热能与动力

环形中心钝体驻涡燃烧室后钝体进气位置研究

  • 高翠翠 ,
  • 韩吉昂 ,
  • 钟兢军 ,
  • 李晓东
展开
  • (大连海事大学  轮机工程学院,辽宁 大连 116026)
高翠翠(1990—),女,硕士生.

收稿日期: 2016-06-27

  修回日期: 2016-09-17

  网络出版日期: 2016-09-18

基金资助

辽宁省高等学校创新团队资助项目(LT2015004).

Study of air injection position on aft- bluff -body in an annular central bluff-body trapped vortex combustor

  • GAO Cui-cui ,
  • HAN Ji-ang ,
  • ZHONG Jing-jun ,
  • LI Xiao-dong
Expand
  • (Marine Engineering College,Dalian Maritime University,Dalian 116026,China)

Received date: 2016-06-27

  Revised date: 2016-09-17

  Online published: 2016-09-18

摘要

采用Fluent软件对驻涡腔不同后钝体进气位置时冷态条件下环形中心钝体驻涡燃烧室流场进行数值研究.详细分析了不同后钝体进气位置时,环形中心钝体驻涡燃烧室典型截面的压力与流线分布,并对不同后钝体进气位置时驻涡腔内的流线、平均速度、平均静压以及燃烧室总压损失系数的变化规律进行比较.结果表明:不同后钝体进气位置时,驻涡腔内均形成了4个旋涡,但驻涡腔内旋涡的大小、形状和位置略有不同;在各个后钝体进气位置时,驻涡腔内的平均速度随后钝体进气位置向驻涡腔外侧偏移逐渐减小,平均静压、平均湍流度逐渐增大;燃烧室出口总压损失在后钝体进气位置为1.5时出现最小值,在后钝体进气位置为0.75时其次,其值为0.0799;燃烧室出口总压和出口气流速度沿径向随后钝体进气位置改变变化不大.

本文引用格式

高翠翠 , 韩吉昂 , 钟兢军 , 李晓东 . 环形中心钝体驻涡燃烧室后钝体进气位置研究[J]. 大连海事大学学报, 2017 , 43(1) : 24 -32 . DOI: 10.16411/j.cnki.issn1006-7736.2017.01.005

Abstract

The flow field of an annular central bluff-body trapped vortex combustor with different air injection position on aft-bluff-body was simulated by using the fluent software. Streamlines and pressure distribution on typical cross-section were analyzed in detail under different air injection position on aft-bluff-body. The vortex structure, averaged flow parameters of the trapped vortex cavity and the performance of the annular central bluff-body trapped vortex combustor under different air injection position on aft-bluff-body were comparatively analyzed. Results show that the relatively stable vortex structure can all be formed in the trapped vortex cavity under different air injection position, except the slightly different in size, shape and position of the vortex in the trapped vortex cavity. With air injection position moving outside, the average velocity in the trapped vortex cavity decreases, and the average static pressure and averaged turbulence intensity increases. The total pressure loss coefficient of the combustor is minimal when air injection position on aft-bluff-body is 1.5, followed is when the air injection position on aft-bluff-body is 0.75 with a value 0.0799.The air injection position on aft-bluff-body has little influence on changing trend of flow parameters along flow-path height direction at the exit of the annular central bluff body trapped vortex combustor.

参考文献

[1]HSU K Y,GOSS L P,ROQUEMORE W M. Characteristics of a trapped-vortex combustor[J].Journal of Propulsion and Power,1998,14(1):57-65.
[2]HSU K Y,CARTER C,KATTA V,et al. Characteristics of combustion instability associated with trapped-vortex burner[C]//37th Aerospace Sciences Meeting and Exhibit. Reston,VA:AIAA,1999.
[3] 王璐.某型驻涡燃烧室冷却技术研究[D].南京:南京航空航天大学,2012.
WANG Lu. Research on cooling technology of a trapped vortex combustor[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2012.(in Chinese)
[4] 何小民,张净玉.驻涡燃烧室燃烧组织方式和设计思路分析[J].航空科学技术,2008(2):26-29.
HE Xiao-min,ZHANG Jing-yu. Combustion buildup and design routine of trapped vortex combustor[J].Journal of Aeronautical Science and Technology,2008(2):26-29.(in Chinese)
[5]KENDRICK D,LAWLOR S P,STEELE R C. Trapped vortex combustor:US,US20040020211A1[P].2004-02-05.
[6]BUCHER J,EDMONDS R G,STEELE R C,et al.The development of a lean-premixed trapped vortex combustor[C]//ASME:Combustion and Fuels,2003.
[7]EDMONDS R G,STEELE R C,WILLIAMS J T,et al.Ultra-low NOx advanced vortex combustor[C]//Proceedings of ASME Turbo Expo 2006 Power for Land,Sea,and Air,2006.
[8]LAWLOR S P,STEELE R C,BALDWIN P. Advanced supersonic component engine for military applications[C]//ASME Turbo Expo 2007:Power for Land,Sea,and Air,2007.
[9] 刘河霞,刘玉英,李瑞明,等.驻涡燃烧室凹腔供油位置对流场影响的PIV实验[J].航空动力学报,2009,24(10):2272-2276.
LIU He-xia,LIU Yu-ying,LI Rui-ming,et al. Experimental study on the influence of fuel supply position of concave cavity on the flow field in trapped vortex combustor by PIV[J]. Journal of Aerospace Power,2009,24(10):2272-2276.(in Chinese)
[10] 严明,樊未军,朱菁,等.利用PIV技术对二维驻涡燃烧室冷态流场的初步研究[C]//中国工程热物理学会燃烧学学术会议论文集.大连:中国工程热物理学会,2004.
YAN Ming,FAN Wei-jun,ZHU Jing,et al. Study on the cold flow field of the trapped vortex combustor using the PIV technique[C]//Chinese Society of Engineering Thermophysics, Proceedings of Combustion Conference.Dalian: Chinese Society of Engineering Thermophysics,2004.(in Chinese) 
[11] 何小民,许金生,苏俊卿.驻涡区进口结构参数影响TVC燃烧性能的试验[J].航空动力学报,2008,22(11):1798-1802.
HE Xiao-min,XU Jin-sheng,SU Jun-qing. Effect of air and fuel injection patterns in pilot zone on trapped vortex combustor performance[J].Journal of Aerospace Power,2008,22(11):1798-1802.(in Chinese) 
[12] 钟兢军,刘世青.后驻体喷孔位置对驻涡腔流动冷态数值的影响[J].上海海事大学学报,2011,32(1):44-48.
ZHONG Jing-jun,LIU Shi-qing.Impact of nozzle position on after body on cold flow field values in trapped vortex chamber[J].Journal of Shanghai Maritime University,2011,32(1):44-48.(in Chinese)
[13] 王志凯,曾卓雄,徐义华.后钝体开口先进旋涡燃烧室燃烧特性的数值研究[J].弹箭与制导学报,2015,35(2):81-87.
WANG Zhi-kai,ZENG Zhuo-xiong,XU Yi-hua. Numerical analysis of combustion characteristics in AVC with a slot in the rear blunt body[J].Journal of Projectiles,Rockets,Missiles and Guidance,2015,35(2):81-87.(in Chinese)
[14] 徐舟,曾卓雄,徐义华.含导流片及钝体的驻涡燃烧室的结构优化[J].推进技术,2015,36(7):1020-1026.
XU Zhou,ZENG Zhuo-xiong,XU Yi-hua. Structure optimization of trapped vortex combustor with guide vane and bluff body[J]. Journal of Propulsion Technology,2015,36(7):1020-1026.(in Chinese) 
[15] 王志凯,曾卓雄,徐义华.先进旋涡燃烧室后钝体开口结构的数值研究[J].推进技术,2014,35(6):809-814.
WANG Zhi-kai,ZENG Zhuo-xiong,XU Yi-hua. Numerical simulation of open structure of rear blunt body in advanced vortex combustor[J]. Journal of Propulsion Technology,2014,35(6):809-814.(in Chinese)
[16] 张敏.环形驻涡燃烧室冷态流动特性的数值研究[D].大连:大连海事大学,2013.
ZHANG Min. The numerical study of the cold flow properties in the annular central bluff-body trapped vortex combustor[D].Dalian:Dalian Maritime University,2013.(in Chinese) 
[17] 韩吉昂,李晓东,钟兢军.环形中心钝体驻涡燃烧室驻涡腔有无喷射的对比[J].航空动力学报,2015,30(2):331-340.
HAN Ji-ang,LI Xiao-dong,ZHONG Jing-jun. Comparison of trapped vortex cavity with/without injection in annular central bluff-body trapped vortex combustor[J].Journal of Aerospace Power,2015,30(2):331-340.(in Chinese)
[18] 韩吉昂,李晓东,钟兢军,等.环形中心钝体驻涡燃烧室进气方式研究[J].推进技术, 2015,36(8):1206-1214.
HAN Ji-ang,LI Xiao-dong,ZHONG Jing-jun,et al.Study of air injection mode in an annular central bluff-body trapped vortex combustor[J]. Journal of Propulsion Technology,2015,36(8):1206-1214.(in Chinese)
[19] 刘世青.驻涡燃烧室流动特性的冷态数值研究[D].大连:大连海事大学,2011.
LIU Shi-qing.The numerical study of the cold flow properties in the trapped vortex combustor[D].Dalian:Dalian Maritime University,2011.(in Chinese)
[20] 樊未军,易琪,严明,等.驻涡燃烧室凹腔双涡结构研究[J].中国电机工程学报,2006, 26(9):66-70.
FAN Wei-jun,YI Qi,YAN Ming,et al.A study of double vortex structure in the trapped vortex combustor[J].Proceedings of the CSEE,2006, 26(9):66-70.(in Chinese)
[21] 刘世青,钟兢军,程平.喷射孔径影响驻涡燃烧室性能冷态数值研究[J].汽轮机技术,2010,52(2):107-111.
LIU Shi-qing,ZHONG Jing-jun,CHENG Ping.Numerical investigation on the influence of the injection nozzle size from center body in cold flow field of the trapped vortex combustor[J].Journal of Turbine Technology,2010,52(2):107-111.(in Chinese)

文章导航

/