one unstable mode existed in sector combustor and single-sector combustor.The single-sector and sector combustors can represent one of the unstable modes in full annular combustor,but cannot represent another unstable mode.The three-dimensional finite element method thermo-acoustic simulation method accurately predicted the combustion instabilities of these three different kinds of test rigs,and the predicted dimensionless unstable frequencies were consistent with the experimental results with an error within 2%.
Keywords:combustion instability  thermo-acoustic oscillation  unstable frequency  full annular combustor  sector combustor
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