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凹槽导叶式处理机匣轴向叠合量对风扇性能的影响

陈向艺 楚武利 张皓光 王维 李金鸽

陈向艺, 楚武利, 张皓光, 王维, 李金鸽. 凹槽导叶式处理机匣轴向叠合量对风扇性能的影响[J]. 航空动力学报, 2018, 33(6): 1413-1422. doi: 10.13224/j.cnki.jasp.2018.06.015
引用本文: 陈向艺, 楚武利, 张皓光, 王维, 李金鸽. 凹槽导叶式处理机匣轴向叠合量对风扇性能的影响[J]. 航空动力学报, 2018, 33(6): 1413-1422. doi: 10.13224/j.cnki.jasp.2018.06.015
Effects of blade chord exposure of recess vaned casing treatment on fan performance[J]. Journal of Aerospace Power, 2018, 33(6): 1413-1422. doi: 10.13224/j.cnki.jasp.2018.06.015
Citation: Effects of blade chord exposure of recess vaned casing treatment on fan performance[J]. Journal of Aerospace Power, 2018, 33(6): 1413-1422. doi: 10.13224/j.cnki.jasp.2018.06.015

凹槽导叶式处理机匣轴向叠合量对风扇性能的影响

doi: 10.13224/j.cnki.jasp.2018.06.015
基金项目: 国家自然科学基金(51576162);国家自然科学基金重点项目(51536006)

Effects of blade chord exposure of recess vaned casing treatment on fan performance

  • 摘要: 为探索凹槽导叶式处理机匣(RVCT)轴向叠合量对风扇性能的影响,选取升力风扇为对象,采用数值模拟方法对实壁机匣和4种不同轴向叠合量的凹槽导叶式处理机匣进行研究。结果表明:随着轴向叠合量的增大,带处理机匣风扇相比实壁机匣风扇裕度分别改进1.27%、8.01%、12.3%、32.4%,设计点效率分别下降了0.82%、1.38%、2.2%、4.1%;处理机匣的引入使得凹槽与主流通道间形成局部循环流动,减小了来流攻角和叶顶低能流体的堆积,平衡了叶顶吸、压力面压差,且轴向叠合量越大,局部循环越强烈,风扇稳定性提高;凹槽与风扇主流间的交互流动决定着处理机匣对风扇性能的影响,其中抽吸流和喷射流是反映处理机匣扩稳效果的两个重要参数。

     

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出版历程
  • 收稿日期:  2016-12-19
  • 刊出日期:  2018-06-28

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