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组合型机匣处理提高轴流压气机稳定性的机理

张皓光 王云鹏 吴俊 楚武利 吴艳辉

张皓光, 王云鹏, 吴俊, 楚武利, 吴艳辉. 组合型机匣处理提高轴流压气机稳定性的机理[J]. 航空动力学报, 2015, 30(1): 228-236. doi: 10.13224/j.cnki.jasp.2015.01.030
引用本文: 张皓光, 王云鹏, 吴俊, 楚武利, 吴艳辉. 组合型机匣处理提高轴流压气机稳定性的机理[J]. 航空动力学报, 2015, 30(1): 228-236. doi: 10.13224/j.cnki.jasp.2015.01.030
ZHANG Hao-guang, WANG Yun-peng, WU Jun, CHU Wu-li, WU Yan-hui. Mechanism of improvement on axial-flow compressor stability with assembled casing treatment[J]. Journal of Aerospace Power, 2015, 30(1): 228-236. doi: 10.13224/j.cnki.jasp.2015.01.030
Citation: ZHANG Hao-guang, WANG Yun-peng, WU Jun, CHU Wu-li, WU Yan-hui. Mechanism of improvement on axial-flow compressor stability with assembled casing treatment[J]. Journal of Aerospace Power, 2015, 30(1): 228-236. doi: 10.13224/j.cnki.jasp.2015.01.030

组合型机匣处理提高轴流压气机稳定性的机理

doi: 10.13224/j.cnki.jasp.2015.01.030
基金项目: 

陕西省自然科学基金(2011JQ7018)

西北工业大学基础研究基金(JC201116)

国家自然科学基金重点项目(51236006)

中央高校基本科研业务费专项资金(3102014JCY01004)

国家自然科学基金(51006084)

详细信息
    作者简介:

    张皓光(1981-),男,广西宾阳人,副教授,博士,研究领域为叶轮机械气动热力学.

  • 中图分类号: V231.3

Mechanism of improvement on axial-flow compressor stability with assembled casing treatment

  • 摘要: 用全通道非定常计算方法研究了轴向倾斜缝、自适应机匣处理及两者形成的组合型机匣处理对亚声速轴流式转子稳定工作范围的影响,结果表明:轴向倾斜缝、自适应机匣处理及组合型机匣处理取得的综合裕度改进量分别为12.86%,16.47%及22.72%,其中组合型机匣处理扩稳效果最强,自适应机匣处理次之.通过详细地分析压气机内部流场表明,组合型机匣处理削弱了叶片吸力面气流分离带来的不良影响.从喷气装置流出的高速气流抑制了叶顶间隙泄漏流从相邻叶片叶顶前缘溢出的现象,部分叶片通道受到轴向倾斜缝的作用,泄漏流线被抽吸入缝中,也能抑制前缘溢流的产生.

     

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出版历程
  • 收稿日期:  2013-09-10
  • 刊出日期:  2015-01-28

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