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某型航空发动机用离心喷嘴燃油空间分布特性试验

刘存喜 刘富强 毛艳辉 穆勇 徐纲

刘存喜, 刘富强, 毛艳辉, 穆勇, 徐纲. 某型航空发动机用离心喷嘴燃油空间分布特性试验[J]. 航空动力学报, 2013, 28(4): 783-791.
引用本文: 刘存喜, 刘富强, 毛艳辉, 穆勇, 徐纲. 某型航空发动机用离心喷嘴燃油空间分布特性试验[J]. 航空动力学报, 2013, 28(4): 783-791.
LIU Cun-xi, LIU Fu-qiang, MAO Yan-hui, MU Yong, XU Gang. Experiment of fuel distribution of pressure-swirl atomizers for aero-engine[J]. Journal of Aerospace Power, 2013, 28(4): 783-791.
Citation: LIU Cun-xi, LIU Fu-qiang, MAO Yan-hui, MU Yong, XU Gang. Experiment of fuel distribution of pressure-swirl atomizers for aero-engine[J]. Journal of Aerospace Power, 2013, 28(4): 783-791.

某型航空发动机用离心喷嘴燃油空间分布特性试验

基金项目: 国家重点基础研究发展计划(2007CB210109)

Experiment of fuel distribution of pressure-swirl atomizers for aero-engine

  • 摘要: 建立了平面激光诱导荧光(PLIF)用于燃油分布特性测量的试验装置及其校正方法,并验证了校正方法的有效性.PLIF和平面激光散射(PLS)方法的燃油分布特性测量结果表明PLS方法对直径小于50μm的液滴存在非线性效应使小液滴集中区燃油分布测量结果偏大,PLIF方法适合燃油分布特性测量.利用PLIF方法从喷雾锥角、燃油周向分布不均匀度和分布指数等方面综合评价燃油空间分布特性.偏心和尺寸大小不等的凹槽等分布不均匀的表现形式表明:造成燃油分布不均匀的因素包括喷嘴内部通道表面粗糙度、喷射孔圆度和零件之间的同轴度.利用PLIF方法研究雾锥在供油压差分别为0.14,0.25,2.5MPa时雾锥沿喷射方向的发展过程,液滴随雾锥发展逐渐从环形集中区分散到整个雾锥横截面,并且液滴分散过程随供油压差增加而加快.

     

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出版历程
  • 收稿日期:  2012-05-09
  • 刊出日期:  2013-04-28

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