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离心压气机级串列叶栅扩压器内流场的数值研究

周莉 韦威 蔡元虎

周莉, 韦威, 蔡元虎. 离心压气机级串列叶栅扩压器内流场的数值研究[J]. 航空动力学报, 2012, 27(11): 2562-2568.
引用本文: 周莉, 韦威, 蔡元虎. 离心压气机级串列叶栅扩压器内流场的数值研究[J]. 航空动力学报, 2012, 27(11): 2562-2568.
ZHOU Li, WEI Wei, CAI Yuan-hu. Numerical investigation on flowfield of centrifugal compressor with tandem cascade diffuser[J]. Journal of Aerospace Power, 2012, 27(11): 2562-2568.
Citation: ZHOU Li, WEI Wei, CAI Yuan-hu. Numerical investigation on flowfield of centrifugal compressor with tandem cascade diffuser[J]. Journal of Aerospace Power, 2012, 27(11): 2562-2568.

离心压气机级串列叶栅扩压器内流场的数值研究

基金项目: 国家自然科学基金(50906071); 西北工业大学基础研究基金(JC201011); 西北工业大学翱翔之星

Numerical investigation on flowfield of centrifugal compressor with tandem cascade diffuser

  • 摘要:

    对某一带串列叶栅扩压器的离心压气机级进行了数值模拟,分析了串列叶栅扩压器后排叶片不同周向位置对压气机级流动及性能的影响.结果表明:串列叶栅扩压器性能优于单列叶栅扩压器,其后排叶片在不同周向位置处效率和压比均优于单列叶栅扩压器,效率提高幅度能达到1.9%,压比的提高幅度为2.85%.串列扩压器分流叶片的周向位置对其内部流动情况有显著影响,两排叶片之间存在一个最佳位置使扩压器损失最小.串列叶栅扩压器的主要损失集中在50%叶高以上的区域.

     

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  • 收稿日期:  2011-11-28
  • 刊出日期:  2012-11-28

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