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自激振荡预混燃烧的实验
引用本文:张昊,黄铮,朱民.自激振荡预混燃烧的实验[J].航空动力学报,2011,26(1):28-34.
作者姓名:张昊  黄铮  朱民
作者单位:清华大学,机械工程学院,热能工程系,热科学与动力工程教育部重点实验室,北京,100084
基金项目:国家重点基础研究发展计划
摘    要:通过动态压力测量、化学自发荧光相同步测量的方法对自激振荡燃烧动力学过程进行了实验研究,分析了不同空气流量、化学当量比和边界条件对振荡燃烧过程的影响.实验结果显示,燃烧热负荷的提高会导致燃烧段压力脉动幅值的提高,使燃烧更加不稳定.化学当量比越接近熄火极限,压力脉动的频率越高.同时燃烧室进出口边界条件的改变也会对振荡频率产生影响.

关 键 词:燃气轮机燃烧室  贫预混预蒸发燃烧  振荡燃烧  动态测量  相同步测量
收稿时间:2009/12/4 0:00:00
修稿时间:2010/2/10 0:00:00

Experimental study on self-excited oscillations in premixed combustor
ZHANG Hao,HUANG Zheng and ZHU Min.Experimental study on self-excited oscillations in premixed combustor[J].Journal of Aerospace Power,2011,26(1):28-34.
Authors:ZHANG Hao  HUANG Zheng and ZHU Min
Institution:ZHANG Hao,HUANG Zheng,ZHU Min(Key Laboratory for Thermal Science and Power Engineering of Ministration of Education,Department of Thermal Engineering,School of Mechanical Engineering,Tsinghua University,Beijing 100084,China)
Abstract:Combustion instabilities were studied experimentally by coupling unsteady heat release and pressure perturbations.In this paper,the experimental studies were conducted to analyze the dynamic processes of self-excited combustion oscillations through dynamic pressure and phase-locked chemiluminescence measurements.The effects of air mass flow,equivalence ratio and boundary conditions on combustion system were examined.This shows that the amplitudes of oscillation will enlarge with the increasing system load,l...
Keywords:gas turbine combustor  lean premixed prevaporized combustion  combustion instabilities  dynamical measurement  phase-locked measurement  
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