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机匣处理改善某单级跨声轴流压气机性能的机理研究
引用本文:杜辉,滕金芳.机匣处理改善某单级跨声轴流压气机性能的机理研究[J].航空动力学报,2011,26(9):2089-2094.
作者姓名:杜辉  滕金芳
作者单位:1. 北京航空航天大学能源与动力工程学院,北京,100191
2. 上海交通大学航空航天学院,上海,200240
摘    要:采用全三维数值方法研究了轴向倾斜缝机匣处理对某单级跨声轴流压气机性能的影响.数值结果表明:机匣处理不仅扩宽压气机稳定工作范围,而且还略微提高了单级跨声轴流压气机峰值效率.通过详细分析压气机转子内部流场,揭示了该机匣处理对该单级跨声轴流压气机性能及流场影响的机理,在倾斜缝中形成的回流作用下,使叶顶吸力面气流分离的起始位置...

关 键 词:轴流压气机  机匣处理  压气机性能  泄漏流  流动机理
收稿时间:2010/10/19 0:00:00
修稿时间:2011/4/11 0:00:00

Study on the flow mechanisms of casing treatment on a transonic single stage axial-flow compressor
DU Hui and TENG Jin-fang.Study on the flow mechanisms of casing treatment on a transonic single stage axial-flow compressor[J].Journal of Aerospace Power,2011,26(9):2089-2094.
Authors:DU Hui and TENG Jin-fang
Affiliation:School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;School of Aeronautics and Astronautics, Shanghai Jiaotong University, Shanghai 200240, China
Abstract:The influences of axial skewed slot casing treatment on the performance of a transonic single stage axial-flow compressor were investigated through three-dimensional(3-D) numerical method. The numerical results indicate that the stable operating range of axial compressors is enlarged and the compressor efficiency is increased with casing treatment appreciably. The flow mechanisms of affecting compressor performance were obtained by analyzing in detail the flow-filed in compressor rotor with casing treatment. It was found that the starting location of flow separation near rotor blade suction was moved backward by the back flow formed in the slots, which weakened the adverse influence rooted in interaction of separated flow and tip leakage flow and improved the current ability of blade tip passage. So the compressor stall was suspended.
Keywords:axial-flow compressor  casing treatment  compressor performance  leakage flow  flow mechanisms
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