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Y型喷嘴反压环境粒径的图像捕捉测量技术

王丹 陈鹏飞 杨岸龙 李龙飞

王丹, 陈鹏飞, 杨岸龙, 李龙飞. Y型喷嘴反压环境粒径的图像捕捉测量技术[J]. 航空动力学报, 2018, 33(1): 174-181. doi: 10.13224/j.cnki.jasp.2018.01.021
引用本文: 王丹, 陈鹏飞, 杨岸龙, 李龙飞. Y型喷嘴反压环境粒径的图像捕捉测量技术[J]. 航空动力学报, 2018, 33(1): 174-181. doi: 10.13224/j.cnki.jasp.2018.01.021
Granulometric technique by photographic methods ofYjet nozzles under back pressure condition[J]. Journal of Aerospace Power, 2018, 33(1): 174-181. doi: 10.13224/j.cnki.jasp.2018.01.021
Citation: Granulometric technique by photographic methods ofYjet nozzles under back pressure condition[J]. Journal of Aerospace Power, 2018, 33(1): 174-181. doi: 10.13224/j.cnki.jasp.2018.01.021

Y型喷嘴反压环境粒径的图像捕捉测量技术

doi: 10.13224/j.cnki.jasp.2018.01.021

Granulometric technique by photographic methods ofYjet nozzles under back pressure condition

  • 摘要: 鉴于Y型喷嘴反压条件下的粒径难以采用传统光学测量手段获得有效数据,提出一种基于图像捕捉的粒径处理程序,通过微距镜头拍摄雾场图像,通过图像识别和数据统计获取有效索太尔平均直径(SMD)。该处理方法在大气下与相位多普勒粒子分析仪(PDPA)测量结果误差不超过12%。实验结果表明:在反压条件下,当气流量为0g/s时,雾化粒径较大,随着环境压力升高和液流量增大,雾化粒径呈减小趋势;当加入气流量为55g/s时,雾化粒径显著降低,并且粒径随着环境压力升高而增大(该结果与不加气时恰恰相反),而在同一反压、不同液流量工况下,雾化粒径基本保持不变。在燃烧室变工况条件下,加入少量的气体即可使雾化粒径显著减小且在变工况条件下基本保持一致。

     

  • [1] 侯凌云,侯晓春.喷嘴技术手册[M].2版.北京:中国石化出版社,2007.
    [2] LHUISSIER H,VILLERMAUX E.Effervescent atomization in two dimensions[J].Journal of Fluid Mechanics,2013,714(1):361-392.
    [3] SHEEPARD D T,LUEPTOW R M.Characterization of fire sprinkler sprays using particle image velocimetry[J].Atomization and Sprays,2005,15(3):341-362.
    [4] VILLERMAUX E.Fragmentation[J].Annual Review of Fluid Mechanics,2007,39(1):419-446.
    [5] SONG Yubao,ZHANG Mingchuan.Mathematical modeling and experimental verification of interior gasliquid flows and outflow atomization process for Yjet nozzles[J].Atomization and Sprays,2004,14(6):437=-458.
    [6] 纪利俊,陈葵,武斌,等.Y型气流式喷嘴的雾化滴径和滴径分布[J].高校化学工程学报,2009,23(4):577-581.JI Lijun,CHEN Kui,WU Bin,et al.Droplet size and droplet size distribution of Ytype airblast nozzel[J].Journal of Chemical Engineering of Chinese Universities,2009,23(4):577-581.(in Chinese)
    [7] 马其良,张松寿.Y型喷嘴油雾两相流中雾化细度的差异性研究[J].工业炉,1998(1):9-12.MA Qiliang,ZHANG Songshou.Study on the difference of dropsize (SMD) of a Ytype atomizer[J].Journal of Industrial Furnance,1998(1):9-12.(in Chinese)
    [8] 李广军,王新军,向宇,等.燃油喷嘴气液两相流雾化特性研究[J].热能动力工程,1999,14(4):253-256.LI Guangjun,WANG Xinjun,XIANG Yu,et al.A study of the twophase flow atomizing characteristics of oil spray nozzles[J].Journal of Engineering for Thermal Energy and Power,1999,14(4):253-256.(in Chinese)
    [9] 周月桂,曹威城,柳瑶斌,等.大流量单混合孔Y型喷嘴的雾化特性[J].动力工程,2007,27(6):980-984.ZHOU Yuegui,CAO Weicheng,LIU Yaobin,et al.Atomization characteristics of Yjet nozzles with single large flow mixing orifices[J].Journal of Power Engineering,2007,27(6):980-984.(in Chinese)
    [10] 陈鹏飞,王丹,王玫,等.反压条件下Y型喷嘴的变工况试验[J].火箭推进,2016,42(6):25-30.CHEN Pengfei,WANG Dan,WANG Mei,et al.Experimental study on variableflow performance of Yjet nozzle at back vessel pressure[J].Journal of Rocket Propulsion,2016,42(6):25-30.(in Chinese)
    [11] DUMOUCHEL C,YONGYINGSAKTHAVORN P,COUSIN J.Light multiple scattering correction of laserdiffraction spray dropsize distribution measurements[J].International Journal of Multiphase Flow,2009,35(3):277-287.
    [12] LEE I,KIM D,KOO J.Breakup structure of twophase jets with various momentum flux from a porous injector[J].Journal of Thermal Science,2014,23(1):60-67.
    [13] LUBARSKY E,GOPALA Y,BIBIK O,et al.Experimental investigation of spray dynamics in crossflow of preheated air at elevated pressure[R].AIAA2006-1342,2006.
    [14] 周兵,吉洪湖,张宝诚.旋流空气对双油路离心喷嘴雾化特性影响的实验[J].航空动力学报,2013,28(9):1933-1941.ZHOU Bing,JI Honghu,ZHANG Baocheng.Experiment of swirled air effect on spray characteristic of doubleline pressureswirl atomizer[J].Journal of Aerospace Power,2013,28(9):1933-1941.(in Chinese)
    [15] 郭新华,林宇震,张弛,等.离心式同向双旋流器空气雾化喷嘴雾化特性研究[J].航空动力学报,2009,24(10):2249-2254.GUO Xinhua,LIN Yuzhen,ZHANG Chi.Experiment investigation on atomization characteristic of an airblast atomizer with centrifugal nozzle and codualswirl cup[J].Journal of Aerospace Power,2009,24(10):2249-2254.(in Chinese)
    [16] 刘丹阳,韩雅慧,丁立,等.水滴撞击特性参数的动态图像测量方法[J].航空动力学报,2012,27(5):986-992.LIU Danyang,HAN Yahui,DING Li,et al.Dynamic image processing mesurement method of droplets impingement characteristics[J].Journal of Aerospace Power,2012,27(5):986-992.(in Chinese)
    [17] GADGIL H P,DOLATABADI A,RAGHUNANDAN B N.Mass distribution studies in effervescent sprays[J].Atomization and Sprays,2011,21(5):375-390.
    [18] PASTOR J V,ARRGLE J,PALOMARES A.Diesel spray image segmentation with a likelihood ratio test[J].Applied Optics,2001,40(17):2876-2885.
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出版历程
  • 收稿日期:  2016-05-30
  • 刊出日期:  2018-01-28

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