耦合流动控制方法改善高负荷轴流压气机稳定性OA
Improvement of Stability of a High-Loaded Axial Flow Compressor by a Combined Flow Control Method
为解决转子和静子流动失稳几乎同时触发条件下高负荷轴流压气机常规扩稳手段效果有限的问题,以某高负荷轴流压气机为研究对象,开展转静子耦合流动控制方法及其扩稳机理研究.首先,通过分析压气机失稳过程中的内部流场结构,揭示了该压气机流动失稳主要由转子叶顶区域流动堵塞和静子近轮毂区域流动堵塞共同诱发.随后,分别研究了自循环机匣处理、轮毂抽吸以及二者耦合控制方案对压气机内部流动结构和稳定性的影响.结果表明,自循环机匣处理能够改善转子叶顶区域的流通能力,但由于静子近轮毂区域流动堵塞未得到有效抑制,轮毂区域流场更易率先崩溃并触发压气机失稳,因此其失速裕度提升效果有限;轮毂抽吸能够显著改善静子近轮毂区域流场,但因未能有效抑制转子叶顶区域流动堵塞,其扩稳能力同样受限.进一步将自循环机匣处理与轮毂抽吸相结合后,耦合流动控制方法能够同时改善转子叶顶区域和静子近轮毂区域的流动状态,协同抑制两类关键堵塞结构的发展,从而显著拓宽压气机稳定工作范围.采用该耦合流动控制方法后,压气机失速裕度提高了6.78%.研究结果表明,对于转静子流动失稳耦合触发的高负荷轴流压气机,仅针对单一失稳源的控制方法难以获得理想扩稳效果,而面向多失稳源协同抑制的耦合流动控制方法是提升压气机稳定性的有效途径.
This study investigates a high-loaded axial compressor in which flow instabilities in the rotor and the stator occur almost concurrently.Under these conditions,conventional stability enhancement methods prove to be ineffective.The paper proposes a combined rotor-stator flow control technique.This study reveals that the flow field deterioration stems from combined flow blockage at the rotor tip region and the near-hub region of the stator.Research on flow control methods finds that self-recirculating casing treatment can effectively improve flow capacity in the rotor tip region,but simultaneously reduce flow capacity in the near-hub zone.This makes the hub flow field more susceptible to breakdown and ultimately triggers compressor instability.Thus,the self-recirculating casing treatment fails to enhance stall margin.By contrast,hub suction significantly improves the hub-region flow field.Yet without suppressing the rotor-tip flow blockage,it achieves limited stability enhancement.The integrated solution combining self-recirculating casing treatment with hub suction simultaneously addresses flow blockage at both the rotor tip and the stator near-hub regions.This combined flow control method delivers effective stability enhancement,achieving 6.78%increase in compressor stall margin.
孟德君;尹海宝;刘杰
中国航空发动机集团有限公司沈阳发动机研究所,沈阳 110015,中国中国航空发动机集团有限公司沈阳发动机研究所,沈阳 110015,中国中国航空发动机集团有限公司沈阳发动机研究所,沈阳 110015,中国
航空航天
轴流压气机高负荷稳定性耦合流动控制方法流动机理
axial flow compressorhigh loadstabilitycombined flow control methodflow mechanism
《南京航空航天大学学报(英文版)》 2026 (2)
286-300,15
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