期刊文献+

不同喷嘴结构合成气燃烧室动态特性的实验研究 被引量:4

Experimental Investigation of Dynamic Characteristics of Syngas-Burned Combustors With Different Nozzles
原文传递
导出
摘要 通过中压全尺寸燃气轮机燃烧室测试平台的合成气燃烧试验,对单喷嘴和多喷嘴燃烧室的动态特性进行了比较分析。在本文的测试工况下,燃烧室没有产生强烈的热声振荡,所有的燃烧过程都很稳定,说明喷嘴的设计是合理的。多喷嘴燃烧室在相似工况下动态压力幅值比单喷嘴燃烧室要小一半以上,功率谱曲线相对平滑,说明多喷嘴燃烧室确实能降低燃烧噪声。单喷嘴和多喷嘴燃烧室在某些工况下都出现了低于10 Hz的极低频压力振荡,且振荡功率相对较大,可能会产生较大的危害,需要进一步研究其产生的机理和抑制方法。本文的研究结果为高氢燃气轮机的设计和改造提供了参考。 Through syngas combustion tests in a full-scale gas turbine combustor medium-pressure test rig.this paper compares the dynamic characteristics of the single-nozzle and multi-nozzle combustors.It is found that the combustion processes are very stable under all experimental conditions in this paper,without intensive thermoacoustic oscillation occurred.These mean that the designations of the combustors are reasonable.At the similar operation conditions,the amplitude of combustion noise in the multi-nozzle combustor is lower than that in single-nozzle combustor,which means that the configuration of multi-nozzle can indeed decrease the combustion noise in the gas turbine combustor.There are pressure oscillations with relative high power and the frequencies less than 10 Hz occurring in some operation conditions both in single-nozzle and multi-nozzle combustors which can perhaps result in detriments to gas turbines and need to be investigated further.
出处 《工程热物理学报》 EI CAS CSCD 北大核心 2011年第6期1053-1057,共5页 Journal of Engineering Thermophysics
基金 国家自然科学基金资助项目(No.50976116 No.50806077)
关键词 燃气轮机 燃烧室 合成气 热声振荡 动态特性 gas turbine combustor syngas thermoacoustic oscillation dynamic characteristic
作者简介 宋权斌(1973-),男,江苏海安人,副研究员,博士,主要从事气化、IGCC系统和燃烧不稳定的研究。
  • 相关文献

参考文献4

二级参考文献6

共引文献24

同被引文献13

  • 1BRANDT D E, WESORIEK R R. GE gas turbine design philosophy [R]. GER-3434d, Schenectady.. GE Power Systems, 1994.
  • 2FANACA D, ALEMELA P R, HIRSCH C, et al. Comparison of the flow field of a swirl stabilized premixed burner in an annular and a single burner combustion chamber [J]. Journal of Engineering for Gas Turbines and Power, 2010, 132 (7): 071502-1- 071502-7.
  • 3BOEHM B, DREIZLER A, GNIRSS M, et al. Ex- perimental investigation of turbulence structure in a three-nozzle combustor [ C] // ASME Turbo Expo 2007, GT2007-27111.
  • 4AGUILAR M, MALANOSKI M, ADHITYA G, et al. Helical flow disturbances in a multi-nozzle com- bustor [C] // ASME Turbo Expo 2014, GT2014- 26272. Dtisseldorf.. ASME, 2014.
  • 5MICHAEL T S, BRYAN D Q,JANITH S, et al. Forced flame response of a lean premixed multi-nozzle can combustor [C] //Proceedings of ASME Turbo Expo 2011, GT2011-46080. British Columbia: ASME, 2011.
  • 6BIBIK O, LUBARSKY E, SHCHERBIK D, et al. Rotational traveling of tangential wave in multi-Injec- tors LRE combustor simulator [C] //46th AIAA Aerospace Sciences Meeting and Exhibit. Reno : AIAA, 2008.
  • 7SZEDLMAYER M T, QUAY B D, SAMARASING- HE J, et al. Forced {lame response of a lean premixed multi-nozzle can combustor [C] // Proceed- ings of ASME Turbo Expo 2011, GT2011-46080.British Columbia: ASME, 2011.
  • 8DAY M, TACHIBANA S, BELL J, et al. A eom bined computational and experimental characterization of lean premixed turbulent low swirl laboratory flames I. Methane flames {-J 1. Combustion and Flame, 2012, 159(1): 275-290.
  • 9LITTLEJOHN D, CHENG R K, NOBLE D R, et al. Laboratory investigations of low-swirl injectors operating with syngases [J]. Journal of Engineering for Gas Turbines and Power, 2009, 132(1):1-8.
  • 10唐志国,马培勇,李永玲,唐超君,邢献军,林其钊.基于无焰氧化的煤粉气化炉模型设计与试验研究[J].中国电机工程学报,2010,30(8):50-55. 被引量:12

引证文献4

二级引证文献11

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部