本文已被:浏览 1168次 下载 532次
中文摘要: 为了对比扩散和预混两种不同燃烧模式下大气温度对燃气轮机燃烧稳定性和NOx排放的影响规律, 针对某重型燃气轮机燃烧室,对多旋流喷嘴燃烧室的燃烧稳定性和NOx排放进行了数值研究。结果表明:对 于扩散燃烧,大气温度升高,燃烧室内高频脉动增强,燃烧稳定性变差;对于预混燃烧,大气温度升高,有利于 提高燃烧的稳定性;在扩散燃烧模式下燃烧室燃料喷嘴下游回流区的温度最高,NOx生成量最大;预混燃烧下 燃烧室头部温度分布较均匀,燃烧室NOx生成主要集中在驻涡回流区和燃烧室中下游位置,燃料喷嘴下游回 流区NOx生成量很小;随着大气温度的升高,扩散燃烧和预混燃烧下燃烧室内NOx的生成量均增加。研究结 果可为指导燃气轮机运行提供参考。
Abstract:In order to compare the influence of environmental temperature on combustion stability and NOx emission under different
combustion modes of a gas turbine, taking a heavy gas turbine combustor as the research object,the numerical models of full-scale
combustor for the diffusion and premixed combustion were established. The combustion stability and NOx emissions of the multi-swirl
nozzle combustor were numerically calculated. The results showthat for the diffusion combustion,the high frequency pulsation in the
combustor is enhanced after the environmental temperature rises, and the combustion stability is deteriorated. For the premixed
combustion,the increase of the environmental temperature is beneficial to improve the stability of combustion; In the diffusion
combustion mode,the temperature in the downstream recirculation zone of the combustor fuel nozzle is the highest,and the NOx
production is also the largest. In the premixed combustion mode, the temperature distribution in the combustor head is relatively
uniform,the NOx formation in the combustor is mainly concentrated in the trapped vortex recirculation zone and the middle and
downstream of the combustor,the NOx formation in the downstream recirculation zone of the fuel nozzle is small; As the environmental
temperature increases,the amount of NOx generated in the combustor increases under both diffusion and premixed combustion. The
research results provide a reference for guiding the operation of gas turbines.
文章编号: 中图分类号:TK471 文献标志码:
基金项目:中国华能集团有限公司总部科技项目(HNKJ18 - H11 );西安热工研究院有限公司研究开发基金项目(TI - 18 -TYK06)
Author Name | Affiliation |
Xiao Junfeng | |
Li Xiaofeng | |
Wang Feng | |
Wang Wei | |
Hu Mengqi |
引用文本:
作者.题名[J].刊名,出版年份,卷号(期号):起止页码.
[2]KIM K M, PARK J S, DONG H L, et al. Analysis of conjugated heat transfer, stress and failure in a gas turbine blade with circular cooling passages[J]. Engineering Failure Analysis, 2011, 18(4):1212-1222.
作者.题名[J].刊名,出版年份,卷号(期号):起止页码.
[2]KIM K M, PARK J S, DONG H L, et al. Analysis of conjugated heat transfer, stress and failure in a gas turbine blade with circular cooling passages[J]. Engineering Failure Analysis, 2011, 18(4):1212-1222.