Volume 37 Issue 3
Mar.  2022
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GUI Tao, XIA Limin, QIU Wei, FANG Renlin. Effect of swirler types on spray characteristics of airblast atomizer[J]. Journal of Aerospace Power, 2022, 37(3): 465-477. doi: 10.13224/j.cnki.jasp.20210163
Citation: GUI Tao, XIA Limin, QIU Wei, FANG Renlin. Effect of swirler types on spray characteristics of airblast atomizer[J]. Journal of Aerospace Power, 2022, 37(3): 465-477. doi: 10.13224/j.cnki.jasp.20210163

Effect of swirler types on spray characteristics of airblast atomizer

doi: 10.13224/j.cnki.jasp.20210163
  • Received Date: 2021-04-09
  • Publish Date: 2022-03-28
  • The influences of different swirler types on the spray characteristics of dual-stage swirl airblast atomizer were investigated by using a combination method with experiment and numerical calculation.Particle image velocimetry (PIV) was applied to measure the downstream flow field structures of different swirler types,a high-speed camera and a laser particle size analyzer were used to photograph the atomization morphology,measure Sauter mean diameter (SMD) and Rosin-Rammler distribution under different air flow and fuel flow rates.At the same time,the secondary atomization characteristics of the dual-axial swirl cup were obtained by using the numerical calculation method.The results showed that,under the same working conditions,the atomization cone angle of the atomizer with two-stage axial swirler was slightly larger than that of the radial swirler.The atomization process with dual-stage radial swirler mainly relied on its centrifugal atomization of the atomizer,and the air assisted atomization was limited.The atomization process with dual-stage axial swirler was mainly affected by the first atomization of the atomizer when the pressure loss of swirl cup was small.With the increase of pressure loss,the air assisted atomization effect gradually played a major role.The numerical calculation results were in good agreement with the experimental results,indicating that the numerical calculation method can be used to simulate the atomization process of the dual-stage swirl airblast atomizer,and the numerical results can be used to explain the secondary atomization process.

     

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  • [1]
    MONGIA H,AL-ROUB M,DANIS A,et al.Swirl cup modeling:Ⅰ[R].Cambridge,US:the 37th Joint Propulsion Conference and Exhibit,2001.
    [2]
    刘存喜.多级旋流空气雾化喷嘴雾化特性及光学测试方法研究[D].北京:中国科学院,2012.
    [3]
    张弛,张荣伟,徐国强,等.直射式双旋流式空气雾化喷嘴的雾化效果[J].航空动力学报,2006,21(5):805-809.
    [4]
    徐华胜,黄义勇,王秀兰.喷嘴供油特性对双涡流器头部气动雾化效果的影响研究[J].燃气涡轮试验与研究,2004,17(2):14-17.
    [5]
    王志凯,陈盛,刘冉,等.双级轴向旋流杯气量比对雾化性能影响的试验[J].航空动力学报,2019,34(12):2656-2662.
    [6]
    郭新华,林宇震,张驰,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.
    [7]
    金仁瀚,刘勇,冯志鹏,等.双旋流燃烧室但头部油雾特性实验[J].航空动力学报,2014,29(2):250-258.
    [8]
    陈俊,吉洪湖,张宝诚.双路离心喷嘴雾化特性的实验[J].航空动力学报,2010,25(4):774-779.
    [9]
    张善军,金戈,贾春燕,等.离心喷嘴偏心和凸凹对双旋流器空气雾化特性的影响[J].航空发动机,2015,41(4):65-68.
    [10]
    康尧,林宇震,霍伟业,等.双级旋流杯结构变化对点火特性的影响研究[J].推进技术,2014,35(5):675-680.
    [11]
    于锦峰,郭志辉,张君锋,等.套筒长度对火焰筒流场和雾化特性的影响[J].航空动力学报,2009,24(11):2506-2513.
    [12]
    SUN Y,ALKHEDHAIR A M,GUAN Z,et al.Numerical and experimental study on the spray characteristics of full-cone pressure swirl atomizers[J].Energy,2018,160(C):678-692.
    [13]
    YOO Y L,HAN D H,HONG J S,et al.A large eddy simulation of the breakup and atomization of a liquid jet into a cross turbulent flow at various spray conditions[J].International Journal of Heat and Mass Transfer,2017,112:97-112.
    [14]
    李营,陆欣.高温高压下燃油二次雾化特性的数值研究[J].柴油机设计与制造,2013,19(3):1-4.
    [15]
    HASSANI M A,ELKAIE A,SHAFAEE M.Numerical investigation of the full-cone spray structure and characteristics provided by a jet-swirl atomizer[J].Journal of Aerospace Engineering,2019,233(15):5788-5800.
    [16]
    LING Y,ZALESKI S,SCARDOVELLI R.Multi-scale simulation of atomization with small droplets represented by a Lagrangian point-particle model[J].International Journal of Multiphase Flow,2015,76(1):122-143.
    [17]
    MEHDI B,ANDREALBERT D M,PIERRE-JEAN P S,et al.Aerodynamic fuel injection system for a gas turbine engine: US6035645[P].2000-03-14.
    [18]
    王廷俊.基于视觉的航空油雾喷嘴雾化角度自动检测装置[J].中国设备工程,2018(3):94-96.
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