有限空间内低旋流流动与燃烧特性

邓洋波; 宋德彦; 徐震; 姜曦

doi:10.13224/j.cnki.jasp.2015.07.002

有限空间内低旋流流动与燃烧特性

doi: 10.13224/j.cnki.jasp.2015.07.002

大连海事大学轮机工程学院, 辽宁大连 116026

基金项目:

国家自然科学基金委员会-神华集团有限公司煤炭联合基金资助项目(U1361111)

详细信息

作者简介:
邓洋波(1970-),男,辽宁沈阳人,教授,博士,主要从事高效低污染燃烧技术研究.

中图分类号: V235.21
计量
- 文章访问数: 1198
- HTML浏览量: 4
- PDF量: 760
- 被引次数: 0
出版历程
- 收稿日期: 2014-12-11
- 刊出日期: 2015-07-28

Characteristics of low swirl flow and combustion in a limited space

Marine Engineering College, Dalian Maritime University, Dalian Liaoning 116026, China

摘要

摘要: 为了对低旋流流动特性及其对火焰传播与稳定影响进行深入理解,通过实验与数值模拟相结合的方法,对有限空间内低旋流流动与燃烧特性进行研究.结果表明:改变中心孔板小孔直径,可以形成不同旋流数的旋流喷射器;在冷态条件下,随着旋流数增加,在展向平面上逐渐形成“W”形速度矢量分布;在铅垂截面内,速度矢量分布存在一个环形高速区域、中心低速区和外侧低速区.由于燃烧气体吸热膨胀、涡量诱导和温度斜压效果,使得冷态高旋回流流动转变为了燃烧条件下低旋无回流流动;在有限空间内,低旋流燃烧没有形成脱体火焰,而是形成类似于扩散燃烧火焰;随着旋流数增大,温度分布边界和化学反应边界在展向平面逐渐缩短,而在铅垂截面逐渐扩大.
- 低旋流流动 /
- 旋流数 /
- 流动特性 /
- 燃烧特性 /
- 旋流喷射器
Abstract: To further understand the characteristics of low swirl flow and its effect on the propagation and stability of flame, the characteristics of low swirl flow and combustion in a limited space were studied, through combining experiment method with numerical simulation method. Results show that,changing the diameter of the hole in the plate of center hole can form the swirl injectors with different swirl numbers;in cold state, with increasing of swirl number, gradually formed the “W” shape the velocity vector distribution on spanwise section. there are higher velocity in the annulus zone, lower velocity in central zone and lower velocity outside zone on vertical section. The absorption and heat expansion of gas, vorticity induced and temperature baroclinic effect induce a transition from high swirl flow with recirculation in cold state to low swirl flow without recirculation in combustion state; In a limited space, the low swirl combustion cannot form detached flame, but form a flame similar to the diffusion combustion flame; the temperature distribution boundary and chemical reaction boundary gradually get shorter along spanwise section, and gradually get wider along vertical section.
- low swirl flow /
- swirl number /
- flow characteristic /
- combustion characteristic /
- swirl injector

HTML

参考文献(18)

[1]	Yegian D T,Cheng R K.Development of a lean premixed low-swirl burner for low NOx practical applications[J]. Combustion Science and Technology,1998,139(1):207-227.
[2]	Cheng R K,Fable S A,Chmidt D S,et al.Development of a low swirl injector concept for gas turbines[R].New Orleans,US:International Joint Power Conference,2001.
[3]	Nazeer W A,Smith K O,Sheppard P,et al.Full scale testing of a low swirl fuel injector concept for ultra-low NOx gas turbine combustion systems[R].ASME Paper GT2006-90150,2006.
[4]	Cheng R K,Littlejohn D,Nazeer W A,et al.Laboratory studies of the flow field characteristics of low-swirl injectors for adaptation to fuel-flexible turbines[J].Journal of Engineering for Gas Turbines and Power,2008,130(2):021501.1-021501.10.
[5]	Littlejohn D,Cheng R K.Fuel effects on a low-swirl injector for lean premixed gas turbines[J].Proceedings of the Combustion Institute,2007,31(2):3155-3162.
[6]	Peter T,Cheng R K.Flashback,blow out,emissions,and turbulent displacement flame speed measurements in a hydrogen and methane fired low-swirl injector at elevated pressures and temperatures[R].ASME Paper GT2012-68216,2012.
[7]	葛冰,田寅申,袁用文,等.重型燃气轮机先进低NOx燃烧技术分析[J].热力透平,2013,42(4):251-259. GE Bing,TIAN Yinsheng,YUAN Yongwen,et al.Advanced low NOx combustion technologies for heavy-duty gas turbine[J].Thermal Turbine,2013,42(4):251-259.(in Chinese)
[8]	尹航,戴韧,张建辉,等.旋流器安装角对低旋流燃烧流场的影响[J].动力工程学报,2011,36(9):664-671. YIN Hang,DAI Ren,ZHANG Jianhui,et al.Effect of vane setting angle of swirler on flow field of a low-swirl burner[J].Journal of Chinese Society of Power Engineering,2011,36(9):664-671.(in Chinese)
[9]	尹航,戴韧,邹玉耐,等.贫预混低旋流燃烧器吹脱极限和流场的测量[J].燃气轮机技术,2012,25(2):26-31. YIN Hang,DAI Ren,ZOU Yunai,et al.Measurements of blow off limit and flowfields of low swirl lean premixed burners[J].Gas Turbine Technology,2012,25(2):26-31.(in Chinese)
[10]	尹航,钟仕立,戴韧,等.合成气低旋流燃烧器设计与流动结构的分析[J].动力工程学报,2011,31(2):131-136. YIN Hang,ZHONG Shili,DAI Ren,et al.Design of low swirl syngas burner and analysis on the flow pattern[J].Journal of Chinese Society of Power Engineering,2011,31(2):131-136.(in Chinese)
[11]	柳伟杰,葛冰,田寅申,等.当量比对甲烷预混低旋流燃烧的影响[J].燃烧科学与技术,2014,20(1):65-69. LIU Weijie,GE Bing,TIAN Yinshen,et al.Effect of equivalence ratio on methane pre-mixed low-swirl combustion[J].Journal of Combustion Science and Technology,2014,20(1):65-69.(in Chinese)
[12]	邓洋波,刘阳,朱公志.低旋流燃烧和流动特性数值模拟研究[J].大连海事大学学报,2009,35(4):99-102. DENG Yangbo,LIU Yang,ZHU Gongzhi.Numerical simulation of low-swirl combustion and flowfield[J].Journal of Dalian Maritime University,2009,35(4):99-102.(in Chinese)
[13]	Chan C K,Lau K S,Chin W K,et al.Freely propagating open premixed turbulent flames stabilized by swirl[J].Symposium (International) on Combustion,1992,24(1):511-518.
[14]	Cheng R K,Yegian D T,Miyasato M M,et al.Scaling and development of low-swirl burners for low emission furnace and boilers[J].Proceedings of Combustion Institute,2000,28(1):1305-1313.
[15]	De Lange H C,Houben M P,van Steenhoven A A.Stereo-PIV analysis of the low-swirl flow above a partial oxidation burner[J].Combustion Science and Technology,2006,178(9):1541-1557.
[16]	Johnson M R,Littlejohn D,Nazeer W A,et at,A comparison of the flowfields and emissions of high-swirl injectors and low-swirl injectors for lean premixed gas turbines[J].Proceedings of the Combustion Institute,2005,30(2):2867-2874.
[17]	徐震.IGCC低旋流燃烧器冷态流场的实验与数值研究[D].大连:大连海事大学,2014. XU Zhen.Experimental and numerical research on the flow-field of the IGCC low swirl combustor[D].Dalian:Dalian Maritime University,2014.(in Chinese)
[18]	Yang S C,Chen L C.Swirl generator with axial vanes:United States,5186607[P].1993-02-16.