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自循环机匣处理轴向位置影响扩稳能力的机理

张皓光 安康 谭锋 楚武利 吴艳辉

张皓光, 安康, 谭锋, 楚武利, 吴艳辉. 自循环机匣处理轴向位置影响扩稳能力的机理[J]. 航空动力学报, 2017, 32(4): 983-989. doi: 10.13224/j.cnki.jasp.2017.04.026
引用本文: 张皓光, 安康, 谭锋, 楚武利, 吴艳辉. 自循环机匣处理轴向位置影响扩稳能力的机理[J]. 航空动力学报, 2017, 32(4): 983-989. doi: 10.13224/j.cnki.jasp.2017.04.026
Mechanism of affecting ability of stability enhancement with varying axial position of self-recirculating casing treatment[J]. Journal of Aerospace Power, 2017, 32(4): 983-989. doi: 10.13224/j.cnki.jasp.2017.04.026
Citation: Mechanism of affecting ability of stability enhancement with varying axial position of self-recirculating casing treatment[J]. Journal of Aerospace Power, 2017, 32(4): 983-989. doi: 10.13224/j.cnki.jasp.2017.04.026

自循环机匣处理轴向位置影响扩稳能力的机理

doi: 10.13224/j.cnki.jasp.2017.04.026
基金项目: 国家自然科学基金(51006084);航空科学基金(2014ZB53014);中央高校基本科研业务费专项资金(3102014JCY01004);陕西省自然科学基金(2015JM5202)

Mechanism of affecting ability of stability enhancement with varying axial position of self-recirculating casing treatment

  • 摘要: 为了揭示自循环机匣处理轴向位置影响压气机稳定性的流动机理,采用非定常数值方法研究了3种不同轴向位置对机匣处理(CT)扩稳能力的影响,结果表明:机匣处理喷气装置离叶顶前缘最近且在叶顶前缘上游的扩稳能力最强,喷气装置在叶顶前缘正上方的次之,喷气装置在叶顶前缘上游较远处的最弱,对应机匣处理获得的综合失速裕度改进量分别为9.40%,7.09%,5.49%.通过详细地分析压气机叶顶流场表明:喷气装置离叶顶前缘最近且在叶顶前缘上游的机匣处理施加有利影响程度最高的范围刚好覆盖叶顶前缘处,此处是引起转子失速的关键部位,因此抑制叶顶间隙泄漏流造成的堵塞的效果最好,对应的扩稳能力在3种机匣处理中最强.

     

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  • 收稿日期:  2015-08-07
  • 刊出日期:  2017-04-28

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