Volume 34 Issue 10
Oct.  2019
Turn off MathJax
Article Contents
CHEN Lei, LONG Wuqiang. Experiment on atomization of high disturbance fuel nozzle[J]. Journal of Aerospace Power, 2019, 34(10): 2091-2097. doi: 10.13224/j.cnki.jasp.2019.10.002
Citation: CHEN Lei, LONG Wuqiang. Experiment on atomization of high disturbance fuel nozzle[J]. Journal of Aerospace Power, 2019, 34(10): 2091-2097. doi: 10.13224/j.cnki.jasp.2019.10.002

Experiment on atomization of high disturbance fuel nozzle

doi: 10.13224/j.cnki.jasp.2019.10.002
  • Received Date: 2019-01-24
  • Publish Date: 2019-10-28
  • In order to improve the fuel atomization and verify the feasibility of high perturbed atomization scheme applied to the fuel injection of aero-engine, the spray characteristics of V-shaped cross hole nozzlesand single hole nozzles were measured by using phase Doppler particle analyzer (PDPA) and high-speed photography technology. Results showed that with the increase of injection pressure, the atomization angle increased and the Sauter mean diameter(SMD) value decreased. The cross-hole structure had a significant promoting effect on fuel atomization. Under the same injection pressure and exit cross-section area conditions, the atomization cone angle of the cross-hole was larger and the SMD was smaller; at the same SMD, the required injection pressure of the cross-hole was much smaller than that of the traditional circular straight hole; with the increase of intersection angle, the spray cone angle and SMD were both improved. Air-assisted method can effectively increase the spray cone angle and reduce the SMD value, but the improvement effect decreased gradually with the increase of air pressure. Compared with the traditional single hole nozzle scheme, the high perturbation nozzle can greatly improve the atomization effect of the fuel under the same pressure conditions, and has great potential for aero engine application.

     

  • loading
  • [1]
    张宝诚.航空发动机燃烧室的现状和发展[J].航空发动机,2013,39(6):67-73.ZHANG Baocheng.Status and development of aeroengine combustors[J].Aeroengine,2013,39(6):67-73.(in Chinese)
    [2]
    甘晓华.航空燃气轮机燃油喷嘴技术[M].北京:国防工业出版社,2006:15-55.
    [3]
    LECUORT R,BARRICAU P,STEELANT J.Spray velocity and dropsize measurements in flashing conditions[J].Journal of the International Institutes for Liquid Atomization and Spray Systems,2008,19(2):103-133.
    [4]
    马洪安,张宝诚,刘凯.某型航空发动机燃油喷嘴对比试验研究[J].航空发动机,2009,35(3):54-57.MA Hongan,ZHANG Baocheng,LIU Kai.Comparative experiment study of fuel nozzles for an aeroengine[J].Aeroengine,2009,35(3):54-57.(in Chinese)
    [5]
    姚春德,耿培林,银增辉,等.喷嘴结构对喷雾特性的影响[J].内燃机学报,2016,34(1):41-47.YAO Chunde,GENG Peilin,YIN Zenghui,et al.Effect of nozzle geometry on spray characteristic[J].Transactions of CSICE,2016,34(1):41-47.(in Chinese)
    [6]
    黄豪中,安彦召,苏万华,等.喷射压力和喷孔直径对柴油机混合燃料喷雾特性的影响[J].内燃机学报,2013,31(3):200-207.HUANG Haozhong,AN Yanzhao,SU Wanhua,et al.Investigation on the influence of injection pressure and nozzle diameter on thespray of blended fuel in diesel engine[J].Transactions of CSICE,2013,31(3):200-207.(in Chinese)
    [7]
    王振华,王亮.航空发动机试验测试技术发展探讨[J].航空发动机,2014,40(6):47-51.WANG Zhenhua,WANG Liang.Development of aeroengine testing measurement technology[J].Aeroengine,2014,40(6):47-51.(in Chinese)
    [8]
    董全,隆武强,田江平,等.激光诊断及数值仿真在柴油机V形交叉孔油嘴研究上的应用[J].内燃机工程,2012,33(4):28-35.DONG Quan,LONG Wuqiang,TIAN Jiangping,et al.Application of laser diagnosis and numerical simulation in study on V-type intersecting hole nozzle for diesel engine[J].Chinese Internal Combustion Engine Engineering,2012,33(4):28-35.(in Chinese)
    [9]
    董全.交叉孔和外开式喷油器喷雾特性的测量研究[D].辽宁 大连:大连理工大学,2012.DONG Quan.Diagnostics for the spray characteristics of intersecting hole injectior and outwards-opening injector[D].Dalian Liaoning:Dalian University of Technology,2012.(in Chinese)
    [10]
    冷先银,金煜,何志霞,等.交叉孔喷油嘴内部流动特性的模拟[J].内燃机学报,2015,33(6):522-529.LENG Xianyin,JIN Yu,HE Zhixia,et al.Numerical simulation on internal flow characteristics of intersecting hole nozzles[J].Transactions of CSICE,2015,33(6):522-529.(in Chinese)
    [11]
    隋永旭.柴油机交叉孔喷油嘴内三维流动分析[D].辽宁 大连:大连理工大学,2011.SUI Yongxu.Analysis on the flow in the intersecting hole nozzle of diesel engines[D].Dalian Liaoning:Dalian University of Technology,2011.(in Chinese)
    [12]
    伍文锋,吴建华,钟柳花,等.航空发动机燃油喷嘴雾化角度测量研究[J].航空发动机,2017,43(5):69-73.WU Wenfeng,WU Jianhua,ZHONG Liuhua,et al.Research on aeroengine fuel nozzle spray angle masurement[J].Aeroengine,2017,43(5):69-73.(in Chinese)
    [13]
    张宇璠.柴油机交叉孔喷嘴自由喷雾与平板碰撞特性实验研究[D].辽宁 大连:大连理工大学,2016.ZHANG Yupan.Experimental study on free and flat wall impinging spray characteristics of diesel V-type intersecting-hole nozzles[D].Dalian Liaoning:Dalian University of Technology,2016.(in Chinese)
    [14]
    金煜.交叉孔喷油嘴内部流动和喷雾特性的研究[D].江苏 镇江:江苏大学,2017.JIN Yu.Researches on the internal flow and spray characteristics for intersecting-hole nozzles[D].Zhenjiang Jiangsu:Jiangsu University,2017.(in Chinese)
    [15]
    赵明.交叉孔喷油嘴与双层分流燃烧系统的喷雾和燃烧特性实验研究[D].辽宁 大连:大连理工大学,2015.ZHAO Ming.Experimental study on spray and combustion characteristics of V-type intersecting hole nozzle and in double-layer diverging combustion system[D].Dalian Liaoning:Dalian University of Technology,2015.(in Chinese)
    [16]
    于忠强.空气雾化喷嘴雾化特性的实验研究[D].辽宁 大连:大连理工大学,2014.YU Zhongqiang.An experimental study on the spray char acteristics of the air-blast atomizer[D].Dalian Liaoning:Dalian University of Technology,2014.(in Chinese)
    [17]
    HU Jingchao,LIU Bolan,ZHANG Chao,et al.Experimental study on the spray characteristics of an air-assisted fuel injection system using kerosene and gasoline[J].Fuel,2019,235:782-794.
    [18]
    衡思江.小型航空发动机气动雾化喷嘴雾化特性研究[D].北京:中国科学院,2015.HENGSijiang.Investigations of spray characteristics of air-blast fuel nozzle for small aircraft engine[D].Beijing:Chinese Academy of Sciences,2015.(in Chinese)
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (793) PDF downloads(396) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return